SYSTEM FOR MOUNTING A COMPONENT ON A VEHICLE

Abstract

An embodiment of a system is presented that can be attached to the exterior fairing of a vehicle, e.g., an aircraft. The disclosed system comprises: an antenna, a carrier housing coupled to the antenna, the carrier housing having an upper section configured to receive and hold the antenna, and a lower section opposite the upper section, and a mounting base. The mounting base comprises: a frame with a support platform configured and arranged to connect to the lower section of the carrier housing, a lower section opposite the frame, the lower section being configured and arranged to connect to the exterior fairing of the vehicle, and a passage with an opening in the lower section.The passage extends from the lower section towards the frame and is configured and arranged to accommodate a structural feature of the vehicle that extends from the outer wall of the vehicle.

Description

CROSS-REFERENCE TO A RELATED REGISTRATION

[0001] This application claims priority over preliminary US patent application No. 63 / 653,073, which was filed on May 29, 2024. TECHNICAL AREA

[0002] The embodiments of the object described here generally relate to vehicle components. In particular, embodiments of the object relate to a mounting system or assembly for an aircraft component, e.g., a communications antenna. BACKGROUND

[0003] Vehicles such as aircraft, automobiles, and watercraft often incorporate components attached to or integrated into external walls, features, or structures. For example, cameras, spoilers, antennas, sensors, and similar items may be mounted on the exterior of cars. Similarly, aircraft may use fuselage-mounted instruments, lighting fixtures, communication equipment, antennas, and other components. Mounting such components can be challenging and often requires balancing various factors, including weight, cost, structural integrity, aesthetics, and aerodynamic performance.

[0004] Accordingly, it is desirable to have a mounting system for a component that is to be attached to or integrated into the exterior of a vehicle. Additionally, it is desirable to have a component fastening system that is robust, secure, and aerodynamic. Further desirable features and characteristics will become apparent from the following detailed description and the accompanying claims in conjunction with the accompanying drawings and the preceding technical field and background information. BRIEF SUMMARY

[0005] A system for attaching a component to the outer wall of a vehicle is presented here. One embodiment of the system comprises: a support housing with an upper section configured to receive and hold the component, and a lower section opposite the upper section; and a mounting base. The mounting base comprises: a frame with a support platform configured and arranged to connect to the lower section of the support housing; a lower section opposite the frame, the lower section being configured and arranged to connect to the outer wall of the vehicle; and a passage with an opening in the lower section.The passage extends from the lower section towards the frame, and the passage is configured and arranged to accommodate a structural feature of the vehicle that extends from the outer wall of the vehicle.

[0006] Another embodiment of the system comprises: an antenna component; a carrier housing coupled to the antenna component, the carrier housing having an upper section configured to receive and hold the antenna component, and a lower section opposite the upper section; and a mounting base. The mounting base comprises: a frame with a support platform configured and arranged to connect to the lower section of the carrier housing; a lower section opposite the frame, the lower section being configured and arranged to connect to the outer wall of the vehicle; and a passage with an opening in the lower section.The passage extends from the lower section towards the frame, the passage being configured and arranged to accommodate a structural feature of the vehicle that extends from the outer wall of the vehicle.

[0007] Furthermore, a vehicle, e.g. an aircraft, is presented here that has a system for attaching a component to an outer wall of the vehicle.

[0008] This summary serves to present, in simplified form, a selection of concepts that are described in detail below. This summary is not intended to identify key features or essential characteristics of the claimed subject matter, nor is it intended to assist in determining the scope of the claimed subject matter. BRIEF DESCRIPTION OF THE DRAWINGS

