CN217375309U

CN217375309U - Unmanned aerial vehicle transportation bracket

Info

Publication number: CN217375309U
Application number: CN202220996379.6U
Authority: CN
Inventors: 侯宝林; 魏昌进; 杨超
Original assignee: Sichuan Hengshenglixun Intelligent Equipment Co ltd
Current assignee: Sichuan Hengshenglixun Intelligent Equipment Co ltd
Priority date: 2022-04-24
Filing date: 2022-04-24
Publication date: 2022-09-06
Anticipated expiration: 2032-04-24

Abstract

The utility model discloses an unmanned aerial vehicle transportation bracket, which belongs to the technical field, and comprises a bracket frame, wherein a plurality of transverse rods are arranged inside the frame body of the bracket frame, a fixing frame is arranged at the intersection of a longitudinal rod transverse rod and a longitudinal rod inside the frame body of the bracket frame, a fixing seat is arranged at the top of the fixing frame, the fixing seat is fixedly arranged inside the fixing frame in a welding mode, a rubber pad is arranged at the top of the fixing seat, side plates are arranged at two adjacent sides of the fixing seat, adjusting bolts are arranged at the outer sides of the side plates, an interface pressing block is arranged at the top of the rubber pad, a rubber layer is arranged at the bottom of the interface pressing block, pre-tightening bolts are arranged at two sides of the top of the fixing seat, and a compression nut is arranged at the top end of the pre-tightening bolts, through the design to the fixing base and set up the rubber layer of rubber pad and interface briquetting bottom, realize the protection to the fuselage, prevent to take place the friction, lead to aircraft fuselage surface impaired.

Description

Unmanned aerial vehicle transportation bracket

Technical Field

The utility model belongs to the technical field of the unmanned aerial vehicle transportation, concretely relates to unmanned aerial vehicle transports bracket.

Background

An unmanned aircraft, referred to as "drone", is an unmanned aircraft that is operated by a radio remote control device and a self-contained program control device, or is operated autonomously, either completely or intermittently, by an onboard computer. Unmanned aerial vehicles can be classified into military and civil applications according to the application field. For military use, unmanned aerial vehicles divide into reconnaissance aircraft and target drone. In the civil aspect, the unmanned aerial vehicle + industry application is the real new need of the unmanned aerial vehicle, relates to sensor technology, communication technology, information processing technology, intelligent control technology, aviation power propulsion technology and the like, and is a product with high technical content in the modern era. The unmanned aerial vehicle has the value of forming an aerial platform, is combined with other parts for expanding application, and replaces human beings to finish aerial operation. With the gradual maturity of unmanned aerial vehicle research and development technology, the manufacturing cost is greatly reduced, the unmanned aerial vehicle is widely applied in various fields, besides military application, the unmanned aerial vehicle also comprises civil fields such as agricultural plant protection, electric power inspection, police law enforcement, geological exploration, environment monitoring, forest fire prevention and film and television aerial photography, the application field of the unmanned aerial vehicle is rapidly expanded, and the unmanned aerial vehicle can be classified into different categories according to different scenes, platforms and application modes, such as application scenes, flight platforms, control modes, sight distances, weight scales, task heights, activity radiuses and the like. The general aviation administration of China divides unmanned aerial vehicles into six types of I, II, IV, XI and X according to weight 1.5KG, 7KG, 25KG, 150KG and 5700 KG. Plant protection type unmanned aerial vehicle belongs to V class, and unmanned dirigible belongs to VI class, and beyond visual range unmanned aerial vehicle belongs to I class. In actual operation, I, II, IHI, IV, XI and XII are classified.

The FXX-B/WYX-1 transportation device is suitable for domestic transportation of an unmanned aerial vehicle platform and security equipment of the FXX system. FXX-B/WYX-1 transportation device is suitable for placing decomposed aircraft parts (such as a fuselage, wings, vertical tails, nose cones and an airspeed tube) during transition transportation, and the FXX transportation device adopts an exposed form to transport an unmanned aerial vehicle (the unmanned aerial vehicle is decomposed into 1 pair of wing bodies, 2 pairs of vertical tails and 1 pair of nose cone assemblies), is provided with a special bracket fixing wing body, and is provided with a special packing box for fixing 2 pairs of vertical tails and the nose cone assemblies (comprising the airspeed tube).

