CN220350438U

CN220350438U - Wing transportation bracket

Info

Publication number: CN220350438U
Application number: CN202322062332.XU
Authority: CN
Inventors: 魏昌进; 侯宝林; 杨超
Original assignee: Sichuan Hengshenglixun Intelligent Equipment Co ltd
Current assignee: Sichuan Hengshenglixun Intelligent Equipment Co ltd
Priority date: 2023-08-02
Filing date: 2023-08-02
Publication date: 2024-01-16
Anticipated expiration: 2033-08-02

Abstract

The utility model discloses a wing transportation bracket which comprises a rectangular supporting frame, an upper wing body joint fixing assembly, a lower wing body joint fixing assembly and a rear hanging point supporting and fixing assembly, wherein a wing placement frame strip groove is formed in the rectangular supporting frame, and a pair of large triangular support frames are arranged on two side frames at one end part of the wing placement frame strip groove; the outer bottom corner positions of the pair of large triangular supports are provided with lower wing body joint fixing assemblies, the inner bottom corner positions of the pair of large triangular supports are provided with rear hanging point supporting and fixing assemblies, and the vertex corner positions of the pair of large triangular supports are provided with upper wing body joint fixing assemblies; the design matched with the wing structure is adopted, the design is realized by adopting a bracket minimization technology, the long-distance transportation of the wings is facilitated, and the double-wing transportation bracket is adopted, so that the transportation efficiency is improved, and the transportation cost is saved.

Description

Wing transportation bracket

Technical Field

The utility model relates to the technical field of transportation auxiliary equipment, in particular to a wing transportation bracket.

Background

The aircraft manufacturing is a highly integrated systematic engineering, the size of most parts of the aircraft is suitable for transportation of the existing transportation equipment, and the transportation difficulty is basically avoided, but the parts such as the fuselage, the wings and the like are large-scale frameworks and are limited by the transportation equipment, so that the transportation cannot be performed at any time; improper protection of the wing during transport can cause damage to the wing.

The existing wing transportation device cannot well protect the aircraft wings and can not transport the aircraft wings with different specifications at the same time, so that the efficiency of transporting the wings is reduced, and the safety and reliability of transportation are affected. When the aircraft is transported and driven, the corresponding wing transportation device is generally used, the aircraft has various types, the wings of various aircraft have the self mechanism characteristics, and the transportation bracket cannot be suitable for the wings of various types, so that the special transportation fixing tool is designed aiming at a special large carrier vehicle for road transportation of the aircraft wing parts, and the aircraft wing parts are fixed and are convenient to transport.

Disclosure of Invention

The utility model aims to overcome the defects of the prior art, provide a wing transportation bracket and solve the problems that the transportation bracket is difficult to match with a wing and the transportation safety measures are insufficient in the transportation of the aircraft wing.

The utility model is realized by the following technical scheme:

the wing transportation bracket comprises a rectangular supporting frame, an upper wing body joint fixing assembly, a lower wing body joint fixing assembly and a rear hanging point supporting and fixing assembly, wherein a wing placement frame strip groove is formed in the rectangular supporting frame, and a pair of large triangular support frames are arranged on frames on two sides of one end part of the wing placement frame strip groove; the outer bottom corner positions of the pair of large triangular supports are provided with lower wing body joint fixing assemblies, the inner bottom corner positions of the pair of large triangular supports are provided with rear hanging point supporting and fixing assemblies, and the vertex corner positions of the pair of large triangular supports are provided with upper wing body joint fixing assemblies;

the upper wing body joint fixing assembly comprises an upper wing body joint fixing seat assembly and an upper wing body joint assembly used for connecting an upper wing joint;

the lower wing body joint fixing assembly comprises a lower wing body joint fixing seat assembly and a lower wing body joint assembly used for connecting a lower wing joint;

the rear hanging point supporting and fixing assembly comprises a rear hanging point supporting and fixing seat assembly and a wing surface rear hanging point assembly used for connecting the wing surface hanging points.

Furthermore, two wing placing frame strip grooves are symmetrically formed in the rectangular supporting frame, and each wing placing frame strip groove can be used for placing one wing.

Further, the upper wing body joint fixing seat assembly, the lower wing body joint fixing seat assembly and the rear hanging point supporting fixing seat assembly have the same structure and comprise a holding shaft seat and a pressing plate, wherein the holding shaft seat is arranged on the frame through the bottom plate, the left side and the right side of the holding shaft seat are respectively provided with a radial pressing plate, and the radial pressing plates are provided with radial pressing screws; an axial jacking plate is arranged on the outer side of the axle holding seat, an axial jacking screw is arranged on the axial jacking plate, the pressing plate is buckled and installed on the axle holding seat, and an adapter shaft on the upper wing body joint fixing seat assembly, the lower wing body joint fixing seat assembly or the rear hanging point supporting fixing seat assembly is limited in the axle holding seat assembly.