[0009] A more complete understanding of the subject matter will result from the detailed description and claims when considered in conjunction with the following figures, where identical reference numbers refer to similar elements in the figures. Fig. Figure 1 is a perspective top view of an aircraft with a component mounted on it using a mounting system configured in accordance with certain embodiments of the invention; Fig. Figure 2 is a perspective view from above showing a section of an aircraft fuselage with an antenna and an associated mounting system attached to it, in accordance with certain embodiments of the invention; Fig. 3 is a perspective view from top to back, showing the in Fig. The antenna and mounting system shown in section 2 are also shown; Fig. 4 is a top view showing the Fig. The antenna and mounting system shown in Figure 2 are depicted; Fig. 5 is a left side view, showing the Fig. The antenna and mounting system shown in Figure 2 are depicted; Fig. Figure 6 is a perspective top view of the area in Fig. 2 antennas shown; Fig. 7 is a perspective top view of an embodiment of a carrier housing for use with the in Fig. The fastening system shown in section 2 is suitable; Fig. 8 is a perspective view of the underside of the in Fig. 7 carrier housing shown; Fig. 9 is a top view of the in Fig. 7 carrier housings shown; Fig. 10 is a view of the underside of the in Fig. 7 carrier housing shown; Fig. Figure 11 is a top view of an embodiment of a holding frame for use with the in Fig. The fastening system shown in section 2 is suitable; Fig. Figure 12 is a perspective view from above of an embodiment of a mounting base for use with the in Fig. The mounting system shown in section 2 is suitable; Fig. 13 is a perspective view of the in Fig. 12 mounting bases shown from top to back; Fig. Figure 14 is a perspective view from below of the in Fig. 12 mounting bases shown; Fig. 15 is a top view of the in Fig. 12 mounting bases shown; Fig. 16 is a view from below of the in Fig. 12 mounting bases shown; Fig. 17 is a front view of the in Fig. 12 mounting bases shown; Fig. Figure 18 is a perspective side view showing the inside of one half of the Fig. 12 shown mounting base; Fig. Figure 19 is a perspective view showing an exemplary arrangement of components and features (for assembly, installation and structural support) located under the fuselage skin of a host aircraft; Fig. Figures 20-26 are schematic top views showing the installation of an antenna and an associated mounting system configured according to the embodiments of the invention; Fig. Figure 27 is a perspective view from above of an alternative embodiment of a component assembly system; and Fig. 28 is a perspective exploded view of the in Fig. 27 shown fastening systems for components. DETAILED DESCRIPTION

[0010] The following detailed description is for illustrative purposes only and is not intended to limit the embodiments of the subject matter or the application and use of such embodiments. As used herein, the word "exemplary" means "to serve as an example, instance, or illustration." Any implementation described herein as exemplary is not necessarily to be understood as preferred or advantageous over other implementations. Furthermore, there is no intention to be bound by any express or implied theory set forth in the preceding technical field, background, brief summary, or the following detailed description.

[0011] The following description can refer to elements, nodes, or features that are "connected" or "coupled" to one another. Unless explicitly stated otherwise, "coupled" means that an element / node / feature is directly or indirectly connected to (or directly or indirectly interacts with) another element / node / feature, not necessarily mechanically. Similarly, unless explicitly stated otherwise, "connected" means that an element / node / component is directly connected to (or directly communicates with) another element / node / component, not necessarily mechanically.

[0012] Furthermore, certain terms in the following description may be used for reference purposes only and should therefore not be considered restrictive. For example, terms such as "top," "bottom," "above," and "below" refer to directions in the referenced drawings. Terms such as "front," "back," "side," "outside," and "inside" describe the orientation and / or location of parts of the component within a uniform but arbitrary frame of reference, which becomes clear by referring to the text and the associated drawings in which the component in question is described. This terminology may include the terms explicitly mentioned above, their derivatives, and terms of similar meaning. Similarly, the terms "first," "second," and other numerical terms relating to structures do not imply any order unless clearly evident from the context.

[0013] A fairing for a vehicle component and the associated installation and mounting system are presented here. According to certain non-limiting embodiments, the vehicle component and the associated mounting system are used on board an aircraft, such as an airplane. However, it should be noted that embodiments of the presented item may be used for other vehicle applications, including, but not limited to: trains, helicopters, automobiles, watercraft, submarines, monorails, amusement park rides, transportation systems, spacecraft, and the like. Although the exemplary application described here relates to the mounting of an antenna component, the presented item may also be used in conjunction with other types of vehicle-mounted components, e.g.,Cameras, instruments, sensors, lighting fixtures, aerodynamic features, structural elements, windows, solar panels and the like.

[0014] Certain embodiments of the disclosed product relate to a system for attaching a component to the outer wall of a vehicle. The disclosed system comprises an aerodynamic mounting base and associated assemblies for mounting an antenna component to the upper fuselage of an aircraft. According to certain embodiments, the disclosed product provides a solution for installing a flat satellite communications antenna on the upper fuselage skin of an aircraft. A flat antenna is attached and held in a support housing (serving as an adapter) resembling a picture frame, and the adapter is supported by a base assembly that can be implemented as a single component or as a combination of several components that are coupled together or otherwise interact in a desired configuration.Certain features and structures of the mounting system are shaped, dimensioned, and configured to provide resistance or protection against lightning strikes and bird strikes. The mounting system can be reinforced by a system of Dopplers, frames, intercostals, clips, and / or other components to respond to any stresses occurring on the antenna and mounting elements and to safely distribute these stresses across the aircraft structure.

