Novel multifunctional cabin structure of carrier

Abstract

The invention provides a novel multifunctional cabin structure of a vehicle. The novel multifunctional cabin structure comprises an upper end frame, a lower end frame, a skin, a plurality of stringers, a middle frame, an explosive bolt box, a separation hinge support and a separation spring support. The upper end frame is fixedly connected with a satellite bracket and a fairing; the two ends of the stringers are fixedly connected with the upper end frame and the lower end frame respectively, the stringers are evenly arranged in the circumferential direction of the upper end frame at intervals, and the arranged stringers define a conical frame. The skin is fixedly connected to the conical frame defined by the stringers, and a conical space is defined by the interior of the skin. The middle frame is fixedly connected in an internal space surrounded by the skin; and the explosive bolt box, the separation hinge support and the separation spring support are fixedly connected with the upper end frame. The multi-functional vehicle not only has an instrument loading function, but also has a switching function, so that the multi-functional vehicle is multifunctional, the structure of the vehicle can be simplified, the weight of the upper stage can be reduced, the cost is reduced, and the carrying capacity is improved.

Description

Technical Field

[0001] The present application relates to the technical field of instrument cabins, and in particular to a novel multifunctional cabin structure for a carrier. Background Art

[0002] The instrument cabin, the "brain" of the launch vehicle, belongs to the upper stage structure of the launch vehicle. It is equipped with the control system, instruments and equipment of other systems, and the final stage correction system. The instrument cabin of traditional launch vehicles is often arranged at the front end of the rocket body, which is far away from the engine and has less vibration, which is beneficial to the instruments and equipment.

[0003] The traditional instrument cabin is generally connected to the fairing on top, and there is usually a transition frame between the two structures to support the separation of the fairing. Specifically, the top of the instrument cabin is connected to the bottom of the transition frame, and the transition frame has an explosive bolt box inside, which is connected to the fairing with explosive bolts. The outside of the transition frame is equipped with a separation hinge and a spring top seat, which are used to spring open the fairing and separate the half-cover. The advantage of this setting is that the upper and lower stages can be connected and separated in an orderly manner, and the structural reliability is high. However, the transition frame is generally a whole ring. In order to meet the strength requirements, the wall thickness is at least 5mm, which leads to a lot of redundant weight beyond the structural function, which greatly reduces the carrying capacity of the carrier and also increases the launch cost invisibly.

[0004] Therefore, the technical problem that urgently needs to be solved is: how to provide a new type of multifunctional cabin structure for the carrier, which not only has the function of loading instruments but also has the function of switching, so as to make it multifunctional, simplify the carrier structure, reduce the weight of the upper stage, reduce costs and improve the carrying capacity. Summary of the invention

[0005] The purpose of this application is to provide a new type of multifunctional cabin structure for a carrier, eliminating the adapter frame and integrating the adapter frame function into the instrument cabin. Through reasonable layout, the explosive bolt box, separation spring and separation assembly are all installed on the upper end frame, so that the multifunctional cabin structure not only has the function of loading instruments but also has the function of transfer, making it multifunctional, which can not only simplify the carrier structure, but also reduce the weight of the upper stage, reduce costs, and improve the carrying capacity.

[0006] To achieve the above-mentioned purpose, the present application provides a new type of multifunctional cabin structure of a carrier, which includes: an upper end frame, a lower end frame, a skin, a plurality of stringers, an intermediate frame, an explosive bolt box, a separation hinge support and a separation spring support; the upper end frame is fixedly connected to the satellite bracket and the fairing; the two ends of the plurality of stringers are respectively fixedly connected to the upper end frame and the lower end frame, and the plurality of stringers are evenly spaced and arranged along the circumferential direction of the upper end frame, and the arranged stringers form a conical frame; the skin is fixedly connected to the conical frame formed by the stringers, and the interior of the skin is surrounded by a conical space; the intermediate frame is fixedly connected in the internal space surrounded by the skin; the explosive bolt box, the separation hinge support and the separation spring support are all fixedly connected to the upper end frame.

