Conveyor airborne equipment support

Abstract

The utility model relates to the technical field of conveyors, in particular to a conveyor airborne equipment support which comprises an adjustable frame, a matching frame arranged at the bottom of the adjustable frame, a bearing plate arranged above the adjustable frame and a plurality of steel wire rope shock absorbers used for connecting the bearing plate and the adjustable frame. The matching frame is fixed to various conveyor fixing points in a matched mode, and a plurality of bearing holes are formed in the bearing plate. When the support is used, the support is matched with various conveyor fixing points to be fixed through the matching frame, the fixing position of the bearing plate is adjusted through the adjustable frame, special equipment such as various testing instruments and meters can be fixed through the bearing holes in the bearing plate, and shock absorption can be conducted on the bearing plate through the steel wire rope shock absorbers; the support is adjustable in size, can be matched with connecting structures of various machine bodies, is safer and more reliable in the transportation process, can also be matched with conveyor fixing points of various machine bodies, and is more convenient to use.

Description

Technical Field

[0001] The utility model relates to the technical field of transport aircraft, in particular to an airborne equipment bracket for a transport aircraft. Background Art

[0002] When special equipment such as test instruments are added to a transport aircraft, there are no dedicated fixtures in the cabin for these instruments. Three common methods are used to secure the equipment: 1. Install the equipment in a cabinet, which is then secured to the cabin; 2. Secure the equipment directly to the cabin using tie-down ropes; 3. Use the equipment's own accessories to secure it to the cabin.

[0003] However, in actual applications, the above three methods have limited effect. The standard cabinet size is fixed and does not match the body connection structure; the fastening rope has high tension, and there is a safety hazard of loosening during the shaking of the transport aircraft; the equipment's own accessories are not aviation standards and are difficult to match the transport aircraft's fixed points, making them inconvenient to use. Therefore, a transport aircraft onboard equipment bracket is designed to address the shortcomings of the existing technology. Utility Model Content

[0004] The purpose of the present utility model is to address the above-mentioned deficiencies and provide a transport aircraft onboard equipment bracket, the bracket size is adjustable, can match the connection structure of various bodies, the transportation process is safer and more reliable, and can also match the transport aircraft fixing points of various bodies, making it more convenient to use.

[0005] In order to achieve the above purpose, the present invention adopts the following technical solutions:

[0006] A transport aircraft onboard equipment bracket includes an adjustable frame, a matching frame arranged at the bottom of the adjustable frame, and a load-bearing plate arranged above the adjustable frame, which is used to connect the load-bearing plate and multiple wire rope shock absorbers used by the adjustable frame. The matching frame is suitable for being fixed at various transport aircraft fixing points, and the load-bearing plate is provided with multiple load-bearing holes.

[0007] Furthermore, the adjustable frame includes a symmetrically arranged support plate, a rectangular frame arranged above the support plate, and a plurality of telescopic frames used to connect the support plate and the rectangular frame. A lower adjustment groove is provided on the bottom end of the support plate facing the telescopic frame, and an upper adjustment groove is provided on the top end of the rectangular frame facing the telescopic frame. The telescopic frame and the lower adjustment groove, and the telescopic frame and the upper adjustment groove are tightened by adjusting bolts, and the wire rope shock absorber is connected to the rectangular frame.

[0008] Furthermore, the telescopic frame includes a lower slide frame, the bottom end of which is slidably connected to an upper slide frame of the lower slide frame, and a plurality of lower slide holes are provided on the lower slide frame along the length direction of the lower slide frame, and a plurality of upper slide holes are provided on the upper slide frame opposite to the lower slide holes, and the opposite lower slide holes and the upper slide holes are tightened by bolts, the top end of the upper slide frame is connected to the upper adjustment slot by the second adjusting bolt on the upper side, and the bottom end of the lower slide frame is connected to the support plate by the second adjusting bolt on the lower side.

[0009] Furthermore, the matching frame includes two connecting rods arranged at the bottom of the support plate, a locking piece arranged on the connecting rod, one end of the connecting rod is rotatably connected to the support plate, a plurality of fixing holes are provided on the connecting rod, and the rotatable ends of the two connecting rods are respectively arranged near the two ends of the support plate.

[0010] Furthermore, the locking part includes a shell, an internal threaded through hole arranged in the shell, one end of a stud 1 screwed to the internal threaded through hole, and one end of a stud 2 screwed to the internal threaded through hole, the other end of the stud 1 is provided with a stud hole, and the other end of the stud 2 is provided with an auxiliary hole.

[0011] Furthermore, a receiving hole is provided at the bottom of the support plate, and when the connecting rod is in the rotated state, the fixing hole is opposite to the receiving hole.