[0015] Fig. Figure 1 is a perspective view of an aircraft 100 from above, showing an exemplary embodiment of a component mounting system 102 attached to an outer wall (e.g., a fuselage skin 104 or a section thereof) of the aircraft 100. The system 102 described here comprises an antenna mounted in a carrier housing, which in turn is attached to the aircraft 100 by a mounting base. Fig. Figure 2 is a perspective view from above, showing a section of the aircraft fuselage 106 with an antenna 108 and two main components of the system 102 (a carrier housing 110 and a mounting base 112). The exposed outer surface of the fuselage 106 corresponds to the fuselage skin 104. Fig. Figure 3 is a perspective view from above looking back, showing the antenna 108 and the mounting system 102. Fig. 4 is a top view and Fig. 5 is a view from the left side.

[0016] The illustrated embodiment of the mounting system 102 comprises two main components: the mounting base 112, which can be a single, one-piece component or an assembly of several physically distinct parts, and the carrier housing 110, which can also be a single, one-piece component or an assembly of several physically distinct parts. When the system 102 is deployed, the mounting base 112 is connected to the fuselage 106, the carrier housing 110 is connected to the mounting base 112, and the antenna 108 is connected to the carrier housing 110. Electrical cables, wires, conduits, and signal paths are routed between the antenna 108 and the required components, couplers, and / or subsystems of the host aircraft 100.

[0017] Referring to Fig. 2. The aircraft 100 contains a structural feature (e.g., a dorsal structure 116) that extends over the outer fuselage skin 104. The dorsal structure 116 is also in Fig. 20-25. As explained in more detail below, the mounting base 112 is suitably designed and manufactured to accommodate the back structure 116, which does not need to be modified, moved, or removed when the system 102 is attached to the aircraft 100. For example, the mounting base 112 may include or define a slot or passage 118 for the back structure 116 (see Fig. 3 and Fig. 4).

[0018] Fig. Figure 6 is a perspective top view of an exemplary embodiment of the antenna 108; Fig. Figures 7-10 are different views of an exemplary embodiment of the carrier housing 110; and Fig. Figure 11 is a top view of an embodiment of a retaining frame 119 suitable for use with the mounting system 102. Fig. Figures 12-18 are different views of an exemplary embodiment of the mounting base 112.

[0019] As previously mentioned, the described version of the Antenna 108 is a flat satellite communication antenna with a flat "tile" configuration. The Antenna 108's design incorporates various mounting holes, cutouts, and a specific shape. As shown in Fig. As shown in Figure 6, the antenna 108 has a main surface 120 and a circumferential edge 122, which corresponds to a side wall of the antenna 108. As explained in more detail below, the support housing 110 is shaped, dimensioned, and configured to surround the circumferential edge 122 of the antenna 108. The support housing 110 is coupled to the antenna 108 and holds the antenna 108 such that the main surface 120 is exposed when the system 102 is installed on the base aircraft 100. The system 102 can be positioned at a desirable location on the fuselage skin 104, which improves the electromagnetic performance of the antenna 108. In certain embodiments, the mounting base 112 can be designed and manufactured as a universal component of the system 102, while the carrier housing 110 can be designed, configured and manufactured for compatibility with the specific shape, size, dimensions and layout of the antenna 108.In this way, the same mounting base 112 can be used (and retained in its installed state) to mount different types of antennas or other components, as long as the carrier housing 110 can be redesigned or adapted while still being compatible with the universal mounting base 112.

[0020] The in Fig. The embodiment of the antenna 108 shown in Figure 6 comprises a plurality of mounting points 126 distributed around the outer circumference of the antenna 108. In this particular embodiment, the antenna 108 has twelve mounting points 126 – three on each side. Each mounting point 126 includes or interacts with a projection containing a mounting hole. Furthermore, each mounting point 126 can be defined by a cutout or recess such that an upper main surface of each mounting point 126 lies below an uppermost circumferential surface of the antenna 108. In this context, Figure 6 shows Fig. Six twelve recesses around the outer circumference of the antenna 108, the projections and mounting holes being arranged together with the projections. These structural features of the antenna 108 cooperate with the corresponding structural features of the support housing 110 and the mounting frame 119, as described below.

[0021] As from the Fig. As can be seen, the mounting housing 110 is appropriately configured to be compatible with the specific shape, size, and dimensions of the antenna 108 and to accommodate and hold the antenna 108 according to the desired installation scheme. The mounting housing 110 is made of a strong and durable material such as steel, aluminum, a composite material, plastic, or similar. The mounting housing 110 can be manufactured as a single, unified component or as an assembly consisting of any number of individual parts.

[0022] The illustrated embodiment of the carrier housing 110 is designed to receive and hold the antenna 108, which can be attached to compatible mounting features or structures of the carrier housing 110 by means of bolts, screws, fasteners, clips, or the like. The carrier housing 110 generally comprises, without limitation: an upper section 202; a lower section 204 opposite the upper section 202; a front section 206; a rear section 208 opposite the front section 206; a bottom section 210; a component cavity 212; an access opening 214 defined in the lower section 204; and webs 216 arranged to be compatible with the specific physical configuration of the antenna 108.

