Self-propelled tillage machine with modularly constructed and mounted energy source

Abstract

A self-propelled soil tillage machine (10) with a trunk soil tillage machine (11), the trunk soil tillage machine (11) comprising: - a machine frame (12), - a drive (28), - a chassis (26) with a plurality of running gears (20, 22) which can roll on a base (U), - a working device (42), wherein the working device (42) has a working tool (44) designed for soil cultivation, - a control station (34), and - a control device (38), wherein the hull-type soil tillage machine (11) is designed to accommodate a power arrangement (56), wherein the power arrangement (56) comprises a power device (58) designed to provide working energy for operating at least one of the consumers of the soil tillage machine (10). The hull-type soil tillage machine (11) comprises: - a first storage interface (62), - a first signal interface (92), and - at least one working energy interface (84), wherein the power arrangement (56) has a first support device (60) which supports the power device (58; 58'), wherein the first support device (60) has a first bearing counter-interface (64) for connection to the trunk soil tillage machine (11), and wherein the power device (58) is held on the first support device (60) by a connection of a power device interface (68) and a power device counter-interface (66).

Description

The present invention relates to a self-propelled soil working machine having a hull soil working machine, wherein the hull soil working machine comprises:a machine frame,a travel drive as a first consumer of the soil-working machine,a running gear having a plurality of running gears which can roll on a base and which carries the machine frame standing on the base, at least one running gear being drivable by the running gear,a working device as a second consumer of the soil-working machine, wherein the working device has a working tool designed for soil working,an operator stand as the workplace of an operator operating the floor processing machine, anda control device for controlling an operation of the soil working machine.The fuselage soil-working machine and of this machine frame in particular are designed to receive a force arrangement as a force source of the soil-working machine, wherein the force arrangement comprises a force device which is designed to provide working energy for operation of at least one of the consumers of the soil-working machine.Such a soil-working machine is generally known, for example from DE 10 2021 129 619 A1 or DE 10 2014 011 195 A1. As in the case of DE 10 2021 129 619 A1, the self-propelled soil-working machine is also preferably intended in the present application to be a road milling machine, a stabilizer, a recycler or a surface miner. The working tool is therefore preferably a rotating working tool which is designed for removing material from the ground, in particular a milling drum having a plurality of milling chisels which are supported on the outer side of a milling drum tube, preferably in a helical arrangement.At present, self-propelled soil-working machines, such as in particular road milling machines, stabilizers, recyclers and surface miners, are constructed from their individual parts, wherein individual functional assemblies, such as, for example, an internal combustion engine as the central power source of the soil-working machine, a running gear with revolving track, the working device or / and the working tool, and the like, are mounted as pre-mounted assemblies on the self-propelled soil-working machine produced during assembly.Different secondary requirements placed on the soil-working machine away from the direct soil-working, for example with regard to noise emission, dirt emission in different fields of application, in particular due to different legislation, different availability of energy quantities and / or energy forms and different technical boundary conditions for the respective working operation, can under certain circumstances no longer be fulfilled in the desired quality by a single soil-working machine. Manufacturers of self-propelled soil-working machines are therefore faced with the increasingly more demanding challenge of providing a soil-working machine which is as suitable as possible for a respective case of demand.This provision of soil-working machines which are suitably equipped for a predetermined machining spectrum but are constructed differently in order to fulfil the machining spectrum while taking into account existing secondary requirements leads without further measures to a considerable additional outlay at least in assembly and consequently probably also to an increased space requirement for assembly, since without further measures it is not to be expected that, with regard to their energy conversion and / or their energy transmission, conceptually different soil-working machines can be mounted at one and the same mounting location without problems.It is therefore the object of the present invention to reduce the effort required for providing soil processing machines which, although suitable for completing one and the same soil processing spectrum, differ conceptually with respect to an energy conversion and / or energy transmission always required on a soil processing machine, and to enable economic diversification of the product range of soil processing machines for one and the same processing spectrum.Even today, manufacturers of soil-working machines already provide different soil-working machines for a similar working spectrum, because it is based on the same physical operating principle. However, these soil-working machines differ primarily by their performance limits, i.e. substantially by a dimensioning of their working device, in particular of their working tool, and consequently by the power consumption of the working device. Thus, different soil working machines are offered for different working widths and / or different work capacities, which in turn can be equipped with different working tools for similar soil workings, because soil working according to the same physical principle of action, in particular soil removing soil but not identical in the working result.In the particularly preferred case of removing soil working, different removal widths can be realized by soil working machines with working tools of different widths. Different removal priorities, such as the greatest possible removal power compared to the most finely machined ground surface, can be realized by working tools with removal devices, such as milling cutters, which differ in terms of their construction and / or number and / or arrangement.The machining spectrum that can be performed by a floor machining machine results from the totality of working tools that can be attached to one and the same basic device. The basic device is essentially determined by its machine frame, which sets limits for the working devices and / or working tools that can be attached to it. In the technical field of particular interest here of soil-removing milling machines, different milling tools can be mounted on one and the same basic device, which milling tools differ in their respective milling widths, which can be selected within a predetermined milling width range, or / and which can differ in terms of the number and / or the shape of the milling chisels mounted thereon.However, independently of a pallet available for a given soil working machine on different working devices and working tools, the remaining soil working machine, i.e. the basic device, generally remains unchanged in the region of its working device due to the selection of components.The present invention is therefore not based on the question of how one and the same soil-processing machine can be made usable for different processing tasks, but rather how one and the same soil-processing machine can best fulfil one and the same soil-processing task under different legal and / or technical and / or economic boundary conditions. This naturally also does not exclude a change of working device and / or working tool on a soil working machine according to the invention. Such a change is, however, not necessary for achieving the object defined above.This object is achieved according to the invention in that the soil cultivation machine is constructed in modular fashion with respect to its force arrangement as its force source.This makes it possible, already during the planning of the soil-working machine, to select a force arrangement which is particularly suitable for the later application from a plurality of different, fundamentally possible force arrangements and to install it on the soil-working machine.To realize the modular construction with regard to the force arrangement, the fuselage soil-working machine comprises:a first mounting interface for the preferably intentionally detachable physical connection of the force arrangement to the machine frame,a first signal interface for establishing a signal-transmitting first signal connection, preferably as intended, between the control device and the force arrangement, andat least one working energy interface for establishing a working energy connection, preferably as intended, which transmits working energy, between the at least one load and the force arrangement.By means of the interfaces mentioned, the power arrangement can be connected mechanically to the fuselage soil working machine through the first mounting interface, in terms of signal and data transmission through the first signal interface and for the transmission of working energy to the at least one consumer through the working energy interface.The connection of an arrangement mentioned in the present invention, such as the above of the power arrangement, to the fuselage soil-working machine ultimately means a direct or indirect connection of the components to the machine frame.The first bearing interface can comprise a plurality of mechanical coupling and / or fastening means. Possible coupling means can be, for example, bearing recesses or bearing projections. Possible fastening means can be connecting means, such as at least one fastening opening with a form-fit contour, such as in particular an internal thread, or / and at least one fastening projection with a form-fit contour, such as in particular an external thread. The mechanical coupling and / or fastening means of the first bearing interface are preferably designed for complementary interaction with a corresponding first bearing mating interface on the side of the force arrangement. According to a possible solution, which is however less preferred because of its lower flexibility after a connection of the force arrangement and the fuselage soil-working machine has taken place, the first bearing interface can be at least one joining formation for producing an intended non-detachable joining connection, such as by riveting or welding.The first signal interface may comprise a plug and / or a socket and / or a plurality of plugs and / or sockets or any other type of electrical or electronic coupling means. The first signal interface makes it possible, by preferably complementary coupling to a correspondingly configured first signal mating interface, to exchange signals and data between the components and / or modules thus coupled.The at least one working energy interface serves to transmit working energy provided by the force arrangement. Depending on the configuration of the respective consumer, the working energy interface can comprise or be, for example, a shaft stub or a hub, a transmission means arranged on a shaft stub, such as, for example, a gearwheel or a friction wheel for a gear train, or a drive belt for a belt drive and the like. At least one working energy interface of the at least one working energy interface can therefore be designed for the transmission of mechanical working energy, that is to say by input of working energy or working power in the form of force and / or torque and movement.Depending