CN220996768U - Light fixed wing aircraft wing conveyer - Google Patents
Light fixed wing aircraft wing conveyer Download PDFInfo
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- CN220996768U CN220996768U CN202322546829.9U CN202322546829U CN220996768U CN 220996768 U CN220996768 U CN 220996768U CN 202322546829 U CN202322546829 U CN 202322546829U CN 220996768 U CN220996768 U CN 220996768U
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- 230000003014 reinforcing effect Effects 0.000 claims abstract description 20
- 230000000149 penetrating effect Effects 0.000 claims abstract description 5
- 238000000034 method Methods 0.000 abstract description 9
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Abstract
The utility model provides a light fixed-wing aircraft wing transportation device, which comprises: a frame for constructing a main body structure of a wing transport device for a light fixed wing aircraft; the first vertical supporting rod is fixed in the middle of the frame through a three-way connecting piece and used for reinforcing the frame; the second vertical supporting rod is fixed at one end of the frame through a three-way connecting piece and is parallel to the first vertical supporting rod and used for reinforcing the frame; the third vertical supporting rod is fixed at the other end of the frame through a three-way connecting piece and is parallel to the first vertical supporting rod and used for reinforcing the frame; the diagonal brace is fixed on the diagonal direction of the rectangular frame with smaller area formed by the second vertical brace and the edge of the frame and is used for preventing the frame from deforming; the transverse long rod is arranged on the opposite side edges of the frame and is perpendicular to the first vertical supporting rod and used for reinforcing the frame; the movable hanging frame is fixedly connected above the frame in a penetrating way and is used for hanging the wing. The utility model solves the problems of complicated ground transportation loading procedures, long time consumption, safety guarantee and the like of the wings of the light fixed-wing aircraft.
Description
Technical Field
The embodiment of the utility model relates to the technical field of aircraft disassembly and assembly, in particular to a light fixed wing aircraft wing transportation device.
Background
Fixed wing aircraft are widely used because of their wide range of applications and areas of use. However, the ground transportation of the light fixed-wing aircraft is lack of a general wing transportation mode at present, and the transportation is mainly carried out after the large-scale trailer is bound and fixed, so that the transportation mode has the defects of collision and the like on the wing, and the damage to the wing is easy to cause. Therefore, developing a light-weight fixed-wing aircraft wing transportation device can effectively overcome the defects in the related art, and the technical problem to be solved is urgent in the industry.
Disclosure of utility model
Aiming at the problems existing in the prior art, the embodiment of the utility model provides a light fixed-wing aircraft wing transportation device.
In a first aspect, embodiments of the present utility model provide a lightweight fixed wing aircraft wing transport device comprising: a frame 1 for constructing a main structure of a wing transport device of a light fixed-wing aircraft; the first vertical supporting rod 2 is fixed in the middle of the frame 1 through a three-way connecting piece and is used for reinforcing the frame 1; the second vertical supporting rod 3 is fixed at one end of the frame 1 through a three-way connecting piece and is parallel to the first vertical supporting rod 2 and used for reinforcing the frame 1; the third vertical supporting rod 4 is fixed at the other end of the frame 1 through a three-way connecting piece and is parallel to the first vertical supporting rod 2 and used for reinforcing the frame 1; diagonal brace 5 fixed on diagonal direction of rectangular frame with smaller area formed by second vertical brace 3 and edge of frame 1, for preventing frame 1 from deforming; the transverse long rods 6 are arranged on the opposite sides of the frame 1 and are perpendicular to the first vertical supporting rods 2, and are used for reinforcing the frame 1; the movable hanging frame 7 is fixedly connected above the frame 1 in a penetrating way and is used for hanging wings.
Based on the foregoing embodiment, the light-duty fixed-wing aircraft wing transportation device provided in the embodiment of the present utility model further includes: the first lower supporting leg 8 is fixedly arranged at one end of the bottom of the frame 1 and is used for bearing and fixing the front end of the lower edge of the wing.
Based on the foregoing embodiment, the light fixed wing aircraft wing transportation device provided in the embodiment of the present utility model includes: the second lower supporting leg 9 is fixedly arranged at the other end of the bottom of the frame 1 and is used for bearing and fixing the front end of the lower edge of the wing.
Based on the foregoing embodiment, the light-duty fixed-wing aircraft wing transportation device provided in the embodiment of the present utility model further includes: the transverse short rod 10 is riveted on the frame 1 and used for fixing the frame 1 and mounting the wing.
Based on the foregoing embodiment, the light-duty fixed-wing aircraft wing transportation device provided in the embodiment of the present utility model further includes: and the bolt 11 is arranged on one side of the transverse short rod 10 and is used for rapidly detaching the wing hook.
Referring to fig. 2, based on the foregoing embodiment, in the light-duty fixed wing aircraft wing transportation device provided in the embodiment of the present utility model, the frame 1 is divided into left and right parts, and the space is 10 cm to 15 cm wider than the thickness of the wing.