At present, current unmanned aerial vehicle's conveyer, the measure that mostly does not possess the fixed point to the aircraft and carry out the protection, and do not go forward to relax the measure to all junctions, at the in-process of transportation, can be because vibrations or jolt for the junction appears not hard up, leads to the fixed point of transportation frame and aircraft to produce friction or collision, leads to aircraft surface to damage, for this we propose an unmanned aerial vehicle transportation bracket.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an unmanned aerial vehicle transportation bracket to propose current unmanned aerial vehicle's conveyer in solving above-mentioned background art, do not possess the measure of protecting the fixed point of aircraft mostly, and do not go on relaxing the measure to all junctions, at the in-process of transportation, can perhaps because vibrations or jolt, make the junction appear not hard up, lead to the fixed point of transportation frame and aircraft to produce friction or collision, lead to the problem of aircraft surface damage.

In order to achieve the above object, the utility model provides a following technical scheme: an unmanned aerial vehicle transportation bracket comprises a bracket frame, a fixed seat and a packaging box, wherein a plurality of transverse rods are arranged inside the frame body of the bracket frame, the transverse rods are fixedly arranged inside the bracket frame in a welding mode, longitudinal rods are also arranged inside the frame body of the bracket frame, the longitudinal rods are fixedly arranged inside the frame body of the bracket frame in a welding mode, the transverse rods and the longitudinal rods are arranged in a crossed mode, a fixed frame is arranged at the crossed position of the transverse rods and the longitudinal rods, the fixed frame is fixedly arranged at the crossed position of the transverse rods and the longitudinal rods in a welding mode, reinforcing ribs are arranged on one side of the fixed frame, the fixed frame is of a cylinder structure, a fixed seat is arranged at the top of the fixed frame, the fixed seat is fixedly arranged inside the fixed frame in a welding mode, a rubber pad is arranged at the top of the fixed seat in a gluing mode, the two adjacent sides of the fixing seat are respectively provided with a side plate, an adjusting bolt is arranged on the outer side of each side plate and is in threaded connection with the side plates, one end of each adjusting bolt penetrates through the side plate to extend to the other side of each side plate, a connector pressing block is arranged at the top of the rubber pad, a rubber layer is arranged at the bottom of each connector pressing block, pre-tightening bolts are arranged on the two sides of the top of the fixing seat, the top ends of the pre-tightening bolts penetrate through the rubber pad and the connector pressing blocks to extend to the tops of the connector pressing blocks, and the top ends of the pre-tightening bolts are provided with compression nuts which are in threaded connection with the pre-tightening bolts.

The working principle of the technical scheme is as follows:

the aircraft body of the aircraft is lifted by the aircraft hanger and slowly hung and placed on the structure between the two fixing frames, so that the aircraft is completely attached and kept stable, the aircraft hanger is in a straightening slight stress state at the moment, the aircraft body is slightly moved, the supporting structure below the aircraft body is stably contacted with the rubber pad at the top of the fixing seat, the interface pressing block is pushed to move towards the direction of the airplane body by sequentially rotating the two adjusting bolts, the supporting structure below the airplane is pressed below the interface pressing block, the pressing nut is arranged on the pre-tightening bolt, so that two ends of the interface pressing block can be in close contact with the rubber pad, thereby compressing the supporting structures at the two sides of the machine body, realizing the fixation of a plurality of joints of the interface pressing block, meanwhile, the protection of the airplane body is realized through the rubber pad arranged on the bottom of the connector pressing block and the rubber layer arranged on the bottom of the connector pressing block, and the airplane body surface damage caused by friction is prevented.

In a further technical scheme, a packing box is arranged at one end of the inner side of the bracket frame, buckles are arranged on two sides of the outer portion of the packing box, the packing box is fixedly bound with one end of the inner side of the bracket frame through a tensioning belt, bottom foam is arranged at the bottom end of the inner portion of the packing box, side foam is arranged on two sides of the inner portion of the packing box, the side foam is fixedly arranged on two sides of the inner portion of the packing box, end foam is arranged at two ends of the inner portion of the packing box, the end foam is fixedly arranged at two ends of the inner portion of the packing box, compression foam is arranged at the middle end of the inner portion of the packing box, the compression foam is fixedly arranged at the middle end of the inner portion of the packing box, and cover plate foam is arranged at the top of the packing box.