[0023] As in Fig. 7 and Fig. As shown in Figure 9, the upper section 202, the component cavity 212, and the webs 216 are shaped, dimensioned, and otherwise configured to receive and hold the antenna 108 in the desired position and orientation. The component cavity 212 is arranged in the upper section 202 such that the antenna 108 can be installed from the top of the support housing 110. According to the illustrated embodiment, the upper section 202 is configured to surround, enclose, or enclose the circumferential edge 122 of the antenna 108 after installation, and the support housing 110 holds the antenna 108 in place, so that the main surface 120 of the antenna 108 is substantially or completely exposed (see Figure 9). Fig. 2).

[0024] According to the in Fig. In the embodiment shown in Figure 6, the support housing 110 comprises a plurality of webs 216 that correspond to the mounting points 126 of the antenna 108. The support housing 110 has twelve webs 216 arranged in a 1:1 relationship to the twelve mounting points 126. Each web 216 has a threaded bore 220 (which in other embodiments may be a through bore) that can engage with a corresponding mounting bore of the antenna 108 and / or with a corresponding mounting bore of the support frame 119. When the antenna 108 is installed in the support housing 110, the undersides of the mounting points 126 align with and rest on the tops of the webs 216.

[0025] In accordance with certain embodiments, the support housing 110 comprises two cover plates 222. The cover plates 222 serve to cover cavities formed in the support housing 110 (the cavities are desirable to reduce the weight of the support housing 110, and the cover plates 222 are shaped and dimensioned to seal the cavities while simultaneously exhibiting a desired aerodynamic profile). In the illustrated embodiment, the cover plates 222 also serve to conceal fasteners used to attach the support housing 110 to the underlying mounting base 112.

[0026] The mounting frame 119 (see Fig. 11) is used to attach the antenna 108 to the carrier housing 110 and to create a smooth and aerodynamic surface for the system 102 used. In the Fig. The mounting frame 119 is shown in its installed state, where it occupies the space between the antenna 108 and the component cavity 212 of the carrier housing 110. The mounting frame 119 comprises a pattern of cutouts 302 and tabs 304 defined around its inner circumference (see Fig. 11) The illustrated embodiment has twelve tabs 304, corresponding to the twelve mounting points 126 of the antenna 108. A mounting hole 306 is defined in each tab 304; the twelve mounting holes 306 are arranged to align with the twelve corresponding mounting holes of the antenna 108 and with the twelve corresponding mounting holes 220 of the support housing 110. Accordingly, threaded fasteners can be screwed through the mounting holes 306 of the support frame 119, through the mounting holes of the antenna 108, and into the mounting holes 220 of the support housing 110 to secure the antenna 108 in place. In this context, the support frame 119 includes at least one connecting structure that overlaps an outer edge region of the antenna 108 to facilitate coupling with the antenna 108.When the antenna 108 is coupled to the carrier housing 110 in this way, the carrier housing 110 surrounds or encloses the circumferential edge 122 of the antenna 108.

[0027] Fig. Figures 12-17 are different views of the mounting base 112 itself, and Fig. Figure 18 is a perspective side view showing the inside of one half of the mounting base 112. The mounting base 112 serves as a "universal" component of the system 100, as it does not need to be modified, altered, or redesigned to accommodate the specific object to be mounted. Instead, the carrier housing 110 is adapted and configured to be compatible with the specific physical properties of the component to be mounted, while remaining compatible with the mounting base 112. The mounting base 112 is made of a strong and durable material such as steel, aluminum, a composite material, plastic, or similar. The mounting base 112 can be manufactured as a single component or as an assembly of any number of individual parts.According to the illustrated embodiment, the mounting base 112 is designed as an assembly comprising a left side part 402 and a right side part 404, which interacts with the left side part 402. In practice, each half of the mounting base 112 can be manufactured as a single, one-piece component or as an assembly of several parts, e.g., from a plurality of segments that are screwed, welded, or otherwise joined together to form one half of the mounting base 112. Although not always necessary, the left and right side parts 402, 404 are each designed as an assembly of three main segments that are joined together. The segmented design is desirable for reasons of ease of manufacture, assembly, and installation.

[0028] The illustrated embodiment of the mounting base 112 (e.g., the left and right side parts 402, 404 in combination) generally comprises, without limitation: an upper section 406; a lower section 408; a front section 410; a rear section 412; a frame 416; the passage 118; an upper opening 424; a lower access opening 428; and an interior 432. The mounting base 112 is generally designed as a hollow shell with large openings at the top and bottom. In this context, the left side component 402 represents the left side wall, part of the front side wall, and part of the rear side wall of the mounting base 112. Similarly, the right side component 404 represents the right side wall, another part of the front side wall, and another part of the rear side wall of the mounting base 112.

