Aircraft folding and unfolding device carried on storage and transportation platform

Abstract

The invention discloses an aircraft folding and unfolding device carried on a storage and transportation platform, which belongs to the technical field of ocean exploration and comprises a traction device, a slide rail support frame, a plurality of slide rails and a pressing beam. The traction device is arranged on the storage and transportation platform and used for dragging the aircraft; the sliding rail supporting frame is arranged on the inner bottom face of the storage and transportation platform and can be driven by the hydraulic device to longitudinally move along the storage and transportation platform and move up and down along the storage and transportation platform at the same time. The sliding rail is arranged on the sliding rail supporting frame in the longitudinal direction of the storage and transportation platform and used for guiding and limiting the aircraft. The pressing beam is arranged at the top end of the storage and transportation platform and used for pressing the aircraft on the top. The aircraft can accurately enter and exit from the storage and transportation platform in the laying and recycling process, stable supporting is provided for the aircraft, meanwhile, collision between the aircraft and the storage and transportation platform is avoided, and therefore the aircraft is protected against damage.

Description

Technical Field

[0001] The present invention belongs to the technical field of ocean exploration, and in particular relates to a vehicle retracting and launching device carried on a storage and transportation platform. Background Art

[0002] With the widespread application of aircraft in the development of the ocean, the deployment and recovery technology of aircraft is also constantly changing. There are many ways to deploy and recover aircraft carried on mother ships. Among them, the deployment and recovery device carried on the storage and transportation platform has the advantages of more flexible movement, small space occupation, simple operation and wide application range. The reasons are: (1) The storage and transportation platform is self-contained and occupies little space. It can be equipped with wheels to achieve amphibious operations. It can move independently in the dock of the mother ship, saving space occupation and improving the space utilization efficiency of the mother ship during operations; (2) The storage and transportation platform is easy to operate and only requires remote control to complete the deployment and recovery of the aircraft, with basically no need for human assistance.

[0003] However, the harsh conditions of the marine environment, such as the invasion and turbulence of waves and surges, make it easy for the aircraft to collide with the storage and transportation platform during and after the retrieval process. Especially for multi-appendage aircraft, since the outer circumference of the multi-appendage aircraft is equipped with multiple wing panels and other vulnerable parts, once a collision occurs, it will cause serious damage to the aircraft. At the same time, due to the limited internal space of the storage and transportation platform, the retrieval of multi-appendage aircraft is more challenging than that of non-appendage aircraft.

[0004] Therefore, ensuring that the multi-appendage vehicle accurately enters the storage and transportation platform and that the multi-appendage vehicle does not shake in the harsh ocean environment is crucial to protecting the vehicle from damage and ensuring its performance. Summary of the invention

[0005] In view of this, the present invention provides an aircraft retrieval device mounted on a storage and transportation platform, so that the aircraft can accurately enter and exit the storage and transportation platform during the deployment and recovery process, provide stable support for the aircraft, and avoid collision between the aircraft and the storage and transportation platform, thereby protecting the aircraft from damage.

[0006] The present invention is achieved through the following technical solutions:

[0007] A vehicle stowage and release device mounted on a storage and transportation platform comprises: a traction device, a slide rail support frame, a plurality of slide rails and a pressure beam;

[0008] The traction device is arranged on the storage and transportation platform and is used for traction of the aircraft;

[0009] The slide rail support frame is arranged on the inner bottom surface of the storage and transportation platform, and the slide rail support frame can move vertically along the storage and transportation platform while being driven by the hydraulic device;

[0010] The slide rail is arranged on the slide rail support frame along the longitudinal direction of the storage and transportation platform, and is used to provide guidance and limit for the aircraft;

[0011] The pressure beam is arranged at the top of the storage and transportation platform and is used to form a pressure on the aircraft at the top.

[0012] Further, the traction device includes: a traction winch, a traction cable and a latch;

[0013] The traction winch is arranged at the head of the top of the storage and transportation platform;

[0014] One end of the traction cable is connected to the traction winch, and the other end is detachably connected to the head of the top end of the traction winch through a latch;

[0015] The traction winch and the latch are arranged in parallel along the transverse direction of the storage and transportation platform, so that the traction cable forms a loop for hooking the hook on the head of the aircraft.

