Conveyor

Abstract

The utility model discloses a conveyor, which relates to the technical field of logistics transportation, and comprises a base, a first telescopic rod piece positioned on the base and used for lifting articles, and a support piece arranged at the front end of the first telescopic rod piece, a second telescopic rod piece used for enabling the first telescopic rod piece to rotate around the rotating piece is arranged between the first telescopic rod piece and the base. The supporting piece comprises a supporting seat and a plurality of supporting legs arranged below the supporting seat, and the upper ends of the supporting legs are rotationally connected with the supporting seat; wherein the first telescopic rod piece comprises a telescopic rod and a sleeve arranged on the telescopic rod in a sleeving mode, a sliding way is arranged on the inner side wall of the sleeve, and a transmission assembly used for driving the telescopic rod piece to slide on the sliding way is arranged in the sleeve. The use scene of the transporter is expanded by achieving the length and transportation of the transportation line, and the stability in the transportation process is improved by arranging the supporting pieces.

Description

Technical Field

[0001] This utility model relates to the field of logistics and transportation technology, specifically to a transport aircraft. Background Technology

[0002] In recent years, the logistics industry has developed rapidly, and the demand for transportation equipment has been increasing. Among these demands, improving transportation efficiency and stability in complex environments and terrains, such as docks, factories, and mountainous areas, has become a major challenge for the industry. While traditional incline transport vehicles have solved the problem of changing the height of cargo transport to some extent, they still have significant limitations.

[0003] First, most traditional inclined transport aircraft have a fixed tilt angle, making them unable to adjust to changes in terrain or actual needs. This results in a low matching rate for transport, requiring the purchase of new models whenever the transport height changes, limiting their operational scenarios. Second, traditional inclined transport aircraft have limited transport line length, making it difficult to meet the needs of long-distance or varied terrain transport. Finally, traditional inclined transport aircraft lack effective support structures, causing a significant reduction in the weight the transport line can bear as the transport length increases, increasing the risk of tipping over and compromising transport safety. Utility Model Content

[0004] This application provides a transport aircraft that can solve the technical problems existing in the prior art, such as the inability to adjust the transport angle, the limited transport scenarios, and the poor stability during the transport process.

[0005] This application provides a transport machine, including: a base; and a first telescopic rod located on the base for lifting items, one end of the first telescopic rod being provided with a rotating member for rotatably connecting to the base, and a second telescopic rod being provided between the first telescopic rod and the base for realizing the first telescopic rod rotating around the rotating member; a support member provided at the front end of the first telescopic rod, the support member including a support base and a plurality of support legs provided below the support base, and the upper ends of the support legs being rotatably connected to the support base; wherein, the first telescopic rod includes a telescopic rod and a sleeve sleeved on the telescopic rod, and a slide rail is provided on the inner side wall of the sleeve, and a transmission assembly for driving the telescopic rod to slide on the slide rail is provided inside the sleeve.

[0006] In one embodiment, the first telescopic rod further includes: an elastic roller for supporting an article, the elastic roller being extended or retracted from the sleeve as the telescopic rod extends or retracts, the elastic roller being located at the end of the telescopic rod away from the support member.

[0007] In one embodiment, the first telescopic rod further includes a first roller for resisting the elastic roller as it retracts into the sleeve. The first roller is located at the opening of the sleeve and resists the elastic roller as the telescopic rod retracts into the sleeve.

[0008] In one embodiment, a belt for transporting goods is tensioned on the outer surface of the first telescopic rod, the belt being tensioned on the outer surface of the sleeve, the bottom surface of the telescopic rod, and the top of the elastic roller as the telescopic rod extends and retracts in a direction away from the sleeve.

[0009] In one embodiment, the second telescopic rod includes: a rotating assembly and a sliding assembly disposed between the rotating assembly. The rotating assembly includes a first rotating rod rotatably connected to the sleeve and a second rotating rod rotatably connected to the base. The sliding assembly includes a sleeve and a sleeve sleeved on the sleeve. One end of the sleeve is fixedly connected to the first rotating rod, and one end of the sleeve is fixedly connected to the second rotating rod.

[0010] In one embodiment, the second telescopic rod further includes: a telescopic column for driving the sleeve rod to slide within the sleeve and a connecting rod for connecting the telescopic column and the sleeve rod, one end of the telescopic column being fixedly connected to the first rotating rod or the second rotating rod, and the other end of the telescopic column being fixedly connected to the connecting rod.