Through the packing box that is equipped with, and set up the side foam respectively at the inside inner wall of packing box, end foam and end foam, realize protecting the spare part that the aircraft decomposed the part, prevent in the transportation, the collision takes place, the spare part that leads to the aircraft is impaired, influence and the integrality of part structure, through the apron foam that is equipped with, realize protecting the top of packing box, through the foam that compresses tightly that is equipped with, come to compress tightly the spare part that the packing box was inside to be placed, prevent to take place to rock, cause the damage to aircraft spare part.

In a further technical scheme, a front support block is arranged between two fixing frames with the same longitudinal position at one end, close to the packaging box, of the bracket frame, two sides of the front support block are fixedly installed between the two fixing frames through installed installation screws, and a rubber layer is arranged at the top of the front support block.

The front end of the airplane body is supported through the front supporting block, and the surface of the airplane body is protected through the rubber layer arranged at the top of the front supporting block.

In a further technical scheme, a rear supporting block is arranged between two fixing frames which are arranged at the same longitudinal position and are far away from one end of the front supporting block on the bracket frame, two sides of the rear supporting block are fixedly arranged between the two fixing frames through arranged mounting screws, and a rubber layer is arranged at the top of the rear supporting block.

The rear end of the airplane body is supported through the rear supporting block, so that the rear end of the airplane body can be completely attached to the airplane body, and the surface of the airplane body is protected by matching with the rubber layer arranged at the top of the rear supporting block.

In a further technical scheme, the surface of end foam is equipped with the recess, the shape of recess is the same with unmanned aerial vehicle's vertical fin shape size.

Through the recess that is equipped with, the recess can be seted up according to aircraft spare part's shape to guarantee the inside that spare part can laminate the recess completely, thereby guarantee the stability of spare part, play the guard action.

In a further technical scheme, the two sides of the two ends of the bottom of the bracket frame are respectively provided with a support, and the supports are fixedly arranged at the bottom of the bracket frame in a welding mode.

Through the support that is equipped with, support the bottom of bracket frame, guarantee the stability of bracket frame, prevent direct and ground contact.

In a further technical scheme, mooring rings are arranged on the periphery of the top of the bracket frame and are fixedly installed on the periphery of the top of the bracket frame through installed mounting screws.

Through the mooring ring that is equipped with, realize hanging the bracket frame to carry it, convenient operation.

Compared with the prior art, the beneficial effects of the utility model are that:

1. the aircraft body of the aircraft is lifted by the aircraft hanger and slowly hung and placed on the structure between the two fixing frames, so that the aircraft is completely attached and kept stable, the aircraft hanger is in a straightening slight stress state at the moment, the aircraft body is slightly moved, the supporting structure below the aircraft body is stably contacted with the rubber pad at the top of the fixing seat, the interface pressing block is pushed to move towards the direction of the airplane body by sequentially rotating the two adjusting bolts, the supporting structure below the airplane is pressed below the interface pressing block, the pressing nut is arranged on the pre-tightening bolt, so that two ends of the interface pressing block can be in close contact with the rubber pad, thereby compressing the supporting structures at the two sides of the machine body, realizing the fixation of a plurality of joints of the interface pressing block, meanwhile, the protection of the airplane body is realized through the rubber pad arranged on the bottom of the connector pressing block and the rubber layer arranged on the bottom of the connector pressing block, and the airplane body is prevented from being damaged due to friction.

2. Through the packing box that is equipped with, and set up the side foam respectively at the inside inner wall of packing box, end foam and end foam, realize protecting the spare part that the aircraft decomposed the part, prevent in the transportation, the collision takes place, the spare part that leads to the aircraft is impaired, influence and the integrality of part structure, through the apron foam that is equipped with, realize protecting the top of packing box, through the foam that compresses tightly that is equipped with, come to compress tightly the spare part that the packing box was inside to be placed, prevent to take place to rock, cause the damage to aircraft spare part.