[0016] Further, two telescopic releases are included;

[0017] The two telescopic releasers are respectively arranged on the two tailgates of the storage and transportation platform;

[0018] The telescopic releaser comprises: a spring switch and a rotating tongue;

[0019] The rotating tongue is stuck by the spring switch and remains in a closed state; when the spring in the spring switch is compressed to a limited position, the rotating tongue opens;

[0020] The traction cable between the traction winch and the latch is locked in the rotating tongue of the telescopic release;

[0021] When the towing cable hooks the hook of the spacecraft, the pulling force of the spacecraft triggers the spring switch, opens the tongue, and releases the lock on the towing cable.

[0022] Furthermore, the slide rail support frame also includes: a connecting rod, two guide rods and two support rod groups;

[0023] The two support rod groups are arranged symmetrically with the longitudinal center line of the storage and transportation platform as the symmetry axis; each support rod group is composed of a number of support rods arranged at intervals along the longitudinal direction, and the bottom end surface of each support rod is hinged to the inner bottom surface of the storage and transportation platform;

[0024] A guide rod is hinged at the upper end of each support rod group; the heads of the two guide rods are connected by a connecting rod;

[0025] The fixed end of the hydraulic device is hinged to the inner bottom surface of the storage and transportation platform, and the actuating end of the hydraulic device is hinged to the connecting rod; the two guide rods are driven to move longitudinally along the storage and transportation platform by extending and retracting the actuating end of the hydraulic device;

[0026] Each guide rod is provided with the slide rail.

[0027] Furthermore, the tails of the two guide rods form a trumpet-shaped structure; and the trumpet-shaped structure of the guide rod is arranged obliquely downward.

[0028] Furthermore, the two support rod groups are arranged in an outward-facing "X" shape.

[0029] Furthermore, it also includes a limit block;

[0030] The limit block is arranged on the inner surface of the head of the storage and transportation platform to limit the head of the aircraft.

[0031] Furthermore, a plurality of lifting mechanisms are arranged between the pressure beam and the storage and transportation platform.

[0032] Furthermore, the driving and lifting mechanisms of the traction device and the hydraulic device are all controlled by remote control.

[0033] Furthermore, the lower end surface of the pressure beam is an arc-shaped surface, which matches the back structure of the aircraft.

[0034] Beneficial effects:

[0035] (1) The present invention provides an aircraft retrieval and deployment device mounted on a storage and transportation platform. The hydraulic device drives the slide rail support frame to move vertically and horizontally along the storage and transportation platform while moving up and down, so that the aircraft can accurately enter the storage and transportation platform, avoiding the collision of the aircraft with the storage and transportation platform during the recovery and deployment process; the slide rail support frame is provided with a slide rail to facilitate the towing or release of the aircraft; as the slide rail support frame moves upward, the aircraft is pressed against the lower end surface of the pressure beam, so that the aircraft cannot be bumped and collided under the action of waves and surges, thereby protecting the aircraft from damage, meeting the diversified deployment and recovery requirements of aircraft in offshore operations, and having a safe, stable, simple and efficient implementation effect.

[0036] (2) The present invention provides a vehicle storage and launching device carried on a storage and transportation platform, wherein one end of a traction cable is connected to a traction winch, and the other end is detachably connected to the traction winch via a latch. When the vehicle is being recovered, the traction cable forms a loop to hook the hook on the head of the vehicle, and tows the vehicle to move to the slide rail support frame; when the vehicle is being deployed, the connection between the latch and the storage and transportation platform is released, so that the vehicle can smoothly enter the water along the slide rail support frame.

[0037] (3) The present invention provides an aircraft storage and release device carried on a storage and transportation platform, wherein a traction cable is hung on a telescopic releaser, and the traction cable can be stretched to both sides by the telescopic releaser to increase the size of the loop formed by the traction cable, so that the hook of the aircraft can easily enter the loop; by expanding the two tail doors outward, the distance between the two telescopic releasers can be increased, and the size of the loop can be further increased; the pulling force generated by the aircraft triggers the spring switch, opens the rotating tongue, releases the locking of the traction cable by the rotating tongue, and can retract the traction cable, thereby realizing the traction of the aircraft.