[0011] In one embodiment, the support further includes a support rod and a support cylinder sleeved on the support rod, wherein the support cylinder is provided with a support spring for elastic connection between the support rod and the support cylinder.

[0012] In one embodiment, the support further includes a limiting rod for limiting the angle at which the support leg opens around the support base, wherein the opposite ends of the limiting rod are fixedly connected to the support rod and the support leg, respectively, and the support leg rotates around the support base as the support rod moves.

[0013] In one embodiment, the support further includes a connecting assembly for fixing the support base to the first telescopic rod and a shock-absorbing spring, wherein the shock-absorbing spring is sandwiched between the support base and the connecting assembly.

[0014] In one embodiment, the connecting assembly includes: a connecting slide rail for fixed connection with the first telescopic rod and a connecting block for slidable connection with the connecting slide rail, wherein the connecting slide rail is provided with a connecting groove, the connecting block is fixedly connected to the side of the support seat away from the shock-absorbing spring, and the connecting block is slidably installed in the connecting groove.

[0015] The beneficial effects of the technical solutions provided in this application include:

[0016] In this embodiment, by setting two telescopic rods, the first telescopic rod can extend the transport line length of the transport machine, enabling the transport machine to meet the transport requirements of various lengths or terrains, thus enriching the application scenarios of the transport machine. At the same time, the second telescopic rod can extend and retract to drive the first telescopic rod to rotate around the rotating component, thereby adjusting the transport angle of the transport machine. This allows the transport machine to be adjusted according to the terrain or other usage needs of the actual use scenario, improving the matching rate of the transport machine. Furthermore, a support member is set at the first telescopic rod to provide support for the transport machine and the transported goods when the transport line length of the transport machine is extended, improving the stability of the transport machine and ensuring safety during the transport process. Attached Figure Description

[0017] To more clearly illustrate the technical solutions in the embodiments of this application, the accompanying drawings used in the description of the embodiments will be briefly introduced below. Obviously, the accompanying drawings described below are only some embodiments of this application. For those skilled in the art, other drawings can be obtained based on these drawings without creative effort.

[0018] Figure 1 This is a schematic diagram of the structure of a transport aircraft provided in one embodiment of this application;

[0019] Figure 2 This is a structural schematic diagram of a first telescopic rod provided in an embodiment of this application;

[0020] Figure 3 This is a structural schematic diagram of the belt and roller winding method in the first telescopic rod provided in an embodiment of this application;

[0021] Figure 4 This is a schematic diagram of the structure of an elastic roller provided in one embodiment of this application;

[0022] Figure 5 This is a structural schematic diagram of the second telescopic rod provided in an embodiment of this application;

[0023] Figure 6 This is a schematic diagram of the structure of a support member provided in one embodiment of this application;

[0024] Figure 7 This is a schematic diagram of the structure of a connecting slide rail provided in one embodiment of this application;

[0025] Figure 8 This is a schematic diagram of the structure of a connecting block provided in an embodiment of this application;

[0026] Figure 9 This is a schematic diagram of the structure of a base provided in one embodiment of this application.

[0027] In the diagram: 1. Base; 11. Base rod; 12. Crossbar; 2. First telescopic rod; 21. Rotating component; 22. Telescopic rod; 23. Sleeve; 24. Slide rail; 241. Second roller; 25. Transmission assembly; 251. Gear; 252. Chain; 253. Connector; 254. Gear groove; 26. Elastic roller; 261. Elastic element; 262. Elastic cylinder; 263. Connector; 27. First roller; 28. Support roller; 291. Driving roller; 292. Driven roller; 3. 2. Telescopic rods; 31. First rotating rod; 32. Second rotating rod; 33. Sleeve rod; 34. Sleeve tube; 35. Telescopic column; 36. Connecting rod; 37. Fixing ring; 4. Support component; 41. Support seat; 42. Support leg; 421. Round head buckle; 422. Foot pad; 43. Support rod; 44. Support cylinder; 45. Support spring; 46. Limiting rod; 47. Connecting assembly; 471. Connecting slide rail; 472. Connecting block; 48. Shock-absorbing spring; 49. Upper support column; 5. Hydraulic oil pump. Detailed Implementation

[0028] To enable those skilled in the art to better understand the present application, the technical solutions in the embodiments of the present application will be clearly and completely described below with reference to the accompanying drawings. Obviously, the described embodiments are only some embodiments of the present application, and not all embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative effort are within the scope of protection of the present application.