[0012] The beneficial effects of the utility model are:

[0013] In actual application, when in use, the bracket is adapted to various fixed points of transport aircraft through the matching frame, the fixed position of the load-bearing plate is adjusted through the adjustable frame, and various test instruments and other special equipment can be fixed through the multiple load-bearing holes on the load-bearing plate, and the load-bearing plate is shock-absorbing through multiple wire rope shock absorbers; the bracket of the utility model is adjustable in size and can match the connection structure of various bodies, making the transportation process safer and more reliable, and can also match the fixed points of transport aircraft of various bodies, making it more convenient to use. BRIEF DESCRIPTION OF THE DRAWINGS

[0014] Figure 1 It is a schematic diagram of the overall structure of the utility model;

[0015] Figure 2 It is the main view of the utility model;

[0016] Figure 3 This is a bottom view of the utility model when in use;

[0017] Figure markings: adjustable frame 1; support plate 11; lower adjustment slot 111; storage hole 112; rectangular frame 12; upper adjustment slot 121; telescopic frame 13; lower slide 131; lower slide hole 1311; upper slide 132; upper slide hole 1321; matching frame 2; connecting rod 21; fixing hole 211; locking member 22; housing 221; stud one 222; stud hole 2221; stud two 223; auxiliary hole 2231; load-bearing plate 3; load-bearing hole 31; wire rope shock absorber 4. DETAILED DESCRIPTION

[0018] like Figure 1 、 Figure 2 and Figure 3 As shown, a transport aircraft onboard equipment bracket includes an adjustable frame 1, a matching frame 2 arranged at the bottom of the adjustable frame 1, and a load-bearing plate 3 arranged above the adjustable frame 1, which is used to connect the load-bearing plate 3 and multiple wire rope shock absorbers 4 used by the adjustable frame 1. The matching frame 2 is suitable for being fixed at various transport aircraft fixing points, and the load-bearing plate 3 is provided with multiple load-bearing holes 31.

[0019] When in use, the bracket is adapted to various fixed points of transport machines through the matching frame 2, the fixed position of the load-bearing plate 3 is adjusted through the adjustable frame 1, and various test instruments and other special equipment can be fixed through the multiple load-bearing holes 31 on the load-bearing plate 3, and the load-bearing plate 3 is shock-absorbing through multiple wire rope shock absorbers 4; the size of the bracket of the utility model is adjustable and can match the connection structure of various bodies, making the transportation process safer and more reliable. It can also match the fixed points of transport machines of various bodies, making it more convenient to use.

[0020] like Figure 1 、 Figure 2 and Figure 3 As shown, the adjustable frame 1 includes a symmetrically arranged support plate 11, a rectangular frame 12 arranged above the support plate 11, and a plurality of telescopic frames 13 used to connect the support plate 11 and the rectangular frame 12. A lower adjusting groove 111 is provided on the support plate 11 at the bottom end facing the telescopic frame 13, and an upper adjusting groove 121 is provided on the rectangular frame 12 at the top end facing the telescopic frame 13. The telescopic frame 13 and the lower adjusting groove 111, and the telescopic frame 13 and the upper adjusting groove 121 are tightened by adjusting bolts 1, and the wire rope shock absorber 4 is connected to the rectangular frame 12; in this embodiment, the installation height of special equipment such as test instruments and meters on the load-bearing plate 3 can be adjusted by the telescopic frame 13, and the installation position of the special equipment on the support plate 11 can be adjusted by adjusting the tightening position of the adjusting bolts 1 in the upper adjusting groove 121 and the lower adjusting groove 111.

[0021] like Figure 1 、 Figure 2 and Figure 3As shown, the telescopic frame 13 includes a lower slide frame 131, and an upper slide frame 132 of the lower slide frame 131 is slidably connected to the lower slide frame 131 at its bottom end. Along the length direction of the lower slide frame 131, a plurality of lower slide holes 1311 are provided on the lower slide frame 131, and a plurality of upper slide holes 1321 are provided on the upper slide frame 132 opposite to the lower slide holes 1311. The opposite lower slide holes 1311 and the upper slide holes 1321 are tightened by bolts, and the top of the upper slide frame 132 is connected to the upper adjustment slot 121 through the upper adjusting bolt 2, and the bottom end of the lower slide frame 131 is connected to the support plate 11 through the lower adjusting bolt 2; in this embodiment, by adjusting the opposite upper sliding holes 1321 and the lower sliding holes 1311, the height of the rectangular frame 12 at the top of the telescopic frame 13 can be adjusted, thereby adjusting the installation height of the special equipment.

