Aircraft composite mounting device, rack system and aircraft

Abstract

The utility model relates to an aircraft composite mounting device, a rack system and an aircraft, relates to the technical field of flight equipment, and aims to solve the problems that an aircraft hanging frame in the prior art cannot meet the transportation requirements of different types of articles and is low in loading capacity. The utility model discloses a composite mounting device for an aircraft. The composite mounting device comprises a side hanger, a belly hanger and a mounting plate assembly, the side hanging rack is connected with the abdomen hanging rack, and the mounting plate assembly is arranged on the side hanging rack and / or the abdomen hanging rack. The rack-mounted system provided by the utility model comprises the aircraft composite mounting device. The aircraft provided by the utility model comprises the rack system. The multi-purpose carrying vehicle is high in bearing capacity, wide in application range, high in applicability and capable of carrying articles in a large-range and multi-purpose mode.

Description

Technical Field

[0001] The utility model relates to the technical field of flying devices, in particular to a composite mounting device for an aircraft, a frame system and an aircraft. Background Art

[0002] With the development and progress of flying device technologies such as unmanned aerial vehicles, flying devices are increasingly used in item transportation operations.

[0003] According to the requirements of the tasks to be performed, flying devices often need to carry items of different shapes and types, such as emergency supplies, fire extinguishing bombs, etc. The connection methods between different items and the hanging brackets of the flying devices also vary, such as being connected to the hanging brackets of the flying devices by bolts, being lifted by hooks, etc.

[0004] In the prior art, the connection method between the hanging bracket and the item to be transported is relatively single, unable to meet the transportation requirements of different types of items, with low applicability; the loading space of the hanging bracket is small and the loading capacity is low. Summary of the Utility Model

[0005] In view of the above analysis, the utility model aims to provide a composite mounting device for an aircraft, a frame system and an aircraft, so as to solve the problems that the hanging brackets of flying devices in the prior art cannot meet the transportation requirements of different types of items and have low loading capacity.

[0006] The utility model provides a composite mounting device for an aircraft, including side hanging brackets, an abdominal hanging bracket and a mounting plate assembly;

[0007] The side hanging brackets are connected to the abdominal hanging bracket, and the mounting plate assembly is arranged on the side hanging brackets and / or the abdominal hanging bracket.

[0008] Further, the mounting plate assembly includes a sliding member and a mounting plate, and the mounting plate is connected to the side hanging brackets and / or the abdominal hanging bracket through the sliding member.

[0009] Further, there are two side hanging brackets, symmetrically arranged on both sides of the abdominal hanging bracket.

[0010] Further, it further includes a first fixing member. A first joint is arranged on the side hanging bracket, a second joint is arranged on the abdominal hanging bracket, and the first joint cooperates with the second joint and is fixed through the first fixing member.

[0011] Further, the mounting plate assembly further includes a lifting member, the lifting member is arranged on the mounting plate, and mounting holes are arranged on the mounting plate.

[0012] The utility model also provides a frame system, including a frame and the above-mentioned composite mounting device for an aircraft.

[0013] Furthermore, the aircraft composite mounting device further includes a first connection component and a second connection component. The first connection component is connected to the side mounting rack, and the second connection component is connected to the belly mounting rack.

[0014] Furthermore, the first connection component includes a side mounting rack connection section, a frame connection section, and a connecting piece. One end of the side mounting rack connection section is connected to the side mounting rack, and the other end is connected to the frame connection section. The connecting piece is arranged on the frame connection section, and the connecting piece connects the frame connection section to the frame.

[0015] Furthermore, it further includes a second fixing piece. A third joint is arranged on the frame. The second connection component includes a connecting rod and a fourth joint. One end of the connecting rod is connected to the belly mounting rack, and the other end is connected to the fourth joint. The fourth joint cooperates with the third joint and is fixed by the second fixing piece.

[0016] The present utility model also provides an aircraft, including the above-mentioned frame system.

[0017] The technical solution of the present utility model can at least achieve one of the following effects:

[0018] (1) For the aircraft composite mounting device of the present utility model, by setting a side mounting rack and a belly mounting rack connected to the side mounting rack, the mounting space of the aircraft mounting rack is increased, thereby improving the mounting capacity of the aircraft and the efficiency of transporting items by the aircraft;

[0019] (2) For the aircraft composite mounting device of the present utility model, a first joint is arranged on the side mounting rack, and a second joint is arranged on the belly mounting rack. The first joint and the second joint are fixed by a fixing piece, so that the side mounting rack and the belly mounting rack are detachably connected, facilitating the disassembly and assembly of the side mounting rack and the belly mounting rack, and increasing the adaptability of the composite mounting device;

[0020] (3) For the aircraft composite mounting device of the present utility model, by setting an installation plate assembly, the installation plate can move along the side mounting rack and / or the belly mounting rack through a sliding piece, so as to adjust the installation plate according to the items to be transported, and enable the installation plate to carry the items to be transported;

[0021] (4) For the aircraft composite mounting device of the present utility model, by arranging a hoisting piece and mounting holes on the installation plate, the installation plate can also hoist items and connect the items to the installation plate through the mounting holes, thereby increasing the transporting capacity and the scope of use of the aircraft composite mounting device.