[0029] This application provides a transport aircraft that can solve the technical problems existing in the prior art, such as the inability to adjust the transport angle, the limited transport scenarios, and the poor stability during the transport process.

[0030] Figure 1 This is a schematic diagram of the structure of a transport aircraft provided in one embodiment of this application. Figure 2 This is a structural schematic diagram of a first telescopic rod provided in an embodiment of this application. Figure 6 This is a schematic diagram of the structure of a support member provided in an embodiment of this application.

[0031] Reference Figure 1 , Figure 2 and Figure 6This application provides a transport machine, including: a base 1; and a first telescopic rod 2 located on the base 1 for lifting items, one end of the first telescopic rod 2 is provided with a rotating member 21 for rotatably connecting to the base 1, and a second telescopic rod 3 is provided between the first telescopic rod 2 and the base 1 for realizing the rotation of the first telescopic rod 2 around the rotating member 21; a support member 4 is provided at the front end of the first telescopic rod 2, the support member 4 includes a support seat 41 and a plurality of support legs 42 provided below the support seat 41, and the upper end of the support legs 42 is rotatably connected to the support seat 41; wherein, the first telescopic rod 2 includes a telescopic rod 22 and a sleeve 23 sleeved on the telescopic rod 22, and a slide 24 is provided on the inner side wall of the sleeve 23, and a transmission assembly 25 for driving the telescopic rod 22 to slide on the slide 24 is provided inside the sleeve 23.

[0032] Figure 9 This is a schematic diagram of the structure of a base 1 provided in one embodiment of this application. (Refer to reference...) Figure 1 and Figure 9 Specifically, the base 1 also includes a base rod 11 and a cross rod 12, which are inserted together to form the base 1, improving the structural stability of the base 1, so that the base 1 is sufficient to support the first telescopic rod 2 and the second telescopic rod 3.

[0033] In one embodiment of this application, the rotating component 21 is a bearing, and a hollow sheet metal is fixedly connected to the base 1. The first telescopic rod 2 is rotatably connected to the base 1 via the bearing. The second telescopic rod 3 is rotatably connected to the base 1 and the first telescopic rod 2 via the bearing and the hollow sheet metal, respectively. In some other embodiments of this application, other rotatable connection methods may be used, which are not limited here.

[0034] Figure 4 This is a schematic diagram of the structure of an elastic roller 26 provided in one embodiment of this application. (Refer to reference...) Figure 1 , Figure 2 and Figure 4 In one embodiment of this application, the first telescopic rod 2 further includes an elastic roller 26 for supporting the article. The elastic roller 26 pops out or retracts into the sleeve 23 as the telescopic rod 22 extends or retracts. The elastic roller 26 is located at the end of the telescopic rod 22 away from the support member 4.

[0035] Specifically, the elastic roller 26 includes an elastic cylinder 262, a connector 263, an elastic element 261, and an elastic groove. The elastic element 261 is fixed between the elastic cylinders 262 by the connector 263, and the elastic element 261 slides into or out of the elastic groove as the telescopic rod 22 extends and retracts.

[0036] In this embodiment, the transmission assembly 25 includes gears 251, a chain 252, and a connector 253. The telescopic rod 22 is fixedly connected to the chain 252 inside the sleeve 23 via the connector 253. Two gears 251 are disposed in the gear 251 grooves. The chain 252 guides the telescopic rod 22 to slide on the slide rail 24 through the rotation of the gears 251. A second roller 241 is provided on the slide rail 24 to assist the sliding of the telescopic rod 22.

[0037] In one embodiment of this application, the first telescopic rod 2 further includes a first roller 27 for resisting the elastic roller 26 as it retracts into the sleeve 23. The first roller 27 is located at the opening of the sleeve 23 and resists the elastic roller 26 as the telescopic rod 22 retracts into the sleeve 23.

[0038] Specifically, multiple elastic rollers 26 are arranged at intervals at the end of the telescopic rod 22 away from the support member 4. The elastic rollers 26 support the items for transport on the belt. When the telescopic rod 22 extends out of the sleeve 23, the elastic rollers 26 can sequentially pop out of the sleeve 23 to lift the belt and assist in transportation. When the telescopic rod 22 retracts into the sleeve 23, it shortens back into the sleeve 23 under the resistance of the first roller 27, so as not to affect transportation.

[0039] In one embodiment of this application, a belt for transporting goods is tensioned on the outer surface of the first telescopic rod 2. The belt is tensioned on the outer surface of the sleeve 23, the bottom surface of the telescopic rod 22, and the top of the elastic roller 26 as the telescopic rod 22 extends and retracts in a direction away from the sleeve 23.