Drawings

Fig. 1 is a schematic view of the overall structure of the present invention;

fig. 2 is a schematic top view of the present invention;

fig. 3 is a left side schematic view of the present invention;

fig. 4 is a right side schematic view of the present invention;

fig. 5 is a schematic diagram of the front end structure of the present invention.

In the figure: 1. a bracket frame; 2. a cross bar; 3. a longitudinal bar; 4. a mooring ring; 5. a fixed mount; 6. a rear supporting block; 7. a fixed seat; 8. a rubber pad; 9. packing cases; 10. side foam; 11. compacting the foam; 12. a base foam; 13. an interface pressing block; 14. adjusting the bolt; 15. a support; 16. a front support block; 17. end foam; 18. a groove; 19. cover plate foam; 20. and (5) pressing the nut.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative work belong to the protection scope of the present invention.

Please refer to fig. 1-5, the utility model provides an unmanned aerial vehicle transportation bracket technical scheme: the packaging box comprises a bracket frame 1, a fixed seat 7 and a packaging box 9, wherein a plurality of transverse rods 2 are arranged inside the frame body of the bracket frame 1, the transverse rods 2 are fixedly arranged inside the bracket frame 1 in a welding mode, longitudinal rods 3 are also arranged inside the frame body of the bracket frame 1, the longitudinal rods 3 are fixedly arranged inside the frame body of the bracket frame 1 in a welding mode, the transverse rods 2 and the longitudinal rods 3 are arranged in a crossed mode, a fixed seat 5 is arranged at the crossed position of the transverse rods 2 and the longitudinal rods 3, the fixed seat 5 is fixedly arranged at the crossed position of the transverse rods 2 and the longitudinal rods 3 in a welding mode, one side of the fixed seat 5 is provided with a reinforcing rib, the fixed seat 5 is of a cylinder structure, the fixed seat 7 is arranged at the top of the fixed seat 5, the fixed seat 7 is fixedly arranged inside the fixed seat 5 in a welding mode, the top of the fixed seat 7 is provided with a rubber pad 8, the rubber pad 8 is fixedly arranged at the top of the fixed seat 7 in a gluing mode, two adjacent sides of the fixed seat 7 are provided with side plates, adjusting bolt 14 is arranged on the outer side of the side plate, adjusting bolt 14 is in threaded connection with the side plate, one end of adjusting bolt 14 penetrates through the side plate and extends to the other side of the side plate, an interface pressing block 13 is arranged at the top of rubber pad 8, a rubber layer is arranged at the bottom of interface pressing block 13, pre-tightening bolts are arranged on two sides of the top of fixing base 7, the top ends of the pre-tightening bolts penetrate through rubber pad 8 and interface pressing block 13 and extend to the top of interface pressing block 13, and a compression nut 20 is arranged on the top ends of the pre-tightening bolts and is in threaded connection with the pre-tightening bolts.

The working principle of the technical scheme is as follows:

in the embodiment, the aircraft body of the aircraft is lifted by the aircraft hanger and slowly hung on the structure between the two fixing frames 5 to be completely attached and kept stable, at the moment, the aircraft hanger is in a straightening slight stress state, the aircraft body is slightly moved to ensure that the supporting structure below the aircraft body is stably contacted with the rubber pad 8 at the top of the fixing base 7, the interface pressing block 13 is pushed to move towards the aircraft body by sequentially rotating the adjusting bolts 14, the supporting structure below the aircraft is pressed below the interface pressing block 13, the gland nut 20 is installed on the pre-tightening bolt to ensure that two ends of the interface pressing block 13 can be tightly contacted with the rubber pad 8 so as to tightly press the supporting structures at two sides of the aircraft body, thereby realizing the fixation of a plurality of joints of the interface pressing block 13, and simultaneously realizing the protection of the aircraft body by the rubber pad 8 arranged at the bottom of the interface pressing block 13 and the rubber layer arranged at the bottom of the interface pressing block 13, preventing the occurrence of friction, resulting in damage to the surface of the aircraft fuselage.