[0029] In the illustrated embodiment, the frame 416 forms the uppermost region of the upper section 406. The frame 416 includes a support platform 436, which is configured and arranged to be connected to, or interact with, the lower section 204 of the support housing 110. More precisely, the support platform 436 is shaped, dimensioned, and arranged to be compatible with the surface defined by the base region 210 of the support housing 110 (see Fig. 8 and Fig. 10, which show the underside of the support housing 110). The support platform 436 includes a series of mounting holes formed and arranged to accommodate a corresponding pattern of mounting holes formed in the base area 210 of the support housing 110. These cooperating mounting holes facilitate the installation of the support housing 110 over the mounting base 112.

[0030] The lower section 408 of the mounting base 112 is positioned relative to the upper section 406 and to the frame 416. The lower section 408 is configured and arranged to facilitate a secure connection to an outer wall of the aircraft fuselage 106, e.g., the fuselage skin 104. For this purpose, the lower section 408 includes a mounting platform 440, which also forms the lower surface of the mounting base 112 or cooperates with it. The mounting platform 440 is shaped, dimensioned, and arranged according to the physical properties of the fuselage skin 104 to enable secure attachment of the mounting base 112 to the fuselage skin 104. Furthermore, the left side component 402 of the mounting base 112 includes or works in conjunction with a left mounting flange 444, and the right side component 404 of the mounting base 112 includes or works in conjunction with a right mounting flange 446.The mounting holes 450 formed in the mounting flanges 444, 446 serve to accommodate fastening elements which are used to securely connect the mounting base 112 to the aircraft fuselage 106.

[0031] The interior space 432 of the mounting base 112 is generally defined by its interior surfaces and features. In the illustrated embodiment, the interior space 432 is connected to both the upper opening 424 and the lower access opening 428. In this respect, the interior space 432 is accessible from above via the upper opening 424 and from below via the lower access opening 428. In other words, the interior space 432 extends from the lower access opening 428, which is formed in the lower section 408, to the upper opening 424, which is formed by the frame 416. With further reference to the Fig. Figures 7-10 (showing the carrier housing 110 alone) show that at least part of the access opening 214 of the carrier housing 110 is continuously connected to the interior 432 of the mounting base 112 when the carrier housing 110 is connected to the mounting base 112. This arrangement facilitates the installation of electrical cables and / or connectors of the antenna 108.

[0032] As already mentioned, the passage 118 is designed and arranged to accommodate the rear structure 116 of the aircraft 100 – the rear structure 116 projects beyond the fuselage skin 104 and extends in the longitudinal direction of the aircraft 100. According to the illustrated embodiment, the passage 118 has an opening in the lower section 408 of the mounting base 112 and extends upwards from the lower section 408 towards the frame 416.

[0033] With additional reference to Fig. 2 and Fig. 23 The passage 118 allows the mounting base 112 to flank both sides of the back structure 116 when the mounting base 112 is connected to the fuselage skin 104. In the embodiment described here, the left side component 402 of the mounting base 112 is configured to be installed above the fuselage skin 104, adjacent to and to the left of the back structure 116. Similarly, the right side component 404 is configured to be installed above the fuselage skin 104, adjacent to and to the right of the back structure 116. As shown in Fig. As shown in Figure 17, the passage 118 can include or be defined by a vertical slot 454 and a flanged cutout 458 that is connected to or defined by the vertical slot 454. The width of the vertical slot 454 is adapted to the width of the back structure 116. The height of the vertical slot 454 is adapted to the height of the back structure 116. In certain embodiments, the height of the vertical slot 454 is oversized so that the mounting base 112 is compatible with various airframes (which can use back structures 116 of different heights). A filler plate or plug can be installed to fill any gap that might remain due to an oversized vertical slot 454. Likewise, the width of the vertical slot 454 can be oversized to accommodate back structures 116 of different widths.

[0034] According to exemplary embodiments, the carrier housing 110 and the mounting base 112 work together to form an aerodynamic fairing for the antenna 108. For this purpose, the outer shape and contour of the mounting base 112 can be suitably designed and manufactured to improve its aerodynamics. Furthermore, the front section 410 of the mounting base 112 can be designed and manufactured to provide impact protection (e.g., protection against bird strikes). Similarly, the outer shape and contour of the carrier housing 110 can be suitably designed and manufactured to improve its aerodynamics, and the front section 206 of the carrier housing 110 can also be designed and manufactured to provide impact protection (e.g., protection against bird strikes).