[0040] Specifically, the bottom surface of the telescopic boom 22 is provided with a support roller 28, which can assist the belt in conveying on the telescopic boom 22. The first telescopic boom 2 can extend the transport line length of the transport machine, enabling the transport machine to meet the transport requirements of various lengths or terrains, and making the use scenarios of the transport machine more diverse.

[0041] Figure 3 This is a structural schematic diagram of the belt and roller winding method in the first telescopic rod 2 provided in an embodiment of this application. (Refer to reference...) Figure 1 , Figure 2 and Figure 3 The drive roller 291 is electrically connected to the motor, thereby providing power for the transport of the first telescopic rod 22 and the extension and retraction of the telescopic rod 22. At the same time, the axes of the multiple driven rollers 292 are parallel to each other, and the shortening of the distance between the driven rollers 292 makes the distance between the belts stored on the surface shorter, and the distance of the belt on the surface becomes longer as the telescopic rod 22 extends.

[0042] Figure 5 This is a structural schematic diagram of the second telescopic member 3 provided in an embodiment of this application. (Refer to the reference...) Figure 1 and Figure 5In one embodiment of this application, the second telescopic rod 3 includes: a rotating assembly and a sliding assembly disposed between the rotating assembly. The rotating assembly includes a first rotating rod 31 rotatably connected to the sleeve 23 and a second rotating rod 32 rotatably connected to the base 1. The sliding assembly includes a sleeve 33 and a sleeve 34 sleeved on the sleeve 33. One end of the sleeve 33 is fixedly connected to the first rotating rod 31, and one end of the sleeve 34 is fixedly connected to the second rotating rod 32.

[0043] The first rotating rod 31 and the second rotating rod 32 are hollow base rods 11, which can realize the stable installation between the second telescopic rod 3, the first telescopic rod 2 and the base 1, making the overall structure of the transport aircraft more stable.

[0044] In one embodiment of this application, the second telescopic rod 3 further includes: a telescopic column 35 for driving the sleeve rod 33 to slide within the sleeve 34 and a connecting rod 36 for connecting the telescopic column 35 and the sleeve rod 33. One end of the telescopic column 35 is fixedly connected to the first rotating rod 31 or the second rotating rod 32, and the other end of the telescopic column 35 is fixedly connected to the connecting rod 36.

[0045] Specifically, in this embodiment, the second telescopic rod 3 may include multiple sleeves 33 and multiple sleeves 34, with each sleeve 33 and sleeve 34 corresponding one-to-one. One sleeve 33 slides within one sleeve 34. One end of the sleeve 33 is fixedly connected to either the first rotating rod 31 or the second rotating rod 32, and the other end is fixedly connected to either the second rotating rod 32 or the first rotating rod 31. One end of the sleeve 34 is fixedly connected to either the first rotating rod 31 or the second rotating rod 32, and the other end is fixedly connected to either the second rotating rod 32 or the first rotating rod 31. A connecting rod 36 connects all the sleeves 33 to the telescopic column 35, and the sleeves 33 slide within the sleeve 23 under the telescopic action of the telescopic column 35. In some embodiments of this application, the connecting rod 36 may also connect all the sleeves 34 to the sleeves 33, as long as the telescopic action of the second telescopic rod 3 drives the rotation of the first telescopic rod 2; this is not limited here.

[0046] In this embodiment, a fixing ring 37 is also provided, which connects multiple sleeves 34 and telescopic columns 35 respectively, thereby making the overall structure of the second telescopic rod 3 more stable.

[0047] The telescopic column 35 can be a hydraulic telescopic column. This embodiment also includes a hydraulic oil pump 5, which is electrically connected to the telescopic column 35. The hydraulic oil pump 5 drives the telescopic column 35 to extend and retract, thereby causing the first telescopic rod 2 to rotate around the rotating member 21. The angle between the first telescopic rod 2 and the base 1 changes, allowing the transport vehicle to be adjusted according to the terrain or other usage requirements of the actual application scenario, thus improving the transport vehicle's compatibility.

[0048] Continue to refer to Figure 1 and Figure 6 In one embodiment of this application, the support member 4 further includes: a support rod 43 and a support cylinder 44 sleeved on the support rod 43, wherein the support cylinder 44 is provided with a support spring 45 for elastic connection between the support rod 43 and the support cylinder 44.

[0049] Support component 4 can provide support for the transport aircraft and the transported goods when the transport line length of the transport aircraft is extended, thereby improving the stability of the transport aircraft and ensuring safety during the transport process.