[0022] (5) The frame system of the present utility model connects the aircraft composite mounting device to the frame through the first connection component and the second connection component, facilitating the installation and disassembly of the aircraft composite mounting device and the frame. The operation is simple and the disassembly is convenient.

[0023] (6) The aircraft of the present utility model adopts the frame system, thereby improving the mounting capacity and application range of the aircraft, enabling the aircraft to have functions such as strong load-bearing capacity, wide application range, and strong applicability, and thus realizing large-range multi-purpose transportation of items.

[0024] In the present utility model, the above technical solutions can also be combined with each other to achieve more preferred combination schemes. Other features and advantages of the present utility model will be described in the subsequent description, and some advantages can be made obvious from the description, or understood by implementing the present utility model. The objectives and other advantages of the present utility model can be achieved and obtained through the content specifically pointed out in the description and the drawings. Description of the Drawings

[0025] The drawings are only for the purpose of showing specific embodiments and are not considered to be a limitation of the present utility model. Throughout the drawings, the same reference signs represent the same components.

[0026] Figure 1 It is a schematic diagram of the overall structure of the aircraft composite mounting device of Embodiment 1 of the present utility model;

[0027] Figure 2 It is one of the schematic diagrams of the structure of the belly rack and the mounting plate assembly of Embodiment 1 of the present utility model;

[0028] Figure 3 It is another schematic diagram of the structure of the belly rack and the mounting plate assembly of Embodiment 1 of the present utility model;

[0029] Figure 4 It is a partial schematic diagram of the connection between the first joint and the second joint of Embodiment 1 of the present utility model;

[0030] Figure 5 It is a schematic diagram of the overall structure of the frame system of Embodiment 2 of the present utility model;

[0031] Figure 6 It is a schematic diagram of the structure of the first connection component of Embodiment 2 of the present utility model;

[0032] Figure 7 It is a partial schematic diagram of the connection between the second connection component and the frame of Embodiment 2 of the present utility model;

[0033] Figure 8One of the overall structural schematic diagrams of the aircraft carrying items in Embodiment 3 of the present utility model;

[0034] Figure 9 Another overall structural schematic diagram of the aircraft carrying items in Embodiment 3 of the present utility model.

[0035] Reference numerals:

[0036] 1 - Side hanger; 11 - First joint; 2 - Abdominal hanger; 21 - Second joint; 3 - First connection assembly; 31 - Side hanger connection section; 32 - Frame connection section; 33 - Connecting piece; 4 - Second connection assembly; 41 - Connecting rod; 42 - Fourth joint; 5 - Mounting plate assembly; 51 - Sliding part; 52 - Mounting plate; 53 - Suspended load; 6 - Frame; 61 - Third joint. Detailed implementation manners

[0037] The following will specifically describe the preferred embodiments of the present utility model with reference to the accompanying drawings. Among them, the accompanying drawings form a part of the present utility model and are used together with the embodiments of the present utility model to explain the principle of the present utility model, rather than to limit the scope of the present utility model.

[0038] Embodiment 1

[0039] A specific embodiment of the present utility model discloses an aircraft composite hanging device. As Figures 1 to 2 shown, it includes a side hanger 1, an abdominal hanger 2 and a mounting plate assembly 5; the side hanger 1 is connected to the abdominal hanger 2, and the mounting plate assembly 5 is arranged on the side hanger 1 and / or the abdominal hanger 2; the mounting plate assembly 5 includes a sliding part 51 and a mounting plate 52, and the mounting plate 52 is connected to the side hanger 1 and / or the abdominal hanger 2 through the sliding part 51, so that the mounting plate 52 can move along the side hanger 1 and / or the abdominal hanger 2.

[0040] In this embodiment, the example of the connection between the mounting plate assembly 5 and the abdominal hanger 2 is taken.

[0041] Furthermore, the side hanger 1 is arranged on both sides of the abdominal hanger 2. Preferably, the side hanger 1 is symmetrically arranged on both sides of the abdominal hanger 2, so as to increase the hanging area of the aircraft hanger and maintain the balance of the aircraft.