[0038] (4) The present invention provides an aircraft storage and deployment device carried on a storage and transportation platform, wherein the slide rail support frame includes two guide rods and two support rod groups. The two support rod groups are symmetrically arranged with the center line of the storage and transportation platform in the head and tail direction as the symmetry axis. The upper end face of each support rod group is hinged to a guide rod. The structure of the slide rail support frame can prevent the appendages on the aircraft from being bumped. The upper end of each support rod group is hinged to a guide rod. Each guide rod is provided with a slide rail. When the aircraft moves to the slide rail, the slide rail guides the aircraft so that the aircraft can move in a straight line along the slide rail. At the same time, the slide rail can form a preliminary limit on both sides of the abdomen of the aircraft to prevent the aircraft from deviating from the moving trajectory and bumping during recovery and deployment, and can perfectly avoid the aircraft's more fragile wing panels and other vulnerable components.

[0039] (5) In the present invention, a vehicle stowage and deployment device is mounted on a storage and transportation platform, wherein the tails of two guide rods form a trumpet-shaped structure to guide the vehicle so that the vehicle gradually moves along the guide rods from wide to narrow; further, the trumpet-shaped portion of the guide rod is arranged obliquely downward to prevent the vehicle from colliding with the end of the trumpet-shaped structure when entering the guide rail.

[0040] (6) In the aircraft storage and launching device mounted on a storage and transportation platform of the present invention, the two support rod groups are in an outward-facing "X" structure, which can prevent the appendages at the bottom of the aircraft from colliding with the support rod groups and being damaged.

[0041] (7) In the present invention, a spacer for storing and releasing an aircraft mounted on a storage and transportation platform has a limit block disposed at the head of the storage and transportation platform to prevent the head of the aircraft from colliding with the head of the storage and transportation platform and causing damage.

[0042] (8) In the present invention, a spacecraft stowage and deployment device mounted on a storage and transportation platform has a plurality of lifting mechanisms disposed between a pressure beam and the storage and transportation platform, which can realize the lifting and lowering of the pressure beam and avoid collision between the appendages on the top of the spacecraft and the pressure beam during the deployment and recovery of the spacecraft.

[0043] (9) In the present invention, a vehicle retrieval and deployment device mounted on a storage and transportation platform, the driving and lifting mechanisms of the traction device and the hydraulic device are all controlled by remote control, so that the device is suitable for offshore operations and long-distance recovery and deployment of the vehicle.

[0044] (10) In the aircraft stowage and deployment device mounted on a storage and transportation platform of the present invention, the lower end surface of the pressure beam is an arc-shaped surface, which matches the back structure of the aircraft, thereby improving the fixing effect of the aircraft. BRIEF DESCRIPTION OF THE DRAWINGS

[0045] Figure 1 It is a schematic diagram of the retractable device of the present invention in the aircraft deployment state;

[0046] Figure 2 It is a schematic diagram of the retractable device of the present invention in the aircraft storage state;

[0047] Figure 3 It is a front view of the retractable device of the present invention;

[0048] Among them, 1-traction device, 101-traction winch, 102-traction cable, 103-pin, 2-slide rail support frame, 201-guide rod, 202-support rod, 203-hydraulic device, 3-slide rail, 4-pressure beam, 5-storage and transportation platform, 6-vehicle, 601-hook, 7-limit block. DETAILED DESCRIPTION

[0049] The present invention is described in detail below with reference to the accompanying drawings and embodiments.

[0050] Embodiment 1:

[0051] This embodiment provides an aircraft storage and deployment device mounted on a storage and transportation platform, which is arranged on the storage and transportation platform 5 (which is a frame structure).

[0052] like Figure 1 and Figure 2 As shown, the retracting and releasing device includes: a traction device 1, a slide rail support frame 2, a plurality of slide rails 3, a pressure beam 4 and a limit block 7.

[0053] The stopper 7 is arranged on the inner surface of the head of the storage and transportation platform 5, and is used for limiting the position of the aircraft when it is recovered. The stopper 7 is made of a buffer material, and in this embodiment, the material of the stopper is preferably rubber.

[0054] like Figure 3 As shown, the traction device 1 includes: a traction winch 101 , a traction cable 102 and a latch 103 .

[0055] The traction winch 101 is arranged at the top of the storage and transportation platform 5 (i.e. Figure 1 on the right side of the image).