According to the light fixed wing aircraft wing transportation device provided by the embodiment of the utility model, the three-way connecting piece is effectively fixedly connected with each supporting rod, and the device structure can be adjusted according to the wing surface specification, so that the purpose of safe and rapid transportation, loading and unloading is achieved, the problems of complicated ground transportation and loading procedures, long time consumption, safety guarantee and the like of the light fixed wing aircraft wing are solved, and the light fixed wing aircraft wing transportation device is used for constructing a main body structure of the light fixed wing aircraft wing transportation device through the frame 1; the first vertical supporting rod 2 is fixed in the middle of the frame 1 through a three-way connecting piece and is used for reinforcing the frame 1; the second vertical supporting rod 3 is fixed at one end of the frame 1 through a three-way connecting piece and is parallel to the first vertical supporting rod 2 and used for reinforcing the frame 1; the third vertical supporting rod 4 is fixed at the other end of the frame 1 through a three-way connecting piece and is parallel to the first vertical supporting rod 2 and used for reinforcing the frame 1; diagonal brace 5 fixed on diagonal direction of rectangular frame with smaller area formed by second vertical brace 3 and edge of frame 1, for preventing frame 1 from deforming; the transverse long rods 6 are arranged on the opposite sides of the frame 1 and are perpendicular to the first vertical supporting rods 2, and are used for reinforcing the frame 1; the movable hanging frame 7 is fixedly connected above the frame 1 in a penetrating way and is used for hanging wings. It is possible to.
Drawings
In order to more clearly illustrate the embodiments of the present utility model or the technical solutions in the prior art, a brief description will be given below of the drawings required for the embodiments or the prior art descriptions, and it is obvious that the drawings in the following description are some embodiments of the present utility model, and other drawings may be obtained according to these drawings without any inventive effort for a person skilled in the art.
FIG. 1 is a schematic view of a light fixed wing aircraft wing transport device according to an embodiment of the present utility model;
Fig. 2 is a schematic structural view of another light-duty fixed-wing aircraft wing transportation device according to an embodiment of the present utility model.
Detailed Description
For the purpose of making the objects, technical solutions and advantages of the embodiments of the present utility model more apparent, the technical solutions of the embodiments of the present utility model will be clearly and completely described below with reference to the accompanying drawings in the embodiments of the present utility model, and it is apparent that the described embodiments are some embodiments of the present utility model, but not all embodiments of the present utility model. All other embodiments, which can be made by those skilled in the art based on the embodiments of the utility model without making any inventive effort, are intended to be within the scope of the utility model. In addition, the technical features of each embodiment or the single embodiment provided by the utility model can be combined with each other at will to form a feasible technical scheme, and the combination is not limited by the sequence of steps and/or the structural composition mode, but is necessarily based on the fact that a person of ordinary skill in the art can realize the combination, and when the technical scheme is contradictory or can not realize, the combination of the technical scheme is not considered to exist and is not within the protection scope of the utility model claimed.
The embodiment of the utility model provides a light fixed wing aircraft wing transportation device, referring to fig. 1 and 2, comprising: a frame 1 for constructing a main structure of a wing transport device of a light fixed-wing aircraft; the first vertical supporting rod 2 is welded in the middle of the frame 1 and used for reinforcing the frame 1; the second vertical supporting rod 3 is fixed at one end of the frame 1 through a three-way connecting piece and is parallel to the first vertical supporting rod 2 and used for reinforcing the frame 1; the third vertical supporting rod 4 is fixed at the other end of the frame 1 through a three-way connecting piece and is parallel to the first vertical supporting rod 2 and used for reinforcing the frame 1; diagonal brace 5 fixed on diagonal direction of rectangular frame with smaller area formed by second vertical brace 3 and edge of frame 1, for preventing frame 1 from deforming; the transverse long rods 6 are arranged on the opposite sides of the frame 1 and are perpendicular to the first vertical supporting rods 2, and are used for reinforcing the frame 1; the movable hanging frame 7 is fixedly connected above the frame 1 in a penetrating way and is used for hanging wings.
Referring to fig. 2, on the basis of the foregoing embodiment, the light fixed-wing aircraft wing transportation device provided in the embodiment of the present utility model further includes: the first lower supporting leg 8 is fixedly arranged at one end of the bottom of the frame 1 and is used for bearing and fixing the front end of the lower edge of the wing.
Referring to fig. 2, on the basis of the foregoing embodiment, a light fixed-wing aircraft wing transportation device provided in an embodiment of the present utility model includes: the second lower supporting leg 9 is fixedly arranged at the other end of the bottom of the frame 1 and is used for bearing and fixing the front end of the lower edge of the wing.
Referring to fig. 2, on the basis of the foregoing embodiment, the light fixed-wing aircraft wing transportation device provided in the embodiment of the present utility model further includes: the transverse short rod 10 is fixed on the frame 1 through a three-way connecting piece and is used for fixing the frame 1 and mounting the wing.