[0007] In the novel vehicle multifunctional cabin structure as described above, an instrument mounting plate is fixedly connected to the middle frame, and the instrument mounting plate is located in a conical space surrounded by the inner part of the skin.

[0008] In the novel carrier multifunctional cabin structure as described above, the upper end frame has a circle of ring holes, and the ring holes are provided with fixing parts for connecting the upper end frame with the satellite bracket.

[0009] As described above, in the novel carrier multifunctional cabin structure, the upper end frame has a circle of explosive bolt box holes, and the explosive bolt box holes are equipped with fixings for connecting the upper end frame with the fairing.

[0010] As described above, in the novel carrier multifunctional cabin structure, the instrument mounting plate is fan-shaped; a plurality of fan-shaped instrument mounting plates are spliced ​​together to form a circular ring structure; and the circular ring structure is parallel to the upper end frame.

[0011] As described above, in the novel carrier multifunctional cabin structure, the explosive bolt box is used to install explosive bolts, the side surface of the explosive bolt box is fixedly connected to the arrow wall of the cabin body, and the top surface is fixedly connected to the upper end frame.

[0012] As described above, in the novel carrier multifunctional cabin structure, the separation hinge support is used to install the separation latch, the side surface of the separation hinge support is fixedly connected to the cabin arrow wall, and the top surface is fixedly connected to the upper end frame.

[0013] As described above, in the novel carrier multifunctional cabin structure, the separation hinge lug of the fairing is connected to the separation latch, which plays the role of rotational support for the separation of the fairing.

[0014] As described above, the new type of carrier multifunctional cabin structure, wherein the separation spring support is used to fix the separation springs on both sides of the fairing, the side surface of the separation spring support is fixedly connected to the arrow wall of the cabin body, and the top surface is fixedly connected to the upper end frame.

[0015] As described above, in the novel carrier multifunctional cabin structure, the upper end frame and the lower end frame are both in annular shape, and the maximum diameter of the lower end frame is smaller than the maximum diameter of the upper end frame.

[0016] The beneficial effects achieved by this application are as follows:

[0017] (1) Under the premise of meeting the strength design requirements, the present application not only has the loading function of the instrument cabin, but also is equipped with an upper end frame for internally transferring the satellite bracket, and externally connecting the explosive bolt box and the separation assembly, making it multifunctional.

[0018] (2) The explosive bolt box and separation assembly of the present application are reasonably arranged, which can not only simplify the carrier structure, but also reduce the weight of the upper stage, reduce costs, and improve the carrying capacity. BRIEF DESCRIPTION OF THE DRAWINGS

[0019] In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the drawings required for use in the embodiments or the description of the prior art will be briefly introduced below. Obviously, the drawings described below are only some embodiments recorded in the present application. For those skilled in the art, other drawings can also be obtained based on these drawings.

[0020] Figure 1 This is a schematic structural diagram of a new type of carrier multifunctional cabin structure according to an embodiment of the present application.

[0021] Figure 2 This is a schematic diagram of the upper frame structure of an embodiment of the present application.

[0022] Figure 3 It is a schematic structural diagram of a separate hinge support according to an embodiment of the present application.

[0023] Figure 4 It is a schematic structural diagram of a separation spring support according to an embodiment of the present application.

[0024] Figure 5 This is a schematic structural diagram of an explosive bolt box according to an embodiment of the present application.

[0025] Figure markings: 1-upper end frame; 2-skin; 3-beam; 4-middle frame; 5-instrument mounting plate; 6-explosive bolt box; 7-separation hinge support; 8-separation spring support; 9-lower end frame; 11-ring hole; 12-explosive bolt box hole; 61-top connecting hole of explosive bolt box; 62-side connecting hole of explosive bolt box; 71-side connecting hole of separation hinge support; 72-top connecting hole of separation hinge support; 73-pin connecting hole; 81-side connecting hole of separation spring support; 82-top connecting hole of separation spring support. DETAILED DESCRIPTION

[0026] The following is a clear and complete description of the technical solutions in the embodiments of the present application in conjunction with the drawings in the embodiments of the present application. Obviously, the described embodiments are part of the embodiments of the present application, not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those skilled in the art without creative work are within the scope of protection of the present application.