[0056] One end of the traction cable 102 is wound around the traction winch 101, and the other end is detachably connected to the top head of the storage and transportation platform 5 through a latch 103. Figure 3As shown, the traction winch 101 and the latch 103 are along Figure 3 The traction cables 102 are arranged in parallel in the left and right directions (lateral directions) in the vessel 6, so that the traction cables 102 form a loop for hooking the hook 601 at the head of the vessel 6, and the vessel 6 is towed by the traction winch 101. In this embodiment, the traction cables 102 are preferably low-density and high-strength polypropylene filament cables, which have a strength that can meet the traction strength of the vessel 6, float on the water surface, and hook the hook 601 on the vessel 6. The laying length of the traction cables 102 is adjusted by the traction winch 101.

[0057] The slide rail support frame 2 is arranged on the inner bottom surface of the storage and transportation platform 5, and includes: a connecting rod, a hydraulic device 203, two guide rods 201 and two support rod groups.

[0058] The two support rod groups are arranged symmetrically with the longitudinal center line (along the head-to-tail direction) of the storage and transportation platform 5 as the symmetry axis. Each support rod group is composed of a plurality of support rods 202 arranged at intervals along the longitudinal direction, and the bottom end surface of each support rod 202 is hinged to the inner bottom surface of the storage and transportation platform 5.

[0059] As an example, the two support rod groups are arranged in an outward-facing "X" structure, which can prevent the appendages at the bottom of the aircraft 6 from colliding with the support rod groups and being damaged.

[0060] A guide rod 201 is hinged on the upper end surface of each support rod group. The tails of the two guide rods 201 form a trumpet-shaped structure to guide the aircraft 6. When recovering the aircraft 6, the aircraft 6 moves gradually from wide to narrow along the guide rod 201 through the trumpet-shaped structure at the tail of the guide rod 201 under the traction of the traction cable 102. When the aircraft 6 is slightly deflected, it also plays a role of correction and guidance. As an example, the trumpet-shaped structure is tilted downward to avoid damage to the end of the aircraft 6 that contacts the trumpet-shaped structure when entering the guide rail. The heads of the two guide rods 201 are connected by a connecting rod.

[0061] The fixed end of the hydraulic device 203 is hinged to the inner bottom surface of the storage and transportation platform 5, and the actuating end of the hydraulic device 203 is hinged to the connecting rod. The two guide rods 201 are driven to move forward and backward in the longitudinal direction by extending and retracting the actuating end of the hydraulic device 203, that is, when the actuating end of the hydraulic device 203 is extended, the two guide rods 201 move backward and downward at the same time, and extend out of the storage and transportation platform 5 from the tail of the storage and transportation platform 5, and when the actuating end of the hydraulic device 203 is retracted, the two guide rods 201 move forward and upward at the same time.

[0062] Each guide rod is provided with a slide rail 3 along the longitudinal direction of the storage and transportation platform 5. The slide rail 3 is a roller slide rail. When the aircraft 6 moves to the slide rail 3, the slide rail 3 guides the aircraft 6 and forms a preliminary limit on both sides of the belly of the aircraft 6; the aircraft 6 is pulled along the slide rail 3 by the pulling cable 102 until the head of the aircraft 6 hits the limit block 7.

[0063] The pressure beam 4 is arranged at the middle of the top of the storage and transportation platform 5. Figure 3 As shown, the lower end surface of the pressure beam 4 is an arc surface, which matches the back structure of the aircraft 6. When the aircraft 6 completely enters the internal space of the storage and transportation platform 5, the actuating end of the hydraulic device 203 is retracted, and the guide rod 201 of the slide rail support frame 2 moves forward and upward at the same time, and the aircraft 6 is pressed against the arc surface of the pressure beam 4 to prevent the aircraft 6 from shaking under the action of surges and colliding with the inner wall surface of the storage and transportation platform 5, causing damage.

[0064] As an example, a plurality of lifting mechanisms are provided between the pressure beam 4 and the storage and transportation platform 5. The lifting mechanism lifts the pressure beam 4, so that the pressure beam 4 and the top appendage of the aircraft 6 are prevented from colliding during the deployment and recovery of the aircraft 6; the lifting mechanism pulls the pressure beam 4 back and down, and the aircraft 6 after recovery is fixed between the pressure beam 4 and the slide rail 3, so that the aircraft 6 is prevented from shaking.