[0050] In one embodiment of this application, the support member 4 further includes a limiting rod 46 for limiting the angle of the support leg 42 around the support base 41. The two opposite ends of the limiting rod 46 are fixedly connected to the support rod 43 and the support leg 42, respectively. The support leg 42 rotates around the support base 41 as the support rod 43 moves.

[0051] The support end of the support leg 42 is equipped with a round-headed buckle 421 and a foot pad 422. The round-headed buckle 421 and the foot pad 422 can cooperate with each other to make the support end of the support leg 42 stably supported, thereby making the transport machine stand up stably.

[0052] Specifically, both ends of the limiting rod 46 are provided with collars. One end of the limiting rod 46 is fixedly connected to the support cylinder 44 through the collar, and the other end of the limiting rod 46 is fixedly connected to the support leg 42 through the collar, thereby limiting the change of the opening angle of the support leg 42.

[0053] In one embodiment of this application, the support member 4 further includes a connecting assembly 47 for fixing the support base 41 to the first telescopic rod 2 and a shock-absorbing spring 48, wherein the shock-absorbing spring 48 is sandwiched between the support base 41 and the connecting assembly 47.

[0054] Specifically, the shock-absorbing spring 48 and the upper support column 49 connect the support base 41 and the connecting assembly 47. The setting of the upper support column 49 makes the connection between the support base 41 and the connecting assembly 47 more secure. The shock-absorbing spring 48 can keep the transport machine stable and prevent deformation, keep the structure from deforming, and further improve the safety during transportation.

[0055] Figure 7 This is a schematic diagram of the structure of the connecting slide rail 471 provided in one embodiment of this application. Figure 8 This is a schematic diagram of the structure of a connecting block 472 provided in an embodiment of this application. (Refer to the reference...) Figure 6 , Figure 7 and Figure 8In one embodiment of this application, the connecting component 47 includes: a connecting slide rail 471 for fixed connection with the first telescopic rod 2 and a connecting block 472 for sliding connection with the connecting slide rail 471. The connecting slide rail 471 is provided with a connecting groove. The connecting block 472 is fixedly connected to the side of the support base 41 away from the shock-absorbing spring 48. The connecting block 472 is slidably installed in the connecting groove.

[0056] In this embodiment, by setting two telescopic rods, the first telescopic rod can extend the transport line length of the transport machine, enabling the transport machine to meet the transport requirements of various lengths or terrains, thus enriching the application scenarios of the transport machine. At the same time, the second telescopic rod can extend and retract to drive the first telescopic rod to rotate around the rotating component, thereby adjusting the transport angle of the transport machine. This allows the transport machine to be adjusted according to the terrain or other usage needs of the actual use scenario, improving the matching rate of the transport machine. Furthermore, a support member is set at the first telescopic rod to provide support for the transport machine and the transported goods when the transport line length of the transport machine is extended, improving the stability of the transport machine and ensuring safety during the transport process.

[0057] In the description of this application, it should be noted that the terms "upper," "lower," etc., indicating the orientation or positional relationship are based on the orientation or positional relationship shown in the accompanying drawings, and are only for the convenience of describing this application and simplifying the description, and do not indicate or imply that the device or element referred to must have a specific orientation, or be constructed and operated in a specific orientation, and therefore should not be construed as a limitation of this application. Unless otherwise expressly specified and limited, the terms "installed," "connected," and "linked" should be interpreted broadly. For example, they can refer to a fixed connection, a detachable connection, or an integral connection; they can refer to a mechanical connection or an electrical connection; they can refer to a direct connection or an indirect connection through an intermediate medium; they can refer to the internal communication between two elements. For those skilled in the art, the specific meaning of the above terms in this application can be understood according to the specific circumstances.

[0058] It should be noted that in this application, relational terms such as "first" and "second" are used merely to distinguish one entity or operation from another, and do not necessarily require or imply any such actual relationship or order between these entities or operations. Furthermore, the terms "comprising," "including," or any other variations thereof are intended to cover non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements includes not only those elements but also other elements not expressly listed, or elements inherent to such a process, method, article, or apparatus. Without further limitations, an element defined by the phrase "comprising one..." does not exclude the presence of other identical elements in the process, method, article, or apparatus that includes said element.