on the form in which the working energy is required at a consumer and is provided by the force arrangement, a working energy interface of the at least one working energy interface can be an interface for fluid transmission, in particular for transmission of a liquid, such as hydraulic oil, or of a gas, such as compressed air. The working energy interface can then comprise or be a fluid quick coupling known per se. Such a case can occur, for example, when at least one consumer is a hydraulic motor customary on soil-working machines or a hydraulic piston-cylinder arrangement for which potential working energy is provided by the force arrangement in the form of a quantity of hydraulic fluid at a predetermined pressure level, generally exceeding the atmospheric pressure of the environment. The same applies to the provision of potential working energy in the form of a quantity of gas at a predetermined gas pressure level for at least one pneumatic consumer, such as a pneumatic piston-cylinder arrangement.Likewise, working energy can be electrical energy, for instance when a load is an electrical load, such as an electric motor, a data processing device, such as the control device, a lighting device and the like. Then, at least one working energy interface of the at least one working energy interface can be an electrical interface, that is to say, for example, an electrical plug or an electrical socket. A plurality of working energy interfaces can each be designed as an electrical interface in order to enable use of electrical energy in different forms of development on one and the same soil-working machine. Thus, electrical energy with different frequencies up to the direct current and / or with different voltages and / or with different current intensities can be transmitted to different working energy interfaces.For the case that a plurality of consumers operating according to different physical principles of action are provided on the processing machine, which forms the rule rather than an exception, the soil processing machine preferably has a plurality of working energy interfaces on the side of its machine frame, preferably at least one for each energy form transmitted from the force arrangement to the consumers.For connection to the fuselage soil-working machine, in particular to the machine frame, the force arrangement has, by means of the first mounting interface, a first carrying device which is formed separately from the machine frame and carries the force device. For this purpose, the first support device has a first mounting counter interface for the preferably intentionally detachable physical connection of the force arrangement to the fuselage soil-working machine, in particular to the machine frame. The first support device as a kind of adapter or "shape imparting device" between the fuselage soil-working machine on the one hand and force arrangements on the other hand is an essential component which, during the production of the soil-working machine, enables the quick and uncomplicated, but nevertheless permanent and secure arrangement of different force devices, which operate above all on the basis of different physical principles of action, on the fuselage soil-working machine, in particular on the machine frame.For fastening the force device to the first support device, the force device has a force device interface and the first support device has a force device counter interface different from the first bearing counter interface. In embodiments of the invention, the force device interface cannot be directly coupled to the first mounting interface, for example on account of its shape and / or its connection locations. Regardless of which power device is accommodated on the first support device, the first support device respectively supporting the power device can always be connected to the fuselage soil working machine, in particular to the machine frame, by using the first support interface and the first support counter interface. If different force arrangements with different first support devices are provided for a soil working machine, the mechanical connectivity of the different force arrangements to and thus their storage capacity on the fuselage soil working machine can be ensured by using a quasi-standardized connection of the first bearing interface and the first bearing counter interface.The force device in turn is held on the first support device by a connection of the force device interface to the force device counter interface. The force device interface may include one or more force device bearing formations. The force device counter-interface can have one or more force device abutment formations which can be coupled to the force device bearing formations, wherein force device bearing formations and force device abutment formations in the coupled state are secured or securable against lifting from one another, in particular by positive locking. With regard to the configuration of force device bearing formations and abutment formations, the statements made above with regard to the configuration of the first bearing interface and counter-interface apply accordingly and vice versa.Thus, different first support devices can be prepared for different force devices, the only structural boundary condition of which is the formation or arrangement of a respective force device mating interface. The respective force device counter-interface of a first support device is customized to the respective force device to be received and its force device interface.Therefore, a plurality of different force arrangements can be provided for a production set of components for producing the soil working machine, which differ with respect to their force device, but only to a limited extent with respect to their respective first support devices. The first support devices preferably differ only in their respective force device mating interface for fastening the respective force devices thereto, since each force device will have its own force device bearing formations in individually different shapes and / or at individually different locations.Although it is not necessary, for reasons of simplified production and assembly, the first supporting devices of different force arrangements of the production set, which are basically provided for producing the floor processing machine, are preferably designed and configured identically, with the exception of the individual force device mating interface.The advantage is obvious: with the first support device interposed, a fuselage soil-working machine without a force arrangement can always be designed substantially the same for the purpose of accommodating a force arrangement. Strictly speaking, it is also this in the prior art, with the difference that only exactly one force device without a first support device fits onto the "fuselage soil treatment machine" prepared in this way and can be connected to it. According to the present invention, on the other hand, the force arrangement, regardless of the type, can be connected as a pre-assembled assembly via the connection of the first mounting interface to the first mounting counter-interface quickly, without problems, permanently and securely to the machine frame of the fuselage soil-working machine. On the other hand, on the machine frame side of the fuselage soil-working machine there is preferably no interface for the direct reception of the force device.Since the first mounting interface and the first mounting counter-interface are an interface formation for connecting three-dimensional bodies to one another, both the first mounting interface and the first mounting counter-interface preferably comprise a plurality of cooperating and preferably complementary connection formations.For reasons of increased strength and rigidity, the first bearing interface and the first bearing mating interface are preferably configured for direct connection to one another, preferably as intended. However, a modular construction of the soil-working machine can alternatively require that the first mounting interface and the first mounting mating interface are designed for, preferably intendedly detachable, indirect connection with the intermediate arrangement of at least one force-imparting device, wherein the force-imparting device is different from the first support device. The prefix "force-" is intended here only to indicate that the switching device is used to fix the force arrangement to the machine frame. The switching device can be an adapter which can be connected on its one functional side to the first mounting interface and which can be connected on its other functional side to the first mounting mating interface. Such a force-transmitting device can be, for example, a further carrying device of a functional arrangement other than the force arrangement, as will be described in more detail below.In order to be able to control the force arrangement during operation to the necessary extent and / or in order to be able to detect states and operating states of the force arrangement and to be able to be processed by the control device, the force arrangement can comprise a first signal mating interface which is designed as part of the first signal connection for establishing a signal-transmitting signal coupling, which is preferably releasable as intended, with the first signal interface. The first signal interface and the first signal mating interface can preferably be connected to one another without tools, for example by producing a plug connection. The first signal interface and the first signal mating interface are preferably designed with electrical contacts which are physically complementary to one another, for example as a plug and socket and / or as a contact shoe and contact tongue and the like. The first signal interface and the first signal mating interface can each be realized by an interface body, which ensures particularly fast and simple connectivity. The first signal interface and the first signal counter interface can, however, also be formed by a plurality of interface sub-bodies which can be connected separately to one another, for example if, starting from the force arrangement, signals have to be transmitted to different locations on the machine frame and / or via different lines and / or if the installation space available is not sufficient for forming a single interface body.An undesired disconnection of the produced plug connection between the first signal interface and the first signal mating interface can be achieved by positively locking the bodies carrying the respective contacts to one another. Therefore, one interface of the first signal interface and the first signal mating interface can have a locking formation and the respective other interface can have a locking mating formation cooperating positively with the locking formation.The first signal counter-interface can be connected to at least one sensor or / and to a local control device of the force device or / and to at least one actuator on the force device in a signal-transmitting and / or data-transmitting manner.To output the required working energy, the force arrangement can comprise at least one working energy counter-interface which is designed to establish the working energy connection, which preferably is intended to be detachable, transmitting working energy, with the at least one working energy interface. In this case, at least one working energy counter-interface of the at least one working energy counter-interface can be designed for direct connection to at least one working energy interface of the at least one working energy interface, and / or at least one working energy counter-interface of the at least one working energy counter-interface can be designed for indirect connection to at least one working energy interface of the at least one working energy interface with the interposition of a transmission device. Such a transmission device can be, for example, a transmission or linkage