[0065] In this embodiment, the traction winch 101 is remotely controlled to retract and release the traction cable 102, insert and remove the latch 103, drive the hydraulic device 203, and drive the lifting mechanism of the pressure beam 4 to lift and lower, thereby realizing remote operation.

[0066] Working method:

[0067] When the aircraft 6 is located in the storage and transportation platform 5 and is in a storage state: the slide rail support frame 2 lifts the slide rail 3 to form a support on the belly of the aircraft 6, the pressure beam 4 embraces the aircraft 6 on the back of the aircraft 6, and the traction device 1 pulls the hook 601 on the head of the aircraft 6.

[0068] When it is necessary to deploy the aircraft 6: lift the pressure beam 4 on the top of the storage and transportation platform 5, start the hydraulic device 203 on the slide rail support frame 2, so that the aircraft 6 limited by the slide rail 3 moves backward along with the slide rail support frame 2 to extend out of the storage and transportation platform 5 and is released. During the movement of the slide rail support frame 2 toward the tail of the storage and transportation platform 5, the traction winch 101 releases the traction cable 102, and the aircraft 6 is released from the slide rail 3 and the latch 103 is pulled out, and the traction cable 102 is released from the hook 601 at the head of the aircraft 6. The aircraft 6 slides into the water along the slide rail 3.

[0069] When the aircraft 6 is recovered: the pin 103 at the end of the traction cable 102 is connected to the head at the top of the storage and transportation platform 5, so that the traction cable 102 forms a loop, and the traction winch 101 releases the traction cable 102 to the water surface. The aircraft 6 sinks and moves below the loop. After the traction cable 102 is hooked to the hook 601 at the head of the aircraft 6, the guide rod 201 provided with the slide rail 3 in the slide rail support frame 2 moves backward and downward under the drive of the hydraulic device 203, and extends out of the storage and transportation platform 5. At this time, the height of the slide rail 3 is lower than the belly of the aircraft 6, and the traction winch 101 begins to recover the traction cable 102, and the aircraft 6 moves smoothly to the top of the slide rail 3 along the guide rod 201. As the traction cable 102 shortens, the traction cable 102 pulls the aircraft 6 forward, and the aircraft 6 gradually enters and moves to the top of the slide rail 3 along the trumpet-shaped structure at the tail of the guide rod 201. At this time, the hydraulic device 203 drives the slide rail 3 to be lifted up to the height of the belly of the aircraft 6 along with the slide rail support frame 2, forming a limit on both sides of the front section of the belly of the aircraft 6. At this time, the traction winch 101 continues to recover the traction cable 102, and the aircraft 6 is translated along the slide rail 3 toward the head of the storage and transportation platform 5 under the traction of the traction cable 102. After the belly of the aircraft 6 falls into the slide rail 3 as a whole, the slide rail 3 and the aircraft 6 move upward while the slide rail support frame 2 moves forward. When the aircraft 6 moves into place (that is, the head of the aircraft 6 is against the limit block 7 at the head of the storage and transportation platform 5), the pressure beam 4 on the top of the storage and transportation platform 5 descends, forming a pressure on the aircraft 6 at the top, thereby fixing the aircraft 6.

[0070] Embodiment 2:

[0071] On the basis of the above-mentioned embodiment 1, the retractable device further includes: two telescopic releasers.

[0072] The rear portion of the storage and transportation platform 5 is provided with two tailgates.

[0073] The two telescopic releasers are respectively arranged at the ends of the two tailgates. The telescopic releaser comprises a spring switch and a rotating tongue. The rotating tongue is stuck by the spring switch and remains in a closed state; when the spring in the spring switch is compressed to a limited position, the rotating tongue opens.

[0074] The traction cable 102 between the traction winch 101 and the latch 103 is locked in the rotating tongue of the telescopic release. The telescopic release can stretch the traction cable 102 to both sides, enlarge the loop formed by the traction cable 102, and make it easier for the hook of the aircraft 6 to enter the loop. By expanding the two tailgates outward, the distance between the two telescopic releases can be increased, and the size of the loop can be further increased.

[0075] When the traction cable 102 is hooked on the hook of the aircraft 6, the tension generated by the aircraft 6 compresses the spring in the telescopic releaser to a limited position, opens the rotating tongue, and releases the locking of the traction cable 102 by the rotating tongue, thereby achieving traction.