[0035] The mounting base 112 and the carrier housing 110 are jointly designed to form a smooth and essentially continuous transition at their respective front regions. In this respect, the front region 410 of the mounting base has a base side profile that rises from a front region 410 to a rear region 410. This aerodynamic, upwardly inclined shape of the mounting base 112 is described in the Fig. 2, Fig. 5, Fig. 12 and Fig. 13. Similarly, the front section 206 of the carrier housing 110 has a carrier side profile that rises from a front section of the front section 206 to a rear section of the front section 206. This aerodynamic, upwardly inclined shape of the carrier housing 110 is best seen in Fig. 5 shown. In particular, the side profile of the mounting base 112 transitions into the side profile of the support housing 110 (see e.g. Fig. 2, Fig. 4 and Fig. 5).

[0036] Furthermore, the frame 416 of the mounting base 112 includes a curved edge 462, which is defined in the front area 410 (see Fig. 12 and Fig. 15) The curved edge 462 is curved outwards in the forward direction, and the outer surface of the front region 410 is convex. Similarly, the base region 210 of the support housing 110 has a curved front edge 224, which is shaped, dimensioned, and arranged according to the curved edge 462 of the mounting base 112 (see Fig. 7-10). The curved leading edge 224 is curved outwards in the forward direction and is otherwise shaped, dimensioned, and configured such that the curved edge 462 of the frame 416 aligns with the curved leading edge 224 when the support housing 110 is connected to the mounting base 112. The alignment and matching of these curved features is described in the Fig. 2, Fig. 4 and Fig. 5 is visible.

[0037] Fig. Figure 19 is a perspective view showing an exemplary arrangement of components and features (for assembly, installation and structural support) located under the fuselage skin 104 of the aircraft 100. Fig. Figure 19 shows only a small section of the fuselage 106 with various components, features and structures used for the installation of the mounting base 112 and thus the carrier housing 110 and the antenna 108 (which are shown in Fig. 19 are not visible, as they are located on the outside of the fuselage skin 104). The support and fastening elements are configured, positioned, and installed to allow the mounting base 112 to be attached to an outer wall of the fuselage 106. The support and fastening elements are further configured, positioned, and arranged to provide structural support for the other components of the system 102 when the system 102 is used in the aircraft 100. Fig. Figure 19 is an interior view showing an exemplary implementation of an installation arrangement 500 that can be used for assembly, installation and structural support.

[0038] Fig. 19 corresponds to a view from inside the torso 106, directed upwards towards the concave inner surface 502 of the torso skin 104 (the opposite outer surface of the torso skin 104 is in Fig. 19 not visible). Fig. Figure 19 shows a series of upwardly curved frames 506, which are part of the hull 106. The installation arrangement 500 is designed, configured, and implemented to take into account the existing structure and components of the hull 106, such as frames, stringers, skin, intermediate ribs, supports, and conduits. In this respect, the installation arrangement 500 represents a complementary or reinforcing arrangement of components that can be connected to existing elements of the hull 106 to provide additional structural integrity and robustness. As shown in Fig. As shown in Figure 19, at least some elements of the installation arrangement 500 can be connected to the inner surface 502 of the fuselage skin 104. The various elements of the installation arrangement 500 are positioned so that they correspond exactly to the respective features of the system 102 above them (e.g., mounting devices, support structures, mounting holes of the mounting base 112, electrical connections, or cables associated with the antenna 108).

[0039] An embodiment of the installation arrangement 500 can, without limitation, comprise any of the following components: interrib supports, beams, cross frames, doublers, mounting plates, and brackets. In the illustrated embodiment, longitudinally arranged interrib supports 510 are used. Although not specifically indicated, any number of doublers can be used to provide structural support in specific areas beneath the fuselage skin 104. Any number of mounting plates can be used to accommodate fasteners for components located outside the fuselage 106. Any number of clamps (which can be implemented in various shapes, sizes, and configurations) can be used to connect adjacent structural components.For example, brackets can be used to connect an intermediate rib support 510 to a transverse frame or a curved frame 506.

[0040] The Fig. These are schematic top views illustrating the installation of an antenna and the associated mounting system according to the embodiments of the invention. For the sake of simplicity, the fuselage skin is omitted in these figures so that the components located beneath the skin are clearly visible. Furthermore, these figures show only a small section of the aircraft fuselage 106.