which connects a working energy counter-interface outputting mechanical working energy to a working energy interface receiving mechanical working energy. In the case of a provision of potential working energy in the form of a fluid quantity, in particular hydraulic fluid quantity, which is at a predetermined pressure level, a transmission device can be realized by a fluidic line arrangement, in particular a hose arrangement and / or pipe arrangement. In the case of a provision of electrical working energy, a transmission device can comprise an electrical line arrangement, optionally with the inclusion of electrical circuits, such as a transformer for changing the electrical voltage and / or a converter for generating and / or changing a frequency of an electrical current provided as working energy. A possible objection, electric current and electric energy, which are different entities, is only theoretically correct in the present case, but irrelevant for the soil working machine under consideration. This is because the working electric energy serves to perform work by the working device and is thus provided as working electric energy per time, consequently as electric power. Electrical power is the product of an electrical voltage and the current flowing at that voltage. Using a converter, both the electrical voltage provided and the current flow caused by this voltage have a frequency. It should be noted here that an alternating electric current on soil-working machines is essentially required for feeding alternating-current or three-phase motors, while other electric loads, as is customary for vehicles, are generally operated with direct current.According to the first principle of thermodynamics, energy cannot be consumed. At most, some of the energy is dissipated to the environment as a thermal loss without any further useful value. Since the required working energy is not available as mechanical energy and is often not readily available in the required quantity in another energy form in a storable manner, the power device preferably has at least one energy conversion machine which converts operating energy of one energy form fed into it on the output side into working energy of another energy form. The power device can have an internal combustion engine and / or an electric motor and / or a fluid motor, in particular a hydraulic motor, as the energy conversion machine. The energy conversion machine in this case directly outputs mechanical energy to a moving output member such as a rotating output shaft. The mechanical energy output by the energy conversion machine can be work energy directly or / and, as will be explained further below, can be converted into another energy form before being supplied to a consumer.The soil cultivation machine preferably has an energy supply arrangement with at least one energy supply device for supplying the power device with operating energy. Not only the use of different power arrangements, but also the different availability of energy forms and / or energy quantities at different locations of use, provision of different energy supply devices for arrangement on the fuselage soil-working machine can make it advantageous.In principle, the energy supply device can be mounted directly fixedly on the machine frame without utilizing a modular construction without a second support device via individual fastening locations and means. Energy supply device bearing formations on the energy supply device are then directly physically connected to energy supply device abutment formations on the machine frame. In this case, the power supply device is the power supply arrangement. However, it is preferably provided that the soil working machine is also modular with regard to its energy supply arrangement as its energy source.The basic idea of modularity in the present invention comprises the basic construction of a functional arrangement consisting of a functional device and a supporting device supporting the functional device. For example, the above-described force arrangement is constructed as a functional arrangement.Accordingly, the energy supply arrangement can have as a further possible functional arrangement according to a preferred development of the soil treatment device discussed in the present case:the energy supply device,a second support device formed separately from the machine frame, the second support device supporting the energy supply device, andan operating energy counter interface which is designed to produce an operating energy coupling, preferably capable of being released as intended, transmitting operating energy, with an operating energy interface.The second support means serves to facilitate the use of different power supply arrangements on one and the same fuselage soil-working machine.The second support device comprises a second support counter-interface which is designed for the preferably intentionally detachable physical fixing of the second support device to a second support interface. The second support device also preferably comprises an energy supply device mating interface having one or more energy supply device abutment formations for physical connection to an energy supply device interface of the respective energy supply device in order to fix the energy supply device to the second support device. The energy supply device interface can comprise at least one energy supply device bearing formation which can be physically connected to the at least one energy supply device abutment formation of the energy supply device mating interface. Of the possible multiple energy supply arrangements of an above-mentioned production set, preferably all the second support devices each have at least the same second bearing mating interface. The second support devices of the production set, however, are likely to have different power supply device mating interfaces adapted to the respective power supply device to be mounted thereon.Therefore, a plurality of different energy supply arrangements can be provided for a production set of components for producing the soil working machine, which energy supply arrangements differ only with regard to their energy supply device. Although the second support devices can be designed differently as long as they have only the second bearing mating interface, the second support devices are preferably of substantially the same structure for ease of manufacture and assembly and preferably differ only in their respective energy supply device mating interfaces, since each energy supply device will have its own energy supply device interface at individually different bearing locations. When an energy supply device is fixed to a second support device, the specific configuration of the energy supply device mating interfaces no longer plays a role for the further mounting of the energy supply arrangement formed in this way on the fuselage floor processing machine.According to a preferred development of the invention, in this case, in fundamental agreement with the statements made above for the first mounting interface applies in particular to the second mounting interface and the second mounting counter-interface,the second bearing interface and the second bearing counter interface can be configured for direct connection to one another, preferably as intended, orthe second mounting interface and the second mounting counter interface can be designed for indirect connection, preferably releasable as intended, with the intermediate arrangement of at least one power supply switching device, wherein the power supply switching device is different from the second support device.Again, the addition "power supply" merely indicates the assignment of the mentioned switching device to the power supply arrangement. Otherwise, the statements made in the present application regarding the force switching device apply to the energy supply switching device.The second bearing interface can be formed directly on the machine frame.The second support device may be the above-mentioned force imparting device and thus may support the force arrangement in addition to the power supply device. It can likewise be provided to fix the second support device to the first support device, so that the energy supply arrangement can be mounted as a premountable module on the first support device. In the latter case, the first support means supports the power means and the power supply arrangement. Finally, the first support device can be the second support device. Then, the first support means supports the power means and the power supply means. In all of the aforementioned embodiments, the first storage interface is also the second storage interface. In both the first-mentioned cases, the force arrangement and the energy supply arrangement can be arranged on the machine frame as a pre-assembled superordinate functional module, despite a respective modular design. In the third case mentioned, the force device, the energy supply device and the first support device likewise form a pre-assembled functional module. Thus, an installation space provided or reserved for functional modules on the machine frame can be optimally utilized, because the individual division of the available installation space between the force arrangement and the energy supply arrangement can take place on the support device directly carrying a functional device and a functional arrangement.Further alternatively, the first and the second mounting interface can be formed separately from one another in different regions on the fuselage soil-working machine, in particular on the machine frame. In this case, the power arrangement and the energy supply arrangement can be fixed independently of one another directly on the fuselage soil processing machine, in particular on the machine frame.What has been stated in the present application for the possible configuration of the first storage interface applies mutatismutatatively correspondingly to the second storage interface.The operating energy interface is designed to establish an operating energy connection, preferably releasable as intended, transmitting operating energy, between the energy supply device and the force device and is arranged on the force arrangement. The operating energy interface can be arranged on the first support device or on the force device. The operating energy can be electrical energy, so that the operating energy interface and the operating energy counter-interface can each have electrical contacts that are physically matched to one another for the production of an electrical line. The electrical contacts, which are dimensioned in accordance with the expected electrical power to be transmitted, can be realized physically complementarily as male and female contacts. The operating energy interface and the operating energy counter interface can be designed as a plug and socket.As already explained above in connection with the first signal interface and the first signal mating interface, the operating energy interface and the operating energy mating interface, as well as any other interface-mating interface combination of the present invention that transmits a fluid or electric current, can also be secured against undesired separation from one another, in particular can be locked to one another by positive locking.The operating energy can be energy stored in fluid, i.e. liquid and / or gaseous, fuels. The operating energy interface and the operating energy counter interface can then be coupling sections of a fluidic quick-action coupling that are complementary to the formation of a fluid line.Rather less preferably than basically possible, the operating energy can be provided as potential energy of a fluid quantity under elevated pressure. In this case as well, the operating energy interface and the operating energy counter interface can be complementary coupling sections of a fluidic quick-action coupling to form a fluid line.For the provision of operating energy, the energy supply device can