[0076] In summary, the above are only preferred embodiments of the present invention and are not intended to limit the protection scope of the present invention. Any modifications, equivalent substitutions, improvements, etc. made within the spirit and principles of the present invention should be included in the protection scope of the present invention.

Claims

1. An aircraft stowage and unloading device mounted on a storage and transportation platform, characterized in that: include: A traction device (1), a slide rail support frame (2), a plurality of slide rails (3) and a pressure beam (4); The traction device (1) is arranged on the storage and transportation platform (5) and is used for traction of the aircraft; The slide rail support frame (2) is arranged on the inner bottom surface of the storage and transportation platform (5), and the slide rail support frame (2) can move vertically along the storage and transportation platform (5) while being driven by the hydraulic device (203); The slide rail (3) is arranged on the slide rail support frame (2) along the longitudinal direction of the storage and transportation platform (5) and is used to provide guidance and position limiting for the aircraft (6); The pressure beam (4) is arranged at the top of the storage and transportation platform (5) and is used to press the aircraft (6) at the top.

2. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in claim 1, characterized in that: The traction device (1) comprises: a traction winch (101), a traction cable (102) and a latch (103); The traction winch (101) is arranged at the head of the top of the storage and transportation platform (5); One end of the traction cable (102) is connected to the traction winch (101), and the other end is detachably connected to the head of the top end of the traction winch (101) via a latch (103); The traction winch (101) and the latch (103) are arranged in parallel along the transverse direction of the storage and transportation platform (5), so that the traction cable (102) forms a loop for hooking the hook (601) at the head of the aircraft (6).

3. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in claim 2, characterized in that: Also included are two telescopic releases; The two telescopic releasers are respectively arranged on two tailgates of the storage and transportation platform (5); The telescopic releaser comprises: a spring switch and a rotating tongue; The rotating tongue is stuck by the spring switch and remains in a closed state; when the spring in the spring switch is compressed to a limited position, the rotating tongue opens; The traction cable (102) between the traction winch (101) and the latch (103) is locked in the rotating tongue of the telescopic release; When the traction cable (102) is hooked on the hook of the aircraft (6), the pulling force of the aircraft (6) triggers the spring switch to open the rotating tongue, thereby releasing the lock of the traction cable (102).

4. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in claim 1, characterized in that: The slide rail support frame (2) further comprises: a connecting rod, two guide rods (201) and two support rod groups; The two support rod groups are arranged symmetrically with the longitudinal center line of the storage and transportation platform (5) as the symmetry axis; each support rod group is composed of a plurality of support rods (202) arranged at intervals along the longitudinal direction, and the bottom end surface of each support rod (202) is hinged to the inner bottom surface of the storage and transportation platform (5); A guide rod (201) is hingedly connected to the upper end of each support rod group; the heads of the two guide rods (201) are connected via a connecting rod; The fixed end of the hydraulic device (203) is hinged to the inner bottom surface of the storage and transportation platform (5), and the actuating end of the hydraulic device (203) is hinged to the connecting rod; the two guide rods (201) are driven to move longitudinally along the storage and transportation platform (5) by extending and retracting the actuating end of the hydraulic device (203); The slide rail (3) is arranged on each guide rod (201).

5. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in claim 4, characterized in that: The tails of the two guide rods (201) form a trumpet-shaped structure; the trumpet-shaped structure of the guide rod (201) is arranged obliquely downward.

6. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in claim 4 or 5, characterized in that: The two support rod groups are in an outward-facing "X" structure.

7. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in any one of claims 1 to 5, characterized in that: Also includes a limit block (7); The limit block (7) is arranged on the inner surface of the head of the storage and transportation platform (5) to limit the head of the aircraft (6).

8. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in any one of claims 1 to 5, characterized in that: A plurality of lifting mechanisms are arranged between the pressure beam (4) and the storage and transportation platform (5).

9. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in claim 8, characterized in that: The driving and lifting mechanisms of the traction device (1) and the hydraulic device (203) are all controlled by remote control.

10. The aircraft stowage and release device mounted on a storage and transportation platform as claimed in any one of claims 1 to 5, characterized in that: The lower end surface of the pressure beam (4) is an arc-shaped surface, which matches the back structure of the aircraft (6).

Images