In further technical scheme, the inboard one end of bracket frame 1 is equipped with packing box 9, the outside both sides of packing box 9 are equipped with the buckle, packing box 9 is fixed through the taut area that is equipped with bindes the inboard one end with bracket frame 1, the inside bottom of packing box 9 is equipped with end foam 12, end foam 12 is placed in the inside bottom of packing box 9, the inside both sides of packing box 9 are equipped with side foam 10, side foam 10 is fixed to be placed in the inside both sides of packing box 9, the inside both ends of packing box 9 are equipped with end foam 17, end foam 17 is fixed to be placed in the inside both ends of packing box 9, the inside middle-end of packing box 9 is equipped with compresses tightly foam 11, compress tightly foam 11 and fix the inside middle-end of placing in packing box 9, the top of packing box 9 is equipped with apron foam 19.

In this embodiment, through the packing box 9 that is equipped with, and set up side foam 10 respectively at the inside inner wall of packing box 9, end foam 17 and end foam 12, realize protecting the spare part of aircraft decomposition part, prevent in the transportation, the collision takes place, the spare part that leads to the aircraft is impaired, influence and part structure's integrality, apron foam 19 through being equipped with, realize protecting the top of packing box 9, foam 11 compresses tightly through being equipped with, come to compress tightly the spare part of 9 inside places of packing box, prevent to take place to rock, cause the damage to aircraft spare part.

In a further technical scheme, a front supporting block 16 is arranged between two fixing frames 5 with the same longitudinal position at one end, close to a packing box 9, of a bracket frame 1, two sides of the front supporting block 16 are fixedly arranged between the two fixing frames 5 through arranged mounting screws, and a rubber layer is arranged at the top of the front supporting block 16.

In this embodiment, the front end of the aircraft body is supported by the front support block 16, and the surface of the aircraft body is protected by the rubber layer arranged on the top of the front support block 16.

In a further technical scheme, a rear supporting block 6 is arranged between two fixing frames 5 which are the same in longitudinal position and at one end, far away from a front supporting block 16, of a bracket frame 1, two sides of the rear supporting block 6 are fixedly arranged between the two fixing frames 5 through arranged mounting screws, and a rubber layer is arranged at the top of the rear supporting block 6.

In this embodiment, through the back tray 6 that is equipped with, hold up the rear end of aircraft fuselage, make it can laminate completely with the fuselage, cooperate the rubber layer that 6 tops of back tray set up, realize the protection to aircraft fuselage surface.

In a further technical scheme, the surface of bottom foam 12 is provided with recess 18, and the shape of recess 18 is the same with unmanned aerial vehicle's vertical fin shape size.

In this embodiment, through the recess 18 that is equipped with, recess 18 can be seted up according to aircraft parts's shape to guarantee that parts can laminate the inside of recess 18 completely, thereby guarantee parts's stability, play the guard action.

In a further technical scheme, both sides at the two ends of the bottom of the bracket frame 1 are provided with supports 15, and the supports 15 are fixedly arranged at the bottom of the bracket frame 1 in a welding mode.

In this embodiment, support 15 through being equipped with comes to hold up the support to the bottom of bracket frame 1, guarantees bracket frame 1's stability, prevents direct and ground contact.

In a further technical scheme, the periphery of the top of the bracket frame 1 is provided with a mooring ring 4, and the mooring ring 4 is fixedly arranged on the periphery of the top of the bracket frame 1 through an arranged mounting screw.

In this embodiment, through the mooring ring 4 that is equipped with, realize hanging bracket frame 1 to carry it, convenient operation.

Although embodiments of the present invention have been shown and described, it will be appreciated by those skilled in the art that changes, modifications, substitutions and alterations can be made in these embodiments without departing from the principles and spirit of the invention, the scope of which is defined in the appended claims and their equivalents.