have at least one device from: a. a tank for storing fluid fuel, b. an internal combustion engine whose output shaft is coupled to the input shaft of a generator, c. an internal combustion engine whose output shaft is coupled to the input shaft of a fluid pump, i.e. an electric motor whose output shaft is coupled to the input shaft of a fluid pump, e. an electrical energy store, f. a photovoltaic arrangement, g. a fuel cell arrangement, h. an electrical line arrangement for connection to an external power source.The enumeration is expressly not exhaustive.Variant a. provides energy usable in a fluid by combustion. The variants b., e., f., g. and h. provide electrical energy as operating energy. Variants c. and d. provide potential energy in the form of a fluid quantity under elevated pressure, in particular hydraulic fluid quantity. Said fluid pump may be a gas compressor or a hydraulic pump. A hydraulic pump is preferred because of the high compressibility of gas to a hydraulic fluid. Variant a. can be combined with a variant of b., c. and g.In order to be able to control the energy supply arrangement during operation to the necessary extent, if necessary, and / or in order to be able to detect states and operating states of the energy supply arrangement and process them by the control device, the energy supply arrangement can comprise a second signal mating interface which is designed as part of a second signal connection for producing a signal-transmitting signal coupling, which is preferably releasable as intended, with a second signal interface which is connected to the control device and is provided on the fuselage floor processing machine. The second signal interface and the second signal mating interface can preferably be connected to one another without tools, for example by producing a plug connection. The statements made above regarding the configuration of the first signal interface and the first signal mating interface, including their lockability to one another, applies as a protection against undesired separation, correspondingly to the second signal interface and the second signal mating interface in a mutual mutant manner.In many cases, the working energy interface of a consumer, in particular of a plurality of consumers, is spaced too far from the working energy counter-interface of the force arrangement in order to connect the working energy interface and the working energy counter-interface to one another in a directly energy-transmitting manner. In order to connect the working energy interface and the working energy counter-interface to one another, the soil cultivation machine can therefore have a transmission arrangement. The transmission arrangement is then arranged in or on the soil working machine for establishing at least one section of the working energy connection. The transmission arrangement preferably has at least one mechanical output.In this case, a mechanical output of the at least one mechanical output is preferably connected or connectable to the working device for transmitting torque by a mechanical transmission energy connection as part of the working energy connection to the at least one load, and / or at least one mechanical output of the at least one mechanical output is connected to an energy converter for converting mechanical energy into another energy form. Energy of the energy form converted by the at least one energy converter is preferably transmittable as working energy by a fluidic and / or electrical transmission energy connection as part of the working energy connection to the at least one load. According to a preferred embodiment of the invention, the energy converter connected to the at least one mechanical output of the transmission arrangement can comprise or be a fluid pump, in particular a hydraulic pump, for generating a fluid flow, in particular hydraulic flow and / or a fluid pressure level, in particular a hydraulic pressure level, and / or the energy converter can comprise or be an electrical generator.The transmission energy connection is an energy connection in which the "transmission" addition merely indicates that the energy connection is assigned to the transmission arrangement and serves for the energy-transmitting connection of the transmission arrangement to at least one load. A mechanical transmission energy connection may comprise or be a drive belt and / or a transmission and / or linkage. A fluidic transmission energy connection can comprise or be at least one fluid line, in particular fluid hose and / or fluid pipe. An electrical transmission energy connection can comprise or be at least one electrical line.Although the power device as shown above can output potential energy as working energy, the power device preferably comprises a thermal or electric engine and outputs mechanical energy as working energy. The working energy counter-interface preferably has an output shaft or output hub for outputting the mechanical working energy. The transmission device can have an input shaft or input hub designed for connection to the working energy counter interface. The transmission device may have an output shaft or output hub configured for connection to the working energy interface.As a functional or transmission device, the transmission arrangement can comprise a transfer case with an input shaft and with at least one output shaft or generally a tapping point, preferably with a plurality of output shafts or generally with a plurality of tapping points, for energy or power that can be tapped at the output side of the transmission arrangement. The transmission arrangement can in particular comprise a so-called pump transfer case, which has at least one auxiliary output, preferably a plurality of auxiliary outputs, to which a hydraulic pump for driving through the transfer case is connected in each case. At least one hydraulic pump can, however, be replaced, if necessary, by an electric generator and / or by a gas compressor, if there is a corresponding need for electric current or compressed gas at the soil working machine. In addition, the pump distribution gear preferably has a mechanical main output which makes a mechanical power input at the input of the pump distribution gear tappable on the output side of the pump distribution gear. This mechanical main output is preferably coupled to the working device in a force-transmitting and / or torque-transmitting manner, in particular to its working energy interface. The main output drive is generally that output drive of the transfer case with the largest power take-off. Main drives and auxiliary drives usually also differ in the transmission ratio from the input side to the output side. This is generally closer to 1 for the main drive than for the auxiliary drives.In order to be able to control the transmission arrangement during operation to the necessary extent, if necessary, and / or in order to be able to detect states and operating states of the transmission arrangement and to be processed by the control device, the transmission arrangement can comprise a third signal mating interface which is designed as part of a third signal connection for producing a signal-transmitting signal coupling, which is preferably releasable as intended, with a third signal interface which is connected to the control device and is provided on the fuselage soil-working machine. The third signal interface and the third signal mating interface can preferably be connected to one another without tools, for example by producing a plug connection. The statements made above regarding the configuration of the first signal interface and the first signal mating interface, including their lockability to one another, applies as a protection against undesired separation, correspondingly to the third signal interface and the third signal mating interface in a mutual mutual mutant manner.Since, as a rule, not only a plurality of consumers but a plurality of consumers operating according to different physical operating principles are arranged on a soil-working machine discussed in the present case, such as, for example, electric motors for motion drives and electric actuators, hydraulic motors and actuators, a mechanical working device, and pneumatic actuators, the at least one working energy interface preferably comprises a mechanical first working energy interface and / or a hydraulic second working energy interface and / or an electrical third working energy interface and / or a pneumatic fourth working energy interface. In particular, the traction drive uses hydraulic motors or also electric motors. Fluidic actuators can be, for example, piston-cylinder arrangements, which serve as steering actuators for steering running gear units of the front axle and / or of the rear axle or as lifting arrangements for lifting and lowering components, such as a roof of the operator's stand and the like.As already indicated above, the transmission arrangement can very generally have a transmission device, wherein the transmission device comprises:an input-side coupling formation for coupling, preferably as intended, to transmit working energy, to the working energy counter-interface, andat least one output-side coupling formation for coupling, preferably as intended, releasable, to the at least one working energy interface and transmitting working energy.Again, the statements made above with respect to the energy supply device also apply, in a corresponding manner, to the transmission device: in principle, without utilizing a modular construction, the transmission device can be mounted fixedly on the machine frame without a carrying device via individual fastening locations and means. A transmission device interface with transmission device bearing formations on the transmission device are then directly physically connected to customised matching transmission device abutment formations on the machine frame. In this case, the transmission device is the transmission arrangement.However, it is precisely the use of different force arrangements on otherwise substantially identical fuselage soil-working machines that can also necessitate or at least make meaningful the use of different transmission arrangements. A third support means may serve to facilitate the use of different transmission arrangements.Therefore, according to a preferred embodiment, the transmission arrangement comprises a third support device which supports the transmission device, wherein the third support device comprises a third support mating interface which is designed for the preferably intentionally detachable physical connection of the third support device to a third support interface. The third support device preferably also comprises a transmission device mating interface with transmission device abutment formations for physical connection to the transmission device interface of a transmission device in order to physically fix the transmission device to the third support device.Therefore, a plurality of different transfer arrangements can be provided for a production set of components for producing the soil working machine, which transfer arrangements differ only with regard to their transfer device. Although the third support devices may be of different design as long as they have only the third bearing mating interface, the third support devices are preferably of substantially the same construction for ease of manufacture and assembly and preferably differ only in their respective transmission device abutment locations, since each transmission device will have its own transmission device bearing locations at individually different locations. If a transmission device is fixed to a third support device, the specific configuration of the transmission device mating interfaces no longer plays a role for the further mounting of the transmission arrangement formed in this way on the fuselage soil-working machine.For the third mounting interface and the third mounting counter-interface, it is preferred that,the third