[0059] The above description is merely a specific embodiment of this application, enabling those skilled in the art to understand or implement this application. Various modifications to these embodiments will be readily apparent to those skilled in the art, and the general principles defined herein may be implemented in other embodiments without departing from the spirit or scope of this application. Therefore, this application is not to be limited to the embodiments shown herein, but is to be accorded the widest scope consistent with the principles and novel features claimed herein.

Claims

1. A transport aircraft, characterized in that, include: Base (1); as well as A first telescopic rod (2) is located on the base (1) for lifting items. One end of the first telescopic rod (2) is provided with a rotating part (21) for rotatably connecting the base (1). A second telescopic rod (3) is provided between the first telescopic rod (2) and the base (1) for realizing the rotation of the first telescopic rod (2) around the rotating part (21). A support member (4) is provided at the front end of the first telescopic rod (2). The support member (4) includes a support base (41) and a plurality of support legs (42) provided below the support base (41). The upper end of the support leg (42) is rotatably connected to the support base (41). The first telescopic rod (2) includes a telescopic rod (22) and a sleeve (23) sleeved on the telescopic rod (22). The inner side wall of the sleeve (23) is provided with a slide (24). The sleeve (23) is provided with a transmission assembly (25) for driving the telescopic rod (22) to slide on the slide (24).

2. The transport aircraft according to claim 1, characterized in that, The first telescopic member (2) further includes: An elastic roller (26) for supporting an item, the elastic roller (26) pops out or retracts into the sleeve (23) as the telescopic rod (22) extends or retracts, the elastic roller (26) is located at the end of the telescopic rod (22) away from the support member (4).

3. The transport aircraft according to claim 2, characterized in that, The first telescopic member (2) further includes: A first roller (27) for resisting the elastic roller (26) as it retracts into the sleeve (23) is provided at the opening of the sleeve (23). The first roller (27) resists the elastic roller (26) as the telescopic rod (22) retracts into the sleeve (23).

4. The transport aircraft according to claim 3, characterized in that, The outer surface of the first telescopic rod (2) is tensioned with a belt for transporting goods. The belt is tensioned on the outer surface of the sleeve (23), the bottom surface of the telescopic rod (22), and the top of the elastic roller (26) as the telescopic rod (22) extends and retracts away from the sleeve (23).

5. The transport aircraft according to claim 1, characterized in that, The second telescopic member (3) includes: The rotating assembly includes a rotating component and a sliding component disposed between the rotating components. The rotating component includes a first rotating rod (31) rotatably connected to the sleeve (23) and a second rotating rod (32) rotatably connected to the base (1). The sliding component includes a sleeve rod (33) and a sleeve (34) sleeved on the sleeve rod (33). One end of the sleeve rod (33) is fixedly connected to the first rotating rod (31), and one end of the sleeve (34) is fixedly connected to the second rotating rod (32).

6. The transport aircraft according to claim 5, characterized in that, The second telescopic member (3) also includes: A telescopic column (35) for driving the sleeve rod (33) to slide inside the sleeve (34) and a connecting rod (36) for connecting the telescopic column (35) and the sleeve rod (33). One end of the telescopic column (35) is fixedly connected to the first rotating rod (31) or the second rotating rod (32), and the other end of the telescopic column (35) is fixedly connected to the connecting rod (36).

7. The transport aircraft according to claim 1, characterized in that, The support member (4) also includes: A support rod (43) and a support cylinder (44) sleeved on the support rod (43), wherein a support spring (45) is provided inside the support cylinder (44) for elastic connection between the support rod (43) and the support cylinder (44).

8. The transport aircraft according to claim 7, characterized in that, The support member (4) also includes: A limiting rod (46) is used to limit the angle of the support leg (42) around the support base (41). The two opposite ends of the limiting rod (46) are fixedly connected to the support rod (43) and the support leg (42) respectively. The support leg (42) rotates around the support base (41) as the support rod (43) moves.

9. The transport aircraft according to claim 8, characterized in that, The support member (4) also includes: A connecting assembly (47) for fixing the support base (41) to the first telescopic rod (2) and a shock-absorbing spring (48), wherein the shock-absorbing spring (48) is sandwiched between the support base (41) and the connecting assembly (47).

10. The transport aircraft according to claim 9, characterized in that, The connection component (47) includes: A connecting slide rail (471) for fixed connection with the first telescopic rod (2) and a connecting block (472) for sliding connection with the connecting slide rail (471). The connecting slide rail (471) is provided with a connecting groove. The connecting block (472) is fixedly connected to the side of the support base (41) away from the shock-absorbing spring (48). The connecting block (472) is slidably installed in the connecting groove.

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