[0027] like Figure 1 As shown, the present application provides a novel multifunctional cabin structure of a carrier, which includes: an upper end frame 1, a lower end frame 9, a skin 2, a plurality of stringers 3, an intermediate frame 4, an explosive bolt box 6, a separation hinge support 7 and a separation spring support 8; the upper end frame 1 is fixedly connected to the satellite bracket and the fairing; the two ends of the plurality of stringers 3 are fixedly connected to the upper end frame 1 and the lower end frame 9 respectively, and the plurality of stringers 3 are evenly spaced and arranged along the circumferential direction of the upper end frame 1, and the arranged stringers 3 form a conical frame; the skin 2 is fixedly connected to the conical frame formed by the stringers 3, and the interior of the skin 2 is surrounded by a conical space; the intermediate frame 4 is fixedly connected in the internal space surrounded by the skin 2; the explosive bolt box 6, the separation hinge support 7 and the separation spring support 8 are all fixedly connected to the upper end frame 1.

[0028] like Figure 1 As shown, an instrument mounting plate 5 is fixedly connected to the middle frame 4 , and the instrument mounting plate 5 is located in a conical space surrounded by the inner part of the skin 2 .

[0029] like Figure 2 As shown, the upper end frame 1 is annular and has an outward-turned frame structure. The upper end frame 1 has a circle of ring holes 11, and the ring holes 11 are installed with fixings for connecting the upper end frame 1 with the satellite bracket. The upper end frame 1 has a circle of explosive bolt box holes 12, and the explosive bolt box holes 12 are installed with fixings for connecting the upper end frame 1 with the fairing.

[0030] As a specific embodiment of the present invention, the ring hole 11 and the explosive bolt box hole 12 are both located on the top surface of the upper end frame 1, and the ring hole 11 and the explosive bolt box hole 12 are evenly spaced apart along the circumferential direction of the upper end frame 1, and the ring hole 11 is located on the inner side of the explosive bolt box hole 12.

[0031] As a specific embodiment of the present invention, the skin 2 adopts a flat plate structure of equal thickness, and the skin 2 can be wrapped into a cylindrical hollow structure. The skin 2 of the present invention is fixedly riveted between the upper end frame 1 and the lower end frame 9 through multiple girders 3. The role of the skin 2 is to maintain the shape, transmit shear force, install instrument cables, etc.

[0032] As a specific embodiment of the present invention, the cross-sectional shape of the stringer 3 is Y-shaped, which improves the structural stability and reliability of the stringer 3. The stringer 3 is connected between the upper end frame 1 and the lower end frame 9 by fixing connectors such as bolts or rivets, and is fixedly connected to the skin 2. The function of the stringer 3 is to realize longitudinal bearing between the upper end frame 1 and the lower end frame 9, and improve the stability and reliability of the connection structure between the upper end frame 1 and the lower end frame 9.

[0033] As a specific embodiment of the present invention, the instrument installation plate 5 is fan-shaped; multiple fan-shaped instrument installation plates are spliced ​​together to form a ring structure; the ring structure is parallel to the upper end frame 1. The instrument installation plate 5 is used to install instruments and equipment. Preferably, the instrument installation plate 5 is made of composite materials, and specifically, the instrument installation plate 5 is a sandwich structure of a carbon panel and a honeycomb core, which improves the reliability of the instrument installation plate 5 to install instruments and equipment.

[0034] As a specific embodiment of the present invention, the middle frame 4 is in a circular ring shape as a whole, and the cross-sectional shape of the middle frame 4 is an omega shape. The middle frame 4 is arranged parallel to the upper end frame 1 and the lower end frame 9. Preferably, the center points of the middle frame 4, the upper end frame 1 and the lower end frame 9 are in a straight line direction.