mounting interface and the third mounting counter interface are configured for direct connection to one another, preferably as intended, orthe third mounting interface and the third mounting counter interface are designed for indirect connection, preferably releasable as intended, with the intermediate arrangement of at least one transmission switching device, wherein the transmission switching device is different from the third carrying device.What has been stated in the present application for the possible configuration of the first and second storage interfaces applies mutatismutatatively correspondingly to the third storage interface.The present invention also relates to a production set for a self-propelled soil working machine as described and further developed above, wherein the production set comprises:a fuselage soil working machine as a machine base, comprising• a machine frame,• a travel drive as a first consumer of the soil-working machine,• a running gear having a plurality of running gears which can roll on a base, wherein the running gear carries the machine frame standing on the base, wherein at least one running gear can be driven by the running gear,• a working device as a second consumer of the soil-working machine, wherein the working device has a working tool designed for soil working,• an operator stand as the workplace of an operator operating the floor processing machine, and• a control device for controlling an operation of the soil working machine,• the first storage interface,• the first signal interface, and• the at least one working energy interface,wherein the kit additionally comprises:a plurality of force arrangements as described and further developed above, wherein the force devices of at least two force arrangements provide working energy on the basis of different physical principles of action.Developments of this production set are described in the above description in connection with the provision of a plurality of different energy supply arrangements and / or in connection with the provision of a plurality of different transmission arrangements.For each support device from the above-mentioned first, second and third support devices, it applies that it can comprise a support frame or a support frame which absorbs the weight forces of the functional device and / or functional arrangement supported by the respective support device. In order to reduce weight without appreciable loss of load-bearing capacity, the supporting frame or the supporting frame can be a framework frame or framework frame, preferably comprising struts and connecting nodes. A framework of a support device can be constructed so as to be removable as intended or can be joined in a non-detachable manner as intended, for example by welding and / or riveting. A support device can be formed in one part or in multiple parts. In a multipart design, at least two of the mechanical coupling and / or fastening means of the bearing mating interface of the support device are provided on different parts of the multipart support device, which parts are formed physically separately from one another.A control device mentioned in the present application is preferably a data processing device and as such preferably has at least one integrated circuit and a data memory. The data memory can store an operating program with control commands executable by the at least one integrated circuit. In addition, the data memory can be used to store operating data during the operation of the soil cultivation machine.The basic idea of the present invention can, in contrast to what has been said above, also be realized on a self-propelled soil-working machine having a force device which is fixed to the machine frame directly, i.e. without an intermediate arrangement of a first support device having a first bearing counter-interface and a force device counter-interface, the energy supply arrangement of which is connected to the machine frame with the intermediate arrangement of a second support device described above which supports it, using the second bearing interface and second bearing counter-interface also described above. Such a soil-working machine then has a second carrying device, but no first carrying device. It likewise has a second storage interface, for example, but no first storage interface.Accordingly, in a second embodiment, the present invention also relates in principle to a self-propelled soil-working machine comprising a fuselage soil-working machine, wherein the fuselage soil-working machine has:a machine frame,a travel drive as a first consumer of the soil-working machine,a running gear having a plurality of running gears which can roll on a base and which carries the machine frame standing on the base, at least one running gear being drivable by the running gear,a working device as a second consumer of the soil-working machine, wherein the working device has a working tool designed for soil working,an operator stand as the workplace of an operator operating the floor processing machine, anda control device for controlling an operation of the soil working machine, anda power device having at least one energy conversion machine, wherein the power device is designed to provide working energy for operation of at least one of the consumers of the soil processing machine,wherein the fuselage soil-working machine is designed to receive an energy supply arrangement, wherein the energy supply arrangement comprises an energy supply device which is designed to supply the power device with operating energy.This soil working machine of the second embodiment is further developed according to the basic idea of the present invention in that the hull soil working machine further comprises:a second storage interface for physically connecting the power supply arrangement to the fuselage soil treatment machine, andan operating energy interface for establishing an operating energy connection between the energy supply arrangement and the power device,wherein the power supply arrangement comprises:a power supply device,an operating energy counter-interface, which is designed to establish an operating energy coupling to the operating energy interface, which transmits operating energy, anda second support device formed separately from the machine frame, wherein the second support device supports the energy supply device and wherein the second support device comprises a second support counter interface which is formed for physically fixing the second support device to the second support interface.The energy supply device has an energy supply device interface. The second support device has a power supply device mating interface different from the first mounting mating interface. The power supply device is supported on the second support device by a connection of the power supply device interface and the power supply device mating interface.According to an advantageous refinement, the fuselage soil-working machine can have a second signal interface for establishing a signal-transmitting second signal connection between the control device and the energy supply arrangement. Thus, the control device can, if required, control an operation of the energy supply arrangement and / or detect operating data and operating states of the energy supply arrangement. The energy supply arrangement then preferably has a second signal counter-interface for connection to the second signal interface.The present invention also relates to a second embodiment of a production set adapted to the above second embodiment of the self-propelled soil-working machine. Accordingly, the present invention also relates to a kit for a self-propelled soil working machine of the second embodiment, comprising a hull soil working machine as described on page 27, lines 4 to 28, having the second storage interface, optionally the second signal interface, and the operating energy interface as a machine base. The production set of the second embodiment additionally has a plurality of energy supply arrangements, the energy supply devices of which provide operating energy on the basis of different physical principles of action and / or in different energy forms.Again, the operating energy is an energy form deviating from the energy form of the working energy.Developments and embodiments of the energy supply arrangement, the energy supply device, the power device, the chassis, the traction drive, the working device, the control device, the machine frame and the interfaces, couplings and connections explained within the scope of the first embodiment are also developments and embodiments of the second embodiment, namely both with respect to the soil working machine and with respect to the production set, provided they do not conflict with the above-described basic shape of the second embodiment.It applies both to the first and to the second embodiment that described developments of the soil-working machine are also developments of the production set in the sense that a correspondingly further developed production set contains those components of the fuselage soil-working machine and further components which are required for producing the further developed soil-working machine.As a rule, if the power device is directly connected to the machine frame, a transmission device possibly present, which is coupled to the power device as a section of the working energy connection, will also be directly coupled to the machine frame. The energy supply arrangement is then preferably the only of the above-mentioned arrangements which is connected to the machine frame with the intermediate arrangement of the second supporting device.The second embodiment is of particular interest for power supply arrangements which supply an electrical power device with electrical operating energy. In this case, as in the first embodiment as well, the power device can comprise a plurality of partial power devices which are formed and arranged separately from one another and which each output working energy to a consumer. The number of consumers may be equal to the number of partial force devices, may be greater than the number of partial force devices, or may be less than the number of partial force devices.The present invention will be explained in more detail below with reference to the attached drawings. It represents: FIG. 1 shows a roughly schematic side view of a first part of a first embodiment of a production kit according to the invention and of a self-propelled soil working machine formed therefrom according to the invention, comprising a fuselage soil working machine, a first power arrangement, a first power supply arrangement and a first transmission arrangement, FIG. 2 shows a roughly schematic side view of a second part of the first embodiment of the production kit according to the invention, comprising a second force arrangement, a second and a third energy supply arrangement, a second transmission arrangement, and a first and a second support device in isolation, and FIG. 3 is a diagrammatic partial view of a second embodiment according to the invention of the soil working machine and the production kit according to the present application.FIGS. 1 and 2 show, by way of example, a section of a first embodiment of a production kit 8 according to the invention for producing a self-propelled soil-working machine 10 in the form of a large-scale ground or road milling machine.The observer of FIG. 1 looks at a floor processing machine 10 or "machine" 10 for short, which is produced from components of the production kit 8, in the direction of the cross-machine direction Q orthogonal to the plane of the drawing of FIG. 1 ; a cross-machine direction orthogonal to the cross-machine direction Q is denoted by L and runs parallel to the plane of the drawing of FIG. 1 A machine height direction H likewise runs parallel to the plane of the drawing of FIG. 1 and orthogonal to the longitudinal machine direction L and to the cross-machine direction Q. The arrow tip of the longitudinal