Referring to fig. 2, on the basis of the foregoing embodiment, the light fixed-wing aircraft wing transportation device provided in the embodiment of the present utility model further includes: and the bolt 11 is arranged on one side of the transverse short rod 10 and is used for rapidly detaching the wing hook.
Referring to fig. 2, on the basis of the above embodiment, in the light fixed wing aircraft wing transportation device provided in the embodiment of the present utility model, the frame 1 is divided into left and right parts, and the space is 10 cm to 15 cm wider than the thickness of the wing.
According to the light fixed wing aircraft wing transportation device provided by the embodiment of the utility model, the three-way connecting piece is effectively fixedly connected with each supporting rod, and the device structure can be adjusted according to the wing surface specification, so that the purposes of safe and rapid transportation, loading and unloading are achieved, and the problems of complicated ground transportation and loading procedures, long time consumption, safety guarantee and the like of the light fixed wing aircraft wing are solved.
The apparatus embodiments described above are merely illustrative, wherein the elements illustrated as separate elements may or may not be physically separate, and the elements shown as elements may or may not be physical elements, may be located in one place, or may be distributed over a plurality of network elements. Some or all of the modules may be selected according to actual needs to achieve the purpose of the solution of this embodiment. Those of ordinary skill in the art will understand and implement the present invention without undue burden.
It should be noted that the terms "comprises," "comprising," or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus. Without further limitation, an element defined by the phrase "comprising … …" does not exclude the presence of other like elements in a process, method, article, or apparatus that comprises the element.
Finally, it should be noted that: the above embodiments are only for illustrating the technical solution of the present utility model, and are not limiting; although the utility model has been described in detail with reference to the foregoing embodiments, it will be understood by those of ordinary skill in the art that: the technical scheme described in the foregoing embodiments can be modified or some technical features thereof can be replaced by equivalents; such modifications and substitutions do not depart from the spirit and scope of the technical solutions of the embodiments of the present utility model.
Claims (6)
1. A lightweight fixed wing aircraft wing transport device, comprising: a frame (1) for constructing a main structure of a wing transport device of a light fixed-wing aircraft; the first vertical supporting rod (2) is welded in the middle of the frame (1) and used for reinforcing the frame (1); the second vertical supporting rod (3) is fixed at one end of the frame (1) through a three-way connecting piece and is parallel to the first vertical supporting rod (2) and used for reinforcing the frame (1); the third vertical supporting rod (4) is fixed at the other end of the frame (1) through a three-way connecting piece and is parallel to the first vertical supporting rod (2) and used for reinforcing the frame (1); the diagonal brace (5) is fixed on the diagonal direction of a rectangular frame with smaller area formed by the second vertical brace (3) and the edge of the frame (1) and is used for preventing the frame (1) from deforming; the transverse long rod (6) is arranged on the opposite side edges of the frame (1) and is perpendicular to the first vertical supporting rod (2) and used for reinforcing the frame (1); the movable hanging frame (7) is fixedly connected above the frame (1) in a penetrating way and is used for hanging wings.
2. The lightweight fixed wing aircraft wing transport device of claim 1, further comprising: the first lower supporting leg (8) is fixedly arranged at one end of the bottom of the frame (1) and used for bearing and fixing the front end of the lower edge of the wing.
3. The lightweight fixed wing aircraft wing transport device of claim 2, wherein the device comprises: the second lower supporting leg (9) is fixedly arranged at the other end of the bottom of the frame (1) and is used for bearing and fixing the front end of the lower edge of the wing.
4. The lightweight fixed wing aircraft wing transport device of claim 3, further comprising: the transverse short rod (10) is fixed on the frame (1) through a three-way connecting piece and is used for fixing the frame (1) and mounting the wing.
5. The lightweight fixed wing aircraft wing transport device of claim 4, further comprising: the bolt (11) is arranged on one side of the transverse short rod (10) and is used for rapidly releasing the wing hooks.
6. The transport device for a light fixed wing aircraft wing according to claim 5, wherein the frame (1) is divided into left and right parts, and the distance between the left and right parts is 10 cm to 15 cm wider than the thickness of the wing.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322546829.9U CN220996768U (en) | 2023-09-19 | 2023-09-19 | Light fixed wing aircraft wing conveyer |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN202322546829.9U CN220996768U (en) | 2023-09-19 | 2023-09-19 | Light fixed wing aircraft wing conveyer |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN220996768U true CN220996768U (en) | 2024-05-24 |
Family
ID=91092805
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN202322546829.9U Active CN220996768U (en) | 2023-09-19 | 2023-09-19 | Light fixed wing aircraft wing conveyer |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN220996768U (en) |
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2023
- 2023-09-19 CN CN202322546829.9U patent/CN220996768U/en active Active
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