Claims

1. The utility model provides an unmanned aerial vehicle transportation bracket, includes bracket frame (1), fixing base (7) and packing box (9), its characterized in that: the support frame is characterized in that a plurality of transverse rods (2) are arranged inside a frame body of the support frame (1), the transverse rods (2) are fixedly arranged inside the support frame (1) in a welding mode, longitudinal rods (3) are further arranged inside the frame body of the support frame (1), the longitudinal rods (3) are fixedly arranged inside the frame body of the support frame (1) in a welding mode, the transverse rods (2) and the longitudinal rods (3) are arranged in a crossed mode, fixing frames (5) are arranged at crossed positions of the transverse rods (2) and the longitudinal rods (3) in a crossed mode, the fixing frames (5) are fixedly arranged at crossed positions of the transverse rods (2) and the longitudinal rods (3) in a welding mode, reinforcing ribs are arranged on one side of each fixing frame (5), the fixing frames (5) are of cylinder structures, fixing seats (7) are arranged at the tops of the fixing frames (5), and the fixing seats (7) are fixedly arranged inside the fixing frames (5) in a welding mode, the top of the fixed seat (7) is provided with a rubber pad (8), the rubber pad (8) is fixedly arranged on the top of the fixed seat (7) in a gluing way, two adjacent sides of the fixed seat (7) are respectively provided with a side plate, the outer side of each side plate is provided with an adjusting bolt (14), the adjusting bolt (14) is in screw connection with the side plate, one end of the adjusting bolt (14) penetrates through the side plate and extends to the other side of the side plate, the top of the rubber pad (8) is provided with an interface pressing block (13), the bottom of the interface pressing block (13) is provided with a rubber layer, two sides of the top of the fixed seat (7) are provided with pre-tightening bolts, the top ends of the pre-tightening bolts penetrate through the rubber gasket (8) and the interface pressing block (13) and extend to the top of the interface pressing block (13), and a compression nut (20) is arranged at the top end of the pre-tightening bolt, and the compression nut (20) is in threaded connection with the pre-tightening bolt.

2. An unmanned aerial vehicle transportation carriage as defined in claim 1, wherein: the packaging box is characterized in that a packaging box (9) is arranged at one end of the inner side of the bracket frame (1), buckles are arranged on two sides of the outer portion of the packaging box (9), the packaging box (9) is fixedly bound with one end of the inner side of the bracket frame (1) through a tensioning belt, bottom foam (12) is arranged at the bottom end of the inner portion of the packaging box (9), the bottom foam (12) is placed at the bottom end of the inner portion of the packaging box (9), side foam (10) is arranged on two sides of the inner portion of the packaging box (9), the side foam (10) is fixedly placed on two sides of the inner portion of the packaging box (9), end foam (17) is arranged at two ends of the inner portion of the packaging box (9), the end foam (17) is fixedly placed at two ends of the inner portion of the packaging box (9), a compression foam (11) is arranged at the middle end of the inner portion of the packaging box (9), the compression foam (11) is fixedly placed at the middle end of the inner portion of the packaging box (9), and cover plate foam (19) is arranged at the top of the packing box (9).

3. An unmanned aerial vehicle transport carriage as defined in claim 2, wherein: the packaging box is characterized in that a front supporting block (16) is arranged between two fixing frames (5) which are identical in longitudinal position and close to one end of the packaging box (9) of the supporting frame (1), two sides of the front supporting block (16) are fixedly arranged between the two fixing frames (5) through mounting screws, and a rubber layer is arranged at the top of the front supporting block (16).

4. An unmanned aerial vehicle transportation carriage as defined in claim 3, wherein: the supporting frame is characterized in that a rear supporting block (6) is arranged between two fixing frames (5) which are the same in longitudinal position and far away from one end of the front supporting block (16) of the supporting frame (1), two sides of the rear supporting block (6) are fixedly arranged between the two fixing frames (5) through mounting screws, and a rubber layer is also arranged at the top of the rear supporting block (6).

5. An unmanned aerial vehicle transport carriage as defined in claim 2, wherein: the surface of end foam (12) is equipped with recess (18), the shape of recess (18) is the same with unmanned aerial vehicle's vertical fin shape size.

6. An unmanned aerial vehicle transportation carriage as defined in claim 1, wherein: both sides at bracket frame (1) bottom both ends all are equipped with support (15), support (15) are fixed to be set up in the bottom of bracket frame (1) through the welded mode.

7. An unmanned aerial vehicle transportation carriage as defined in claim 1, wherein: the novel bracket is characterized in that mooring rings (4) are arranged on the periphery of the top of the bracket frame (1), and the mooring rings (4) are fixedly arranged on the periphery of the top of the bracket frame (1) through mounting screws.