[0022] like Figure 1 、 Figure 2 and Figure 3 As shown, the matching frame 2 includes two connecting rods 21 arranged at the bottom of the support plate 11, and a locking piece 22 arranged on the connecting rod 21. One end of the connecting rod 21 can be rotatably connected to the support plate 11. A plurality of fixing holes 211 are provided on the connecting rod 21. The rotatable ends of the two connecting rods 21 are respectively arranged near the two ends of the support plate 11. In this embodiment, the bracket can be fixed by tightening the fixing holes 211 on the connecting rod 21, the cabin fixing holes 211 on the transport aircraft body and the locking piece 22 with fastening bolts.

[0023] like Figure 1 、 Figure 2 and Figure 3 As shown, the locking member 22 includes a shell 221, an internally threaded through hole arranged in the shell 221, a stud 1 222 screwed to the internally threaded through hole at one end, a stud 223 screwed to the internally threaded through hole at one end, a stud hole 2221 provided at the other end of the stud 1 222, and an auxiliary hole 2231 provided at the other end of the stud 223; in this embodiment, the bracket can be further fixed by tightening the fixing hole 211 on the connecting rod 21, the cabin fixing hole 211 and the stud hole 2221 on the transport aircraft body by tightening the bolts, and tightening the auxiliary hole 2231 and the cabin fixing ear by screws.

[0024] like Figure 1 、 Figure 2 and Figure 3 As shown, a storage hole 112 is further provided at the bottom of the support plate 11. When the connecting rod 21 is in the rotated state, the fixing hole 211 is opposite to the storage hole 112. In this embodiment, when the connecting rod 21 is rotated back to the bottom of the support plate 11, the storage hole 112 and the connecting rod 21 are tightened by bolts, so that the connecting rod 21 can be folded and stored.

[0025] The specific embodiments described herein are merely examples of the present invention. Those skilled in the art may make various modifications or additions to the specific embodiments described, or replace them with similar methods without departing from the scope of the present invention.

Claims

1. A transport aircraft onboard equipment bracket, characterized by: The invention comprises an adjustable frame (1), a matching frame (2) arranged at the bottom of the adjustable frame (1), and a bearing plate (3) arranged above the adjustable frame (1), which is used to connect the bearing plate (3) and a plurality of steel wire rope shock absorbers (4) used by the adjustable frame (1); the matching frame (2) is adapted to be fixed at various fixed points of transport machines, and the bearing plate (3) is provided with a plurality of bearing holes (31).

2. The transport aircraft onboard equipment bracket according to claim 1, characterized in that: The adjustable frame (1) comprises a symmetrically arranged support plate (11), a rectangular frame (12) arranged above the support plate (11), and a plurality of telescopic frames (13) used to connect the support plate (11) and the rectangular frame (12). A lower adjustment groove (111) is provided on the bottom end of the support plate (11) facing the telescopic frame (13), and an upper adjustment groove (121) is provided on the top end of the rectangular frame (12) facing the telescopic frame (13). Adjustment bolts are tightened between the telescopic frame (13) and the lower adjustment groove (111), and between the telescopic frame (13) and the upper adjustment groove (121). The wire rope shock absorber (4) is connected to the rectangular frame (12).

3. The transport aircraft onboard equipment bracket according to claim 2, characterized in that: The telescopic frame (13) includes a lower slide frame (131), an upper slide frame (132) slidably connected to the lower slide frame (131) at its bottom end, a plurality of lower slide holes (1311) are provided on the lower slide frame (131) along the length direction of the lower slide frame (131), and a plurality of upper slide holes (1321) are provided on the upper slide frame (132) opposite to the lower slide holes (1311), and the opposite lower slide holes (1311) and the upper slide holes (1321) are tightened by bolts, the top end of the upper slide frame (132) is connected to the upper adjustment groove (121) by the second upper adjustment bolt, and the bottom end of the lower slide frame (131) is connected to the support plate (11) by the second lower adjustment bolt.

4. The transport aircraft onboard equipment bracket according to claim 2, characterized in that: The matching frame (2) includes two connecting rods (21) arranged at the bottom of the support plate (11), and a locking piece (22) arranged on the connecting rod (21). One end of the connecting rod (21) is rotatably connected to the support plate (11). A plurality of fixing holes (211) are provided on the connecting rod (21). The rotatable ends of the two connecting rods (21) are respectively arranged near the two ends of the support plate (11).

5. The transport aircraft onboard equipment bracket according to claim 4, characterized in that: The locking member (22) includes a shell (221), an internal threaded through hole arranged in the shell (221), a stud 1 (222) screwed to the internal threaded through hole at one end, a stud 2 (223) screwed to the internal threaded through hole at one end, a stud hole (2221) arranged at the other end of the stud 1 (222), and an auxiliary hole (2231) arranged at the other end of the stud 2 (223).

6. The transport aircraft onboard equipment bracket according to claim 4, characterized in that: The bottom of the support plate (11) is further provided with a receiving hole (112); when the connecting rod (21) is in a rotating state, the fixing hole (211) faces the receiving hole (112).

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