machine direction L in FIG. 1 points in the forward direction. The machine height direction H runs parallel to the yaw axis Gi of the machine 10, the machine longitudinal direction L runs parallel to the roll axis Ro and the machine transverse direction Q runs parallel to the pitch axis Ni.The self-propelled soil working machine 10 includes a hull soil working machine 11 as a machine base.The fuselage soil-working machine 11 comprises a machine frame 12 which forms the basic framework for a machine body 14. The machine body 14 comprises the machine frame 12 and components of the machine 10 and of the fuselage soil-working machine 11 which are connected to the machine frame 12 and are possibly movable relative thereto.The machine body 14, the number of components of which increases during the assembly of the self-propelled soil-working machine 10, comprises, on the fuselage soil-working machine 11, front hydraulic lifting columns 16 and rear hydraulic lifting columns 18, which are connected at one end to the machine frame 12 and at the other end to front running gears 20 and to rear running gears 22, respectively.It cannot be seen in the side view of FIG. 1 that the machine 10 has two lifting columns 16 and 18 each with a running gear 20 and 22 connected thereto both in its front end region and in its rear end region. The front lifting columns 16, like the rear lifting columns 18, are each coupled to the running gears 20 and 22 in a manner known per se by means of a running gear connecting structure 24, for example a connecting fork which engages over the respective running gear 20 and 22 in the cross machine direction Q.The running gears 20 and 22 are shown by way of example as tracked running gears. In the exemplary embodiment shown, they are of substantially identical construction and form the chassis 26 of the machine 10 and of the fuselage soil-working machine 11. Each of the running gears 20 and 22 is driven by a motor, in the exemplary embodiment shown by a hydraulic motor 28.In the exemplary embodiment shown, the running gear 20 and the running gear 22 with possible travel directions indicated by the double arrow D each have a radially inner receiving and guiding structure 30, on which a revolving track 32 (only labeled on the front running gear 20) is arranged and guided for revolving movement. The inner guide structure is connected to the drive connection structure 24 in such a way that it can be tilted about a tilting axis parallel to the pitch axis Ni.The distance of the machine frame 12 from the running gears 20 and 22 can be changed by the hydraulic lifting columns 16 and 18.The floor processing machine 10 or the fuselage floor processing machine 11 has a carriage 34, from which a machine operator can control the machine 10 via an operator console 36 with a control device 38 accommodated therein.Below the machine frame 12 is arranged a working device 40, here for example as a milling device 40, with a milling drum 44 accommodated in a milling drum box 42 as a working tool of the working device 40. the milling drum 44 is rotatable about a milling axis R running in the cross-machine direction Q, in order to be able to remove thereby, during soil working, subsurface material starting from the contact surface AO of the subsurface U at a milling depth determined by the relative height position of the machine frame 12 above the contact surface AO. The height adjustability of the machine frame 12 by the lifting columns 16 and 18 consequently also serves for adjusting the milling or general working depth of the machine 10 during soil working. Alternatively or additionally, the milling drum 44 can be accommodated on the machine frame 12 in a height-adjustable manner relative to the latter.For the large road milling machine illustrated in FIG. 1, the arrangement of the milling device 40 in the machine longitudinal direction L between the front and rear running gear units 20 and 22 is typical. Such large milling cutters as well as soil removing machines in general may include a conveyor belt to transport removed soil material away from the machine 10. A conveyor belt which is also fundamentally present in the machine 10 is not shown in FIG. 1 for reasons of better clarity.The lifting column 16 and with it the running gear 20 can be rotated about a steering axis S by a hydraulic steering device 46 which is only indicated roughly schematically. Preferably additionally, but also alternatively, the rear lifting column 18 and with it the running gear 22 can be rotatable by a steering device about a steering axis parallel to the steering axis S.The track 34 is covered by a canopy structure 48 which includes a canopy 50. The protective roof 50 is arranged on the machine frame 12 such that it can be raised and lowered by means of a movement guide 52 and a hydraulic movement drive 54. In FIG. 1, the canopy 50 is shown in its raised operating position in which the machine 10 is ready for a soil cultivation operation.A first force arrangement 56 is arranged on the fuselage soil-working machine 11 in order to form the soil-working machine 10. The fuselage soil working machine 11 receives a power arrangement as a central power plant of the machine 10, which provides substantially the entire working power of the machine 10.The first force arrangement 56 comprises an internal combustion engine 58 as a first force device and comprises a first support device 60. for explaining the configuration of the support device 60, reference is made in addition to FIG. 2, where this is shown in isolation.The fuselage soil-working machine 11 has a first mounting interface 62 on the machine frame 12 or on the machine body 14, on which the first support device 60 is fixed by a first mounting counter-interface 64 arranged on the first support device 60. In the exemplary embodiment shown, the first bearing interface 62 is symbolized by three coupling formations 62 ato which three coupling counterformations 64 aof the bearing counterinterface 64 of the first supporting device 60 are coupled. For a particular positional safety of the arrangement of the first supporting device 60 on the machine frame 12, the coupling formations 62 aand the coupling counter formations 64 aare of complementary design. The coupling formations 62 aand coupling counter formations 64 amay be secured to one another by threaded engagement or by other engagement.The first bearing interface 62 with its coupling formations 62 aand the first bearing mating interface 64 with its coupling mating formations 64 aare again drawn in FIG. 2 for the sake of better clarity.The first bearing mating interface 64 is arranged on the functional side 60 aof the first supporting device 60 assigned to the machine frame 12. The functional side 60 ais also a physical side of the first support device 60.On the functional side 60 bof the first support device 60 opposite the functional side 60 a, the internal combustion engine 58 is arranged. For this purpose, the first support device 60 has, on the functional side 60 b, which is in turn also a physical side of the first support device 60, a force device mating interface 66, on which the internal combustion engine 58 is held by means of its force device interface 68. The power device interface 68 and the power device counter interface 66 can be designed like a motor mounting known per se for mounting an internal combustion engine in a vehicle frame.In FIG. 1, the force device counter-interface 66 is symbolized by two force device abutment formations 66 a. The force device interface 68 is symbolized by two force device bearing formations 68 a.On the functional side 60 bassociated with the functional devices, a pump distributor transmission 70 is also arranged as a transmission device. The first support device 60, which in the illustrated exemplary embodiment supports the transmission device and is consequently also a third support device in the sense of the introduction to the description, has on its functional side 60 atransmission device mating interface 72, symbolized by two transmission device abutment formations 72 a.The pump distributor transmission 70 with its transmission device interface 74 is mounted on the transmission device counter interface 72 in a manner known per se. The transmission device interface 74 is symbolized by two transmission device bearing formations 74 a, of which only the right is provided with a reference sign in FIG. 1 for the sake of better clarity.The pump transfer case 70 and the first and third support means 60 form a transmission arrangement 76.The internal combustion engine 58, for example a diesel internal combustion engine, has, as output element for outputting working power or working energy, an output shaft 78 running orthogonally to the plane of the drawing of FIG. 1 as a working energy counter-interface, which is coupled in the ready-to-use state to an input hub 80 of the pump distributor transmission 70 in a torque-transmitting manner.The pump distributor transmission 70 has as a first mechanical output a belt pulley 82, which can be completed by a drive belt 83 only indicated in FIG. 1 with a belt pulley 84 coupled to the milling drum 44 in a torque-transmitting manner as a working energy interface to form a belt drive. Between the milling drum-side pulley 84 and the milling drum 44, a reduction gear can be arranged, which preferably reduces a rotational speed of the pulley 84 towards the milling drum 44 in a transmission ratio and increases a torque in the reciprocal transmission ratio. Since the transmission-side pulley 82 transmits the working energy required for the working of the milling device 40, the transmission-side pulley 82 forms the main output of the pump distributor transmission 70.A hydraulic pump 86 is arranged on a further output, more precisely on an auxiliary output of the pump distributor transmission 70, which pump during its operation outputs hydraulic fluid at an increased pressure level as fluidic working energy at a quick-coupling formation 88 as a coupling formation. The fluidic working energy of the hydraulic pump 86 can be used by the hydraulic motors 28 for the propulsion of the soil cultivation machine 10, by the hydraulic movement drive 54 of the canopy structure 48 for raising and lowering the canopy 50 and by the steering device 46 for a steering operation of the front lifting columns 16 and / or of the rear lifting columns 18. By means of the hydraulic pump 86, a hydraulic fluid quantity present on the soil working machine 10 can be raised to an increased pressure level via the quick coupling formation 88.The internal combustion engine 58 has its own engine control 90, which, during operation, forms a component control device subordinate to the control device 38. In order to connect the engine control 90 of the internal combustion engine 58 to the control device 38 of the fuselage soil working machine 11 or of the soil working machine 10, the fuselage soil working machine 11 has a first signal interface 92, to which a first signal mating interface 94 of the internal combustion engine 58 can be coupled in a data- and signal-transmitting manner. One of the first signal interface 92 and the first signal mating interface 94 may comprise a plug and the other interface may comprise a mating jack.For supplying fuel as a supplier of operating energy for operating the internal combustion engine 58, the internal combustion engine 58 preferably has a quick-coupling formation 96 as an operating energy interface, through which fuel can be supplied to the internal combustion engine 58.In order to be able to ensure a longer-lasting operation of the internal combustion engine 58, a power supply arrangement 98 is arranged on the fuselage soil working machine 11. The energy supply arrangement 98 supplies the internal combustion engine 58 with operating energy during its operation, i.e. in the present case with fuel.The energy supply arrangement 98 is of modular construction and comprises a tank 100 as energy supply device and a second