[0041] Fig. Figure 20 shows a section of the back structure 116 as it is positioned on the torso 106 - Fig. Figure 20 represents the state of the aircraft before the installation of System 102 began. Fig. Figure 21 shows the state of the aircraft after the installation assembly 500 has been fitted under the fuselage skin. Here too, the installation assembly 500 represents the internal support structure used to attach the mounting base to the fuselage 106. Accordingly, Figure 21 shows the aircraft's condition after the installation assembly 500 has been fitted under the fuselage skin. Fig. 21 the installed positions of the internal support structures in relation to the back structure 116. Fig. Figure 22 shows the state of the aircraft after installation of the right side component 404 of the mounting base, which flanks one side of the dorsal structure 116. Although not shown separately in these figures, a suitably configured gasket and / or a layer of sealing material can be introduced between the underside of the mounting base and the outer surface of the fuselage skin. As shown in Fig. As shown in Figure 22, certain components of the assembly arrangement 500 are aligned with flanges and / or mounting holes of the right component 404 to facilitate the secure attachment of the right component 404 to the fuselage 106. Fig. Figure 23 shows the state of the aircraft after the installation of the left side component 402 of the mounting base. As in Fig. As shown in Figure 23, certain components of the assembly arrangement 500 are aligned with flanges and / or mounting holes of the left side component 402 to facilitate the secure attachment of the left side component 402 to the fuselage 106. Fig. Figure 23 shows how the mounting base accommodates the protruding part of the back structure 116.

[0042] Fig. Figure 24 shows the state of the aircraft after the carrier housing 110 has been connected to the mounting base 112. Although not shown separately, a suitably configured gasket and / or a layer of sealing material can be inserted between the bottom of the carrier housing 110 and the frame of the mounting base 112. Fig. Figure 25 shows the state of the aircraft after the antenna 108 has been installed and secured by the support housing 110. After the antenna 108 has been installed in this way, the retaining frame 119 is inserted and fastened around the circumference of the antenna 108, as shown in Fig. 26 shown (also in the Fig. (shown in Figures 2-4). After installation, the mounting frame 119 secures the antenna 108 to the carrier housing 110.

[0043] The Fig. refer to an embodiment of system 102 that is compatible with antennas that are in Fig. The antenna 108 shown is configured identically or equivalently. As mentioned previously, a universal mounting base 112 can be installed in an aircraft, allowing carrier housings compatible with various antenna configurations to be connected to the universal mounting base 112. Consequently, the carrier housing component can be exchanged as needed to mount the required antenna type (or other type of component) on the universal mounting base 112.

[0044] An alternative embodiment of a component assembly system 600 is described in Fig. 27 (perspective view from above) and Fig. Figure 28 (perspective exploded view) illustrates this. The illustrated embodiment of System 600 includes a mounting base 602, which may be identical, structurally equivalent, or physically similar to the mounting base 112 described above. The mounting base 602 is configured to be installed above the rear structure 116, which rises above the fuselage skin 104 as described above. System 600 uses a support housing 606 that is shaped, dimensioned, and arranged differently from the support housing 110 used by System 102. In this respect, the support housing 606 resembles a lid or cover for the mounting base 602, and the support housing 606 is designed and manufactured to be compatible with an antenna component 610 that has a round or disc-shaped upper portion.

[0045] Fig. Figure 27 shows the system 600 in its extended state. In this state, an antenna cover 614 of the antenna component 610 is visible on top of the carrier housing 606. The remaining elements of the antenna component 610 are located below the antenna cover 614 and are housed inside the mounting base 602. The interior and other elements of the antenna component 610 are described in Fig. Figure 28 illustrates the System 600. This system is presented to demonstrate how a universal or widely compatible mounting base can accommodate various carrier housing configurations, which in turn are compatible with different antenna configurations. It should be clear that other carrier housing form factors can be designed and manufactured to suit the specific application, the dimensions of the component to be mounted, the mounting location, and so on.

[0046] Although at least one exemplary embodiment has been presented in the preceding detailed description, it should be understood that a multitude of variations exist. It should also be noted that the exemplary embodiment(s) described here are not intended to limit the scope, applicability, or configuration of the claimed subject matter in any way. Rather, the preceding detailed description is intended to provide the person skilled in the art with a practical guide for implementing the described embodiment(s). It is understood that various modifications to the function and arrangement of the elements can be made without departing from the scope defined by the claims, which includes known equivalents foreseeable at the time of filing this patent application. QUOTES INCLUDED IN THE DESCRIPTION

[0000] This list of documents cited by the applicant was automatically generated and is included solely for the reader's convenience. The list is not part of the German patent or utility model application. The DPMA accepts no liability for any errors or omissions. Cited patent literature

[0000] US 63 / 653,073

[0001]