[0035] As a specific embodiment of the present invention, the middle frame 4 includes a plurality of middle frames 4, and the plurality of middle frames 4 are fixedly connected to the inner side of the skin 2 at equal intervals. The fixing connection method between the middle frame 4 and the skin 2 is riveting, which is not limited here. The fixing connection method between the middle frame 4 and the skin 2 is only a preferred method, and other fixing methods can also be used. The function of the middle frame 4 is to provide intermediate support as a longitudinal structural member, that is, lateral support.

[0036] like Figure 1 As shown, the explosive bolt box 6 is used to install explosive bolts, the side surface of the explosive bolt box 6 is fixedly connected to the arrow wall of the cabin, and the top surface is fixedly connected to the upper end frame 1.

[0037] like Figure 5 As shown, the side of the explosive bolt box 6 has an explosive bolt box side connecting hole 62, which is used to be fixedly connected to the arrow wall of the cabin, and the top surface has an explosive bolt box top connecting hole 61, which is used to be fixedly connected to the upper end frame 1.

[0038] like Figure 1 As shown, the separation hinge support 7 is used to install the separation pin, the side surface of the separation hinge support 7 is fixedly connected to the arrow wall of the cabin, and the top surface is fixedly connected to the upper end frame 1.

[0039] like Figure 3As shown, the separation hinge support 7 has a separation hinge support side connection hole 71, a separation hinge support top connection hole 72 and a latch connection hole 73. The separation hinge support side connection hole 71 is used for fixed connection with the arrow wall of the cabin, the separation hinge support top connection hole 72 is used for fixed connection with the upper end frame 1, and the latch connection hole 73 is used for installing a separation latch.

[0040] As a specific embodiment of the present invention, the separation hinge lug of the fairing is connected to the separation latch, which plays a role of rotation support for the separation of the fairing.

[0041] As a specific embodiment of the present invention, the separation spring support 8 is used to fix the separation springs on both sides of the fairing. When the separation springs are separated, the separation spring support 8 plays a supporting role of the reaction force. The side surface of the separation spring support 8 is fixedly connected to the arrow wall of the cabin, and the top surface is fixedly connected to the upper end frame 1.

[0042] like Figure 4 As shown, the separation spring support 8 has a separation spring support side connection hole 81 and a separation spring support top connection hole 82; the separation spring support side connection hole 81 is used for fixed connection with the arrow wall of the cabin body, and the separation spring support top connection hole 82 is used for fixed connection with the upper end frame 1.

[0043] It should be explained that the separation hinge support 7 and the separation spring support 8 belong to the separation components. The explosive bolt box 6, the separation hinge support 7 and the separation spring support 8 each include a plurality of them, and the explosive bolt box 6, the separation hinge support 7 and the separation spring support 8 are spaced apart from each other, and the layout is reasonable, and they do not affect each other.

[0044] As a specific embodiment of the present invention, the upper end frame 1 and the lower end frame 9 are both annular, the maximum diameter of the lower end frame 9 is smaller than the maximum diameter of the upper end frame 1, the skin 2 is connected between the upper end frame 1 and the lower end frame 9 to form a conical structure, and a conical space is formed inside the skin 2, and the conical space is used to install instruments and equipment.

[0045] The method of using the multifunctional cabin of a novel carrier of the present invention is as follows:

[0046] Install the instruments and equipment etc. to the fixed position of the instrument mounting plate 5;

[0047] Connect the satellite bracket to the ring hole 11 of the upper end frame 1;

[0048] The fairing is connected to the explosion bolt box hole 12 of the upper end frame 1.

[0049] The present application discloses a novel multifunctional cabin of a carrier, which not only has the function of loading various instruments and equipment into the instrument cabin, but also can install satellite brackets and fairings.

[0050] The beneficial effects achieved by this application are as follows:

[0051] (1) Under the premise of meeting the strength design requirements, the present application not only has the loading function of the instrument cabin, but also is equipped with an upper end frame for internally transferring the satellite bracket, and externally connecting the explosive bolt box and the separation assembly, making it multifunctional.