support device 102 for attachment to the machine frame 12 of the fuselage soil working machine 11 or the soil working machine 10. For this purpose, the fuel delivery line 104 carries a quick coupling counterformation 108 as an operating energy counterinterface, which can be joined together with the internal combustion engine-side quick coupling formation 96 to form the operating energy connection 106 quickly and without tools. The quick coupling formation 96 and the quick coupling counter formation 108 form an operating energy coupling in the coupled, fluid-transmitting state.A delivery module 110 may be arranged in the fuel tank 100, which may be controlled by the control device 38. For this purpose, the fuel tank 100 has a second signal counter-interface 112, which can be coupled to a second signal interface 122, not shown in FIG. 1, on the part of the fuselage floor processing machine 11 for the transmission of signals and data (see FIG. 2 ). The second signal interface 122 can be configured like the first signal interface 92.The fuel tank 100 as a power supply device of the floor processing machine 10 has an individual power supply device interface 114, by means of which it is fixed to a likewise individual power supply device mating interface 116 of the second support device 102. For this purpose, the energy supply device interface 114 has a plurality of energy supply device bearing formations 114 a, which are represented only symbolically and each of which is coupled to a complementary energy supply device abutment formation 116 aand is physically fixed thereto.The energy supply arrangement 98 is fixed via the second support device 102 to a second mounting interface 118 of the machine frame 12 directly on the machine frame 12 or machine body 14. The second support device 102 has a second support mating interface 120 for fixing to the second support interface 118. The second bearing interface 118 is represented in FIG. 1 by two symbolically represented coupling formations 118 a, the second bearing mating interface 120 is represented in FIG. 1 by two symbolically represented complementary coupling mating formations 120 a.The second mounting counter-interface 120 is arranged on the functional and also physical side 102 aof the second support device 102 facing the machine frame 12, and the power supply device counter-interface 116 is arranged on the opposite functional and physical side 102 bof the second support device 102 facing away from the machine frame 12.Thus, the floor processing machine 10 can be constructed in modular fashion with regard to its supply with working energy or working power and can be adapted to the respective customer requirements or boundary conditions of the application.FIG. 2 shows further components of the production kit 8. Basically functionally identical arrangements, devices, interfaces and formations as in FIG. 1, which are designed differently from those of FIG. 1, are provided with the same but apostrophic reference numerals in FIG. 2. For their explanation, reference is expressly made to the description of FIG. 1 already given with reference to the respective reference numerals, unless expressly supplementary details are given.In FIG. 2, the lower left-hand side of that section with the storage interfaces 62 and 118 of the fuselage soil working machine 11 is shown. There, a second signal interface 122 for possible signal- and data-transmitting connection of the energy supply arrangement 98, also as embodiment 98' or 98", to the control device 38 and a third signal interface 124 for possible signal- and data-transmitting connection of the transmission arrangement 76, also as embodiment 76', to the control device 38 are also shown. The respective energy supply arrangement 98 to be connected, optionally as configuration 98' or 98", then has a corresponding second signal mating interface 112 and the respective transmission arrangement 76 to be connected, optionally as configuration 76', has a corresponding third signal mating interface 126.Thus, in contrast to the transmission arrangement 76 of FIG. 1, another transmission arrangement 76', again as a pump distributor transmission 70', is not fixed to the first support device 60 and also not to its own third support device, but rather is mounted directly on the machine frame 12 via corresponding transmission device bearing formations 74a' and abutment formations 72a'.The pulley 82 on the output side of the pump transfer case 70' is unchanged, since the pulley 84 as the working energy interface of the soil working machine is also unchanged. However, the pump transfer case 70' in FIG. 2 has a total of four mechanical power take-offs, each with a hydraulic pump 86' driven thereby, each of which has a fluidic quick-coupling formation 88 for the discharge of hydraulic fluid under elevated pressure. Of the four hydraulic pumps 86' of the pump distribution gear 70', only the two right-hand ones are provided with reference numerals for the sake of better clarity.By using four hydraulic pumps 86', there may be the use of a local control device 128 for controlling the pump distribution transmission 70' or, generally, the transmission arrangement 76', which can be coupled to the third signal interface 124 by a third signal counter-interface 126.In FIG. 2, an alternative power arrangement 56' is also shown with an electric motor 58' as the power device. The output shaft 78' as the working energy counter-interface of the power arrangement 56' of the electric motor 58' is connectable to the input hub 80' of the pump transfer case 70' in a torque-transmitting manner.As an electrical force arrangement 56', the alternative force arrangement 56', unlike the first force arrangement 56 with the internal combustion engine 58, requires operating energy in electrical energy form. For this purpose, an alternative energy supply arrangement 98' is provided, which has an accumulator 130 as energy store. Accordingly, the operating power interface 96' and the operating power mating interface 108' are configured as quick-connect electrical components, such as a plug and socket. Electrical cables therefore connect the electric motor 58' and its power supply, the accumulator 130.In contrast to FIG. 1, the energy supply arrangement 98' can be connected to the machine frame 12 not directly on the machine frame 12 via the second carrying device 102' but indirectly via the first carrying device 60'. The first support device 60' is then also a power supply switching device. In this case, the bearing counter-interface 64 is in function first and second bearing counter-interface 64 and comprises not only the coupling counter-formations 64a but also coupling counter-formations 64a'. The coupling counter formations 120a' of the second bearing counter interface are arranged on the second support device 102'. When the power arrangement 56' and the power supply arrangement 98' are pre-assembled to form a functional module, the coupling formations 62 aand 118 aon the fuselage soil working machine 11 form a common mounting interface of the functional module, which is both a first and a second mounting interface.The coupling counterformations 64 aand the coupling counterformations 120 aare illustrated in the figures merely by way of example with different shapes in order to graphically support their distinguishability. In fact, the coupling counter formations 64 aand the coupling counter formations 120 acan be formed with an identical shape, which is even preferred with regard to the production outlay. The described possible uniformity of shape applies equally to the coupling formations 62a and the coupling formations 118a and to at least two abutment formations consisting of the force device abutment formations 66a, the transmission device abutment formations 72a' and the energy supply device abutment formations 116a and to at least two bearing formations consisting of the force device bearing formations 68a, the transmission device bearing formations 74a' and the energy supply device bearing formations 114a.Instead of the energy supply arrangement 98' with the electrical accumulator 130, a module of an energy supply arrangement 98" with a fuel cell 132 and an operating medium tank 100" connected thereto can be used for conversion into electrical energy in the fuel cell 132. A control device 113 controlling the operation of the fuel cell 132 is connectable by the second signal counter interface 112' to the control device 38 on the fuselage soil working machine 11. Such a power supply arrangement 98" can also be prepared on a second support device 102' for arrangement on the fuselage soil working machine 11. The second support device 102', like that of the energy supply arrangement 98', can be mounted indirectly via the first support device 60' or directly on the machine frame via a second mounting interface.Likewise, the energy supply arrangement 98''' with a cable drum 134 arranged thereon with a line arrangement 136 for connection to a construction site-side power supply can be used as a module prepared on the floor processing machine 10 as an energy supply arrangement.Thus, due to the different arrangements present in the production set 8, the soil working machine 10 can be equipped with different engines and with different energy supply arrangements for supplying operating energy as well as with different transmission arrangements with relatively little outlay and can be configured for different field conditions.The example of different modules given above is exemplary only and not exhaustive.Referring now to Fig. 3, there is shown a second embodiment of a hull soil conditioning machine constructed in accordance with the principles of the present invention and designated 1011. Also shown is a second embodiment of the kit designed in accordance with the principles of the present invention and designated 1008. The placement of one of the various power supply assemblies 1098', 1098", or 1098"' illustrated at the second storage interface 1118 completes the fuselage soil conditioning machine and produces a second embodiment of a self-propelled soil conditioning machine.Arrangements, devices, components and component sections that are the same and have the same function as in FIGS. 1 and 2 relating to the corresponding first embodiments are provided with the same reference numerals in FIG. 3, but increased by the number 1000.The second embodiments of the floor processing machine or fuselage floor processing machine 1011 and production set 1008 will be described below only insofar as they differ from the corresponding first embodiments of FIGS. 1 and 2, the description of which also applies to the explanation of FIG. 3, unless otherwise stated below. Reference is therefore also expressly made to the description of FIGS. 1 and 2 for the explanation of FIG. 3.The essential difference between the fuselage soil-working machine 11 of the first embodiment and the fuselage soil-working machine 1011 is that the power arrangement 1056' with the electric motor 1058' as power device, as well as the transmission arrangement 1076' in the exemplary form of the pump distributor transmission 1070', is directly fixedly connected to the machine frame 1012 via corresponding bearing and abutment formations. The power arrangement 1056' and the transmission arrangement 1076' are thus part of the fuselage soil-working machine 1011.The energy supply arrangements 1098', 1098" and 1098"' alone can be connected, preferably releasably, to the fuselage soil working machine 1011 via a second mounting interface 1118 and a second mounting counter-interface 1120, which preferably fits complementarily thereto, of a second supporting device 1102 or 1102'.Since the second support device 1102 or 1102' is coupled to the machine frame 1012 or the machine body 1014 via the second support interface 1118 and the second support mating interface 1120, all the second support devices 1102 or 1102' of FIG. 3 have the same second support mating interface 1120. The single second support device 1102' in FIG. 3 is apostrophic because it has a different power supply device mating interface 1116' compared to the other second support devices 1102, which is intended to illustrate, however, only by way of example that a second support device can have any suitable power supply device mating interface on its functional side assigned to the power supply device.FIG. 3 shows only one force device 1058,'. In fact, a plurality of partial power devices can be arranged on the fuselage soil working machine 1011, which can be supplied with electrical energy by an energy supply arrangement 1098' or 1098" or 1098"' accommodated at a second mounting interface 1118.Thus, a soil working machine can be equipped individually as required with the respectively most suitable energy supply arrangement.References included in the specificationThis list of documents cited by the applicant has been produced in an automated manner and is only included for the better information of the reader. The list is not part of the German patent application or utility model application. The DPMA does not take any adhesion for any faults or omissions.Patent Literature citedDE 10 2021 129 619 A1