Claims

[1] A system for mounting a component on an outer wall of a vehicle, wherein the system comprises: a carrier housing with an upper section configured to receive and hold the component, and with a lower section opposite the upper section, and a mounting base, having: a frame with a support platform configured and arranged so that it can be connected to the lower section of the carrier housing, a lower section opposite the frame, wherein the lower section is configured and arranged so that it can be connected to the outer wall of the vehicle, and a passage with an opening in the lower section, wherein the passage extends from the lower section to the frame, wherein the passage is configured and arranged to accommodate a structural feature of the vehicle extending from the outer wall of the vehicle. [2] The system according to claim 1, wherein the upper section of the support housing is configured to surround a circumferential edge of the component, and the carrier housing holds the component in such a way that a main surface of the component is exposed. [3] The system according to claim 1, wherein the outer wall has an outside and an opposite inside, wherein the system further comprises an arrangement of support and fastening elements connected to the inside of the outer wall, wherein the arrangement of support and fastening elements is configured to enable the mounting base to be attached to the outer wall, and further configured to provide structural support to the mounting base when the mounting base is attached to the outer wall. [4] System according to claim 1, wherein the passage is designed and arranged in such a way that it can accommodate a dorsal structure of the vehicle. [5] System according to claim 4, wherein the mounting base is configured and arranged to flank both sides of the dorsal structure of the vehicle. [6] The system according to claim 1, wherein the mounting base has a left and a right component, wherein the left component is configured to be installed above the outer wall adjacent to and to the left of the structural feature, and wherein the right component is configured to be installed above the outer wall adjacent to and to the right of the structural feature. [7] The system according to claim 1, wherein the mounting base has a front base area with a base side profile that rises from a front area of ​​the front base area to a rear area of ​​the front base area, and wherein the lower section of the carrier housing has a front carrier area with a carrier side profile that rises from a front area of ​​the front carrier area to a rear area of ​​the front carrier area, where the base side profile transitions into the support side profile. [8] The system according to claim 1, the mounting base has a front base area, wherein the frame has a curved edge that is defined in the front base area, wherein the lower section of the carrier housing has a base area with a curved leading edge, and wherein the curved edge of the frame aligns with the curved front edge of the lower section when the carrier housing is connected to the mounting base. [9] The system according to claim 1, wherein the lower section of the carrier housing has an access opening, wherein the mounting base has an interior space defined therein, the interior space extending from a lower opening formed in the lower section of the mounting base to an upper opening formed by the edge of the mounting base, and where at least part of the access opening is continuously connected to the interior when the carrier housing is connected to the mounting base. [10] System according to claim 1, wherein the carrier housing and the mounting base cooperate to form an aerodynamic fairing for the component. [11] A system configured to be attached to the exterior paneling of a vehicle, the system comprising: an antenna component, a carrier housing coupled to the antenna component, wherein the carrier housing has an upper section configured to receive and hold the antenna component, and a lower section opposite the upper section, and a mounting base, having: a frame with a support platform configured and arranged so that it can be connected to the lower section of the carrier housing, a lower section opposite the frame, wherein the lower section is configured and arranged so that it can be connected to the outer paneling of the vehicle, and a passage with an opening in the floor section, wherein the passage extends from the floor section to the frame, wherein the passage is configured and arranged to accommodate a structural feature of the vehicle extending from the outer paneling of the vehicle. [12] System according to claim 11, wherein the antenna component is a flat panel satellite communication antenna. [13] The system according to claim 11, wherein the outer cladding has an outer side and an opposing inner side, the system further comprises an arrangement of support and fastening elements connected to the inside of the outer cladding, and wherein the arrangement of support and fastening elements is configured to enable the mounting base to be attached to the outer cladding, and is further configured to provide structural support to the mounting base when the mounting base is attached to the outer cladding. [14] System according to claim 11, wherein the mounting base is configured and arranged to flank both sides of a dorsal structure of the vehicle when the mounting base is attached to the outer panel. [15] The system according to claim 14, wherein the mounting base has a left and a right component, wherein the left side component is configured to be installed above the outer cladding adjacent to and to the left of the dorsal structure, and wherein the right side component is configured to be installed above the outer cladding adjacent to and to the right of the dorsal structure. [16] The system according to claim 11, the mounting base has a front base area, wherein the frame has a curved edge that is defined in the front base area, wherein the lower section of the carrier housing has a base area with a curved leading edge, and wherein the curved edge of the frame aligns with the curved front edge of the lower section when the carrier housing is connected to the mounting base. [17] The system according to claim 11, wherein the lower section of the carrier housing has an access opening, wherein the mounting base has an interior space defined therein, the interior space extending from a lower opening formed in the lower section of the mounting base to an upper opening formed by the edge of the mounting base, and where at least part of the access opening is continuously connected to the interior when the carrier housing is connected to the mounting base. [18] System according to claim 1, wherein the carrier housing and the mounting base work together to form an aerodynamic fairing for the antenna component. [19] A vehicle with the system according to claim 10. [20] The vehicle according to claim 19, wherein the vehicle is an aircraft, where the outer wall corresponds to the fuselage skin of the aircraft, and where the antenna component is a flat panel satellite communication antenna.

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