[0052] (2) The explosive bolt box and separation assembly of the present application are reasonably arranged, which can not only simplify the carrier structure, but also reduce the weight of the upper stage, reduce costs, and improve the carrying capacity.

[0053] In the description of this application, the terms "first" and "second" are used for descriptive purposes only and should not be understood as indicating or implying relative importance or implicitly indicating the number of technical features indicated. Thus, a feature defined as "first" or "second" may explicitly or implicitly include one or more of the features. In the description of this application, "plurality" means two or more, unless otherwise clearly and specifically defined.

[0054] In the description of the present application, the word "for example" is used to mean "used as an example, illustration or explanation". Any embodiment described as "for example" in the present application is not necessarily to be construed as being more preferred or advantageous than other embodiments. The following description is given to enable any technician in the field to implement and use the present invention. In the following description, details are listed for the purpose of explanation. It should be understood that a person of ordinary skill in the art can recognize that the present invention can be implemented without using these specific details. In other examples, well-known structures and processes will not be elaborated in detail to avoid obscuring the description of the present invention with unnecessary details. Therefore, the present invention is not intended to be limited to the embodiments shown, but is consistent with the widest scope consistent with the principles and features disclosed in the present application.

[0055] The above description is only an embodiment of the present invention and is not intended to limit the present invention. For those skilled in the art, the present invention may have various modifications and variations. Any modification, equivalent substitution, improvement, etc. made within the spirit and principle of the present invention should be included in the scope of the claims of the present invention.

Claims

1. A new type of multifunctional cabin structure for a carrier, characterized in that: The structure includes: an upper end frame, a lower end frame, a skin, a plurality of stringers, an intermediate frame, an explosive bolt box, a separation hinge support and a separation spring support; The upper end frame is fixedly connected to the satellite bracket and the fairing; Two ends of the plurality of beams are fixedly connected to the upper end frame and the lower end frame respectively, and the plurality of beams are evenly spaced and arranged along the circumferential direction of the upper end frame, and the beams are arranged to form a conical frame; The skin is fixedly connected to the frame formed by the trusses in a cone shape, and the interior of the skin surrounds a cone-shaped space; The middle frame is fixedly connected in the inner space surrounded by the skin; The explosive bolt box, the separation hinge support and the separation spring support are all fixedly connected to the upper end frame.

2. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: An instrument mounting plate is fixedly connected to the middle frame, and the instrument mounting plate is located in a conical space surrounded by the inner part of the skin.

3. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: The upper end frame has a circle of ring holes. The annular hole mounting fixture is used to connect the upper end frame with the satellite bracket.

4. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: The upper end frame has a circle of explosive bolt box holes. The explosive bolt box hole is provided with a fixing piece, which is used for connecting the upper end frame with the fairing.

5. The novel multifunctional cabin structure of a carrier according to claim 2 is characterized in that: The instrument mounting plate is fan-shaped; Multiple fan-shaped instrument installation plates are spliced ​​together to form a ring structure; The circular ring structure is parallel to the upper end frame.

6. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: The explosive bolt box is used for installing explosive bolts, the side surface of the explosive bolt box is fixedly connected to the arrow wall of the cabin, and the top surface is fixedly connected to the upper end frame.

7. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: The separation hinge support is used to install the separation latch, the side surface of the separation hinge support is fixedly connected to the arrow wall of the cabin, and the top surface is fixedly connected to the upper end frame.

8. The novel multifunctional cabin structure of a carrier according to claim 7 is characterized in that: The separation hinge lug of the fairing is connected to the separation latch to provide rotational support for the separation of the fairing.

9. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: The separation spring support is used to fix the separation springs on both sides of the fairing. The side surface of the separation spring support is fixedly connected to the arrow wall of the cabin, and the top surface is fixedly connected to the upper end frame.

10. The novel multifunctional cabin structure of a carrier according to claim 1 is characterized in that: The upper end frame and the lower end frame are both in annular shape, and the maximum diameter of the lower end frame is smaller than the maximum diameter of the upper end frame.

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