[0042] Exemplarily, the sliding part 51 is a hoop, and bolts are arranged on the hoop. According to the specifications of the hanging item, the position of the mounting plate 52 is adjusted through the hoop, and the position of the hoop is fixed by tightening the bolts, so as to fix the position of the mounting plate 52.

[0043] Exemplarily, the sliding part 51 is a ring-shaped buckle, and the position of the mounting plate 52 can be adjusted and fixed through the ring-shaped buckle.

[0044] Preferably, mounting holes are provided on the mounting plate 52, so that the articles to be transported can be connected to the mounting plate 52 through the mounting holes. Exemplarily, the mounting holes are threaded holes, and the articles to be transported are threadedly connected to the mounting holes.

[0045] Preferably, as Figure 3 shown, the mounting plate assembly 5 further includes a lifting member 53. The lifting member 53 is arranged on the mounting plate 52, and the articles can be lifted by the lifting member 53. Exemplarily, the lifting member 53 is a hook.

[0046] Furthermore, as Figure 4 shown, a first joint 11 is arranged on the side hanging rack 1, and a second joint 21 is arranged on the abdominal hanging rack 2. The first joint 11 cooperates with the second joint 21 and is fixed by a first fixing member, so that the side hanging rack 1 is connected to the abdominal hanging rack 2.

[0047] Exemplarily, the first fixing member is a screw, the first joint 11 is a double-ear joint, and the second joint 21 is a single-ear joint. The single-ear joint and the double-ear joint are detachably connected by a screw, so as to facilitate connecting and separating the side hanging rack 1 and the abdominal hanging rack 2 according to the hanging requirements.

[0048] Embodiment 2

[0049] A specific embodiment of the present utility model discloses a frame system, as Figure 5 shown, including a frame 6 and the aircraft composite hanging device described in Embodiment 1.

[0050] The aircraft composite hanging device further includes a first connection component 3 and a second connection component 4. The first connection component 3 is connected to the side hanging rack 1, and the second connection component 4 is connected to the abdominal hanging rack 2. The first connection component 3 and the second connection component 4 are used to connect the composite hanging device to the frame 6.

[0051] Furthermore, as Figure 6 shown, the first connection component 3 includes a side hanging rack connection section 31, a frame connection section 32 and a connecting member 33. One end of the side hanging rack connection section 31 is connected to the side hanging rack 1, and the other end is connected to the frame connection section 32. The connecting member 33 is arranged on the frame connection section 32, and the connecting member 33 connects the frame connection section 32 to the frame 6.

[0052] Preferably, the connecting member 33 is a quick-release pin. By using the quick-release pin, the frame connection section 32 can be quickly connected to and removed from the frame 6, thus saving operation time. The quick-release pin is a prior art and will not be elaborated here.

[0053] Furthermore, as Figure 7As shown in the figure, a third joint 61 is provided on the frame 6. The second connection assembly 4 includes a connecting rod 41 and a fourth joint 42. One end of the connecting rod 41 is connected to the abdominal hanger 2, and the other end is connected to the fourth joint 42. The fourth joint 42 cooperates with the third joint 61 and is fixed by a second fixing member, so that the second connection assembly 4 is connected to the frame 6.

[0054] Exemplarily, the third joint 61 is a double-ear joint, the fourth joint 42 is a single-ear joint, and the second fixing member is a screw. The double-ear joint and the single-ear joint are detachably connected by the screw, so that the abdominal hanger 2 is detachably connected to the frame 6.

[0055] Embodiment 3

[0056] An aircraft includes the frame system described in Embodiment 2. As Figures 8 to 9 shown, the frame system is connected to the aircraft shell, so that the frame 6 is located inside the aircraft shell, the abdominal hanger 2 is located at the belly position of the aircraft, and the side hanger 1 is located on both sides of the belly of the aircraft.

[0057] Exemplarily, the types of the aircraft are helicopter, drone, gyrocopter, etc.

[0058] Preferably, the aircraft is an unmanned helicopter. The staff can transport items by controlling the unmanned helicopter, which increases the carrying capacity of the unmanned helicopter. It is simple to operate, safe to use, and has a wide range of applications. It can improve the carrying capacity and operation efficiency of the unmanned helicopter in scenarios such as using the unmanned helicopter to carry fire extinguishing bombs for fire extinguishing operations and transporting supplies to areas where people cannot enter.

[0059] Exemplarily, as Figure 8 shown, the unmanned helicopter can hoist and transport or drop items through the hoisting member 53.

[0060] Exemplarily, as Figure 9 shown, the unmanned helicopter can load and transport items through the mounting plate 52.

[0061] In addition, the unmanned helicopter can also operate by using the hoisting member 53 and the mounting plate 52 simultaneously within its allowable load range to make full use of the transport capacity of the unmanned helicopter.