[0003] DE 10 2014 011 195 A1

[0003]

Claims

Self-propelled soil-working machine (10) comprising a fuselage soil-working machine (11), wherein the fuselage soil-working machine (11) has: - a machine frame (12), - a travel drive (28) as a first consumer of the soil-working machine (10), - a chassis (26) having a plurality of running gears (20, 22) which can roll on a base (U) and which carries the machine frame (12) standing on the base (U), wherein at least one running gear (20, 22) can be driven by the travel drive (28), - a working device (42) as a second consumer of the soil-working machine (10), wherein the working device (42) has a working tool (44) designed for soil working, - an operating stand (34) as the working station of a machine operator operating the soil-working machine (10), and - a control device (38) for controlling an operation of the soil working machine (10), wherein the fuselage soil working machine (11) is designed to receive a force arrangement (56; 56'), wherein the force arrangement (56; 56') comprises a force device (58; 58') which is designed to provide working energy for an operation of at least one of the consumers of the soil working machine (10), characterized in that the fuselage soil working machine (11) comprises: - a first mounting interface (62) for physically connecting the force arrangement (56; 56') to the fuselage soil working machine (11), - a first signal interface (92) for establishing a signal-transmitting first signal connection between the control device (38) and the force arrangement (56; 56'), and - at least one working energy interface (84) for establishing a working energy connection, which transmits working energy, between the at least one load and the force arrangement (56; 56'), wherein the force arrangement (56; 56') has a first supporting device (60; 60'), which is formed separately from the machine frame (12) and supports the force device (58; 58'), wherein the first supporting device (60; 60') has a first support counter-interface (64; 64') for physically connecting the force arrangement (56; 56') to the fuselage soil-working machine (11), and wherein the force device (58; 58') has a force device interface (68; 68'), wherein the first supporting device (60; 60') has one of the first support counter-interface (64; 64') has different force device counter-interfaces (66; 66'), and wherein the force device (58; 58') is held on the first support device (60; 60') by a connection of the force device interface (68; 68') and the force device counter-interface (66; 66').Self-propelled soil-working machine (10) according to claim 1, characterised in - that the first mounting interface (62) and the first mounting counter-interface (64; 64') are designed for direct connection to one another, or - that the first mounting interface (62) and the first mounting counter-interface (64; 64') are designed for indirect connection with the interposition of at least one force-imparting device, wherein the force-imparting device is different from the first support device (60; 60').Self-propelled soil-working machine (10) according to claim 1 or 2, characterised in that the force arrangement (56; 56') comprises a first signal mating interface (94) which is designed as part of the first signal connection for establishing a signal-transmitting signal coupling with the first signal interface (92).Self-propelled soil-working machine (10) according to one of the preceding claims, characterized in that the force arrangement (56; 56') comprises at least one working energy counter-interface (78; 78'), which is designed to establish the working energy connection transmitting working energy with the at least one working energy interface (84).Self-propelled soil-working machine (10) according to one of the preceding claims, characterized in that the power device (58; 58') has at least one energy converter machine (58; 58') which converts operating energy fed into it on the output side into operating energy, wherein the operating energy is a different energy form than the operating energy, wherein the soil-working machine (10) has an energy supply arrangement (98; 98'; 98"; 98"' for supplying the power device (58; 58') with operating energy.Self-propelled soil-working machine (10) according to claim 5, characterised in that the energy supply arrangement (98; 98'; 98"; 98"') has: - an energy supply device (100; 130; 132, 100"; 136), - a second support device (102; 102') formed separately from the machine frame (12), wherein the second support device (102; 102') supports the energy supply device (100; 130; 132, 100"; 136), and - an operating energy counter-interface (108; 108') which is formed for producing an operating energy-transmitting operating energy coupling with an operating energy interface (96; 96'), wherein the second support device (102; 102') comprises: - a second bearing counter-interface (120) which is formed for physically fixing the second support device (102; 102') is formed on a second mounting interface (118; 118'), wherein the second mounting interface (118; 118') and the second mounting counter-interface (120) are considered to be connected directly to one another, - the second mounting interface (118; 118') and the second mounting counter-interface (120) are formed for direct connection to one another, or - the second mounting interface (118; 118') and the second mounting counter-interface (120) are formed for indirect connection with at least one energy supply switching device (60') being arranged in between, wherein the energy supply switching device (60') is different from the second support device (102; 102'), and wherein the operating energy interface (96; 96') is formed for establishing an operating energy-transmitting operating energy connection between the energy supply device (100; 130; 132, 100"; 136) and the force device (58; 58') and is arranged on the force arrangement (56; 56').Self-propelled soil-working machine (10) according to claim 5 or 6, characterised in that the power device (58; 58') has, as the energy conversion machine (58; 58'), an internal combustion engine (58) and / or an electric motor (58') and / or a hydraulic motor.Self-propelled soil working machine (10) according to one of claims 5 to 7, characterised in that the energy supply device (100; 130; 132, 100"; 136) has at least one device from: - a tank (100) for storing fluid fuel, - an internal combustion engine, the output shaft of which is coupled to the input shaft of a generator, - an internal combustion engine, the output shaft of which is coupled to the input shaft of a fluid pump, - an electric motor, the output shaft of which is coupled to the input shaft of a fluid pump, - an electrical energy store (130), - a photovoltaic arrangement, - a fuel cell arrangement (132), - an electrical line arrangement (136) for connection to an external power source.Self-propelled soil-working machine (10) according to one of the preceding claims, characterized in that the soil-working machine (10) has a transmission arrangement (76; 76'), wherein the transmission arrangement (76; 76') is designed to produce at least one section of the working energy connection, wherein the transmission arrangement (76; 76') has at least one mechanical output, wherein a mechanical output of the at least one mechanical output is mechanically connected or connectable to the working device (42) or / and wherein at least one mechanical output of the at least one mechanical output is connected to an energy converter (86; 86') for converting mechanical energy into another energy form, wherein energy of the energy form converted by the energy converter (86; 86') can be transmitted as working energy by a transmission energy connection as part of the working energy connection to the at least one consumer.Self-propelled soil working machine (10) according to claim 9, including claim 4, characterised in that the power device (58; 58') outputs mechanical energy, wherein the working energy counter-interface (78; 78') has an output shaft (78; 78') or output hub for this purpose, wherein the transmission arrangement (76; 76') has an input shaft or input hub (80; 80') designed for connection to the working energy counter-interface (78; 78').Self-propelled soil-working machine (10) according to claim 9 or 10, characterised in that the energy converter (86; 86') is a generator and / or a fluid pump (86; 86').Self-propelled soil working machine (10) according to one of the preceding claims, characterized in that the at least one working energy interface (84) comprises a mechanical first working energy interface (84) and / or a hydraulic second working energy interface (88) and / or an electrical third working energy interface and / or a pneumatic fourth working energy interface.Self-propelled soil working machine (10) according to one of claims 9 to 12, including claims 4 and 9, characterised in that the transmission arrangement (76; 76') has a transmission device (70; 70'), wherein the transmission device (70; 70') comprises: - an input-side coupling formation (80, 80') for coupling to the working energy counter-interface (78; 78') transmitting working energy, and - at least one output-side coupling formation (82) for coupling to the at least one working energy interface (84) transmitting working energy.Self-propelled soil-working machine (10) according to claim 13, characterised in that the transmission arrangement (76; 76') comprises a third support device (60) which supports the transmission device, wherein the third support device (60) comprises: - a third support mating interface (64) which is designed for physically connecting the third support device (60) to a third support interface (62), wherein the third support interface (62) and the third support mating interface (64) are considered to be connected directly to one another, - the third support interface (62) and the third support mating interface (64) are designed for direct connection to one another, or - the third support interface (62) and the third support mating interface (64) are designed for indirect connection with at least one transmission switching device being arranged in between, wherein the transmission switching device is different from the third support device (60).A kit (8) for a self-propelled soil working machine (10) according to any one of the preceding claims, characterized in that the kit (8) comprises a fuselage soil working machine (11) according to the preamble of claim 1 with the first mounting interface (62), the first signal interface (92) and the at least one working energy interface (84) as a machine base and that the kit (8) additionally comprises a plurality of force arrangements (56; 56'), the force devices (58; 58') of which provide working energy on the basis of different physical principles of action.

Images