[0062] Compared with the prior art, the aircraft composite mounting device of the present utility model increases the mounting space of the aircraft mounting rack by setting the side mounting rack 1 and the abdominal mounting rack 2 connected to the side mounting rack 1, thereby improving the mounting capacity of the aircraft and the efficiency of the aircraft in carrying items; for the aircraft composite mounting device of the present utility model, a first joint 11 is provided on the side mounting rack 1, and a second joint 21 is provided on the abdominal mounting rack 2. The first joint 11 and the second joint 21 are fixed by fixing members, so that the side mounting rack 1 and the abdominal mounting rack 2 are detachably connected, facilitating the disassembly and assembly of the side mounting rack 1 and the abdominal mounting rack 2, and increasing the adaptability of the composite mounting device;

[0063] For the aircraft composite mounting device of the present utility model, by setting the mounting plate assembly 5, the mounting plate 52 can move along the side mounting rack 1 and / or the abdominal mounting rack 2 through the sliding member 51, so as to adjust the mounting plate 52 according to the items to be carried, and make the mounting plate 52 carry the items to be carried; by providing a hoisting member 53 and mounting holes on the mounting plate 52, the mounting plate 52 can also hoist the items and connect the items to the mounting plate 52 through the mounting holes, thereby increasing the carrying capacity and the scope of use of the aircraft composite mounting device.

[0064] For the frame system of the present utility model, the aircraft composite mounting device is connected to the frame 6 through the first connection component 3 and the second connection component 4, facilitating the installation and disassembly of the aircraft composite mounting device and the frame 6, with simple operation and convenient disassembly.

[0065] For the aircraft of the present utility model, by adopting the frame system, the mounting capacity and the scope of use of the aircraft are improved, enabling the aircraft to have functions such as strong carrying capacity, wide scope of use, and strong applicability, so as to realize large-range multi-purpose carrying of items.

[0066] The above is only the preferred specific embodiment of the present utility model, but the protection scope of the present utility model is not limited thereto. Any changes or substitutions that can be easily thought of by those skilled in the art within the technical scope disclosed by the present utility model should be covered within the protection scope of the present utility model.

Claims

1. A composite mounting device for an aircraft, characterized in that It includes a side hanger (1), an abdominal hanger (2) and a mounting plate assembly (5); The side hanger (1) is connected to the abdominal hanger (2), and the mounting plate assembly (5) is arranged on the side hanger (1) and / or the abdominal hanger (2).

2. The aircraft composite mounting device according to claim 1, wherein The mounting plate assembly (5) includes a sliding member (51) and a mounting plate (52), and the mounting plate (52) is connected to the side hanger (1) and / or the abdominal hanger (2) through the sliding member (51).

3. The aircraft composite mounting device according to claim 1, wherein There are two side hangers (1), symmetrically arranged on both sides of the abdominal hanger (2).

4. The aircraft composite mounting device according to claim 1, characterized in that It further includes a first fixing member. A first joint (11) is arranged on the side hanger (1), a second joint (21) is arranged on the abdominal hanger (2), and the first joint (11) cooperates with the second joint (21) and is fixed through the first fixing member.

5. The aircraft composite hanging device according to claim 2, characterized in that, The mounting plate assembly (5) further includes a lifting member (53), the lifting member (53) is arranged on the mounting plate (52), and mounting holes are arranged on the mounting plate (52).

6. A frame system, characterized in that, It includes a frame (6) and the aircraft composite mounting device according to any one of claims 1-5.

7. The rack system according to claim 6, characterized in that, The aircraft composite mounting device further includes a first connection assembly (3) and a second connection assembly (4). The first connection assembly (3) is connected to the side hanger (1), and the second connection assembly (4) is connected to the abdominal hanger (2).

8. The frame system according to claim 7, characterized in that The first connection assembly (3) includes a side hanger connection section (31), a frame connection section (32) and a connecting member (33). One end of the side hanger connection section (31) is connected to the side hanger (1), the other end is connected to the frame connection section (32), the connecting member (33) is arranged on the frame connection section (32), and the connecting member (33) connects the frame connection section (32) to the frame (6).

9. The rack system according to claim 7, wherein It further includes a second fixing member. A third joint (61) is arranged on the frame (6), the second connection assembly (4) includes a connecting rod (41) and a fourth joint (42), one end of the connecting rod (41) is connected to the abdominal hanger (2), the other end is connected to the fourth joint (42), the fourth joint (42) cooperates with the third joint (61), and is fixed through the second fixing member.

10. An aircraft, characterized in that, It includes the frame system according to any one of claims 6-9.

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