According to the structural characteristics of the wing, the rectangular supporting frame is provided with the wing placing frame strip groove, two side frames at one end part of the wing placing frame strip groove are provided with the pair of large triangular support frames, the wing is placed by the wing placing frame strip groove and the pair of large triangular support frames, the design matched with the wing structure is adopted, the technical design of the bracket is adopted to minimize the wing structure, the long-distance transportation of the wing is facilitated, the double-wing transportation bracket is adopted, the transportation efficiency is improved, and the transportation cost is saved.

Further, the upper wing body joint assembly comprises a switching shaft and an upper wing body joint piece, wherein the switching shaft is inserted into the upper part of the upper wing body joint piece, and a joint pin shaft connected with the wing is also inserted into the lower part of the upper wing body joint piece.

Further, a universal rotary hanging ring is arranged on the adapter shaft of the upper wing body joint assembly.

Further, the lower wing body joint assembly comprises a switching shaft and a lower wing body joint piece, wherein the switching shaft is inserted into the upper part of the lower wing body joint piece, and bolt connecting pieces connected with the wings are arranged on two sides of the lower part of the lower wing body joint piece.

Further, the wing surface rear hanging point assembly comprises a left switching shaft, a right switching shaft and a hanging point connector, wherein the inner end of the left switching shaft is provided with a plug rod piece connector, the inner end of the right switching shaft is provided with a plug rod piece connector, the plug rod piece is connected to the plug rod piece connector through threads, and the hanging point connectors are respectively sleeved on the left switching shaft and the right switching shaft.

Further, a pair of small triangular support frames are arranged on the frames at the two sides of the other end part of the wing placement frame strip groove; a pair of wing surface clamping pieces are arranged at the top parts of the pair of small triangular supports;

a pair of wing surface clamping pieces are also arranged on the inner side frames of the pair of large triangular support frames.

Furthermore, lifting points are arranged at four corners of the rectangular supporting frame, mooring rings are arranged around the rectangular supporting frame, and sleepers are arranged at the bottom of the rectangular supporting frame to play a role in shock absorption in the transportation process.

Further, a reinforced U-shaped frame is arranged on the outer inclined frames of the paired large triangular support frames; a reinforcing frame is arranged between two pairs of large triangular supports and between two adjacent sets of large triangular supports.

Compared with the prior art, the utility model has the following advantages and beneficial effects:

1. according to the structural characteristics of the wing, the rectangular supporting frame is provided with the wing placing frame strip groove, two side frames at one end part of the wing placing frame strip groove are provided with a pair of large triangular support frames, the wing is placed by the wing placing frame strip groove and the large triangular support frames in a matched mode, the design of the wing structure is adopted, the technical design of the carrier minimization is adopted, long-distance wing transportation is facilitated, and the double-wing transportation carrier is adopted, so that the transportation efficiency is improved, and the transportation cost is saved;

2. the utility model relates to a wing transportation bracket, which is designed to ensure the safe transportation of wings, and mainly ensures the safety hidden trouble of the wings in the hoisting and transportation processes through the safe fixation of three fixed points of an upper wing body joint fixing assembly, a lower wing body joint fixing assembly and a rear hanging point supporting and fixing assembly and the hoisting installation;

3. according to the wing transportation bracket, the upper wing body joint fixing assembly, the lower wing body joint fixing assembly and the rear hanging point supporting and fixing assembly are movably installed, so that the wing can be conveniently assembled and disassembled, the whole transportation bracket is simple in design, and the safety of the wing in the transportation process is fully ensured.

Drawings

The accompanying drawings, which are included to provide a further understanding of embodiments of the utility model and are incorporated in and constitute a part of this application, illustrate embodiments of the utility model. In the drawings:

FIG. 1 is a schematic perspective view of a wing transport carrier according to the present utility model;

FIG. 2 is a schematic top view of a wing transport carrier according to the present utility model;

FIG. 3 is a schematic view of the structure of a shipping wing of the present utility model;

FIG. 4 is a schematic view of the structure of a lifting wing of the present utility model;

FIG. 5 is a schematic view of the structure of the upper blade body joint securing assembly of the present utility model;

FIG. 6 is a schematic view of the upper wing body joint assembly of the present utility model;

FIG. 7 is a schematic view of the lower blade attachment assembly of the present utility model;

FIG. 8 is a schematic view of the lower wing body joint assembly of the present utility model;

FIG. 9 is a schematic view of the structure of the rear hitch point support securement assembly of the present utility model;

FIG. 10 is a schematic structural view of an airfoil rear hitch point assembly of the present utility model;

FIG. 11 is a schematic cross-sectional structural view of an airfoil rear hitch point assembly of the present utility model.

In the drawings, the reference numerals and corresponding part names:

1-rectangular supporting frame, 2-upper wing body joint fixing component, 3-lower wing body joint fixing component, 4-rear hanging point supporting and fixing component, 5-wing placing frame strip groove, 6-large triangular supporting frame, 7-upper wing body joint fixing seat component, 8-upper wing body joint component, 9-lower wing body joint fixing seat component, 10-lower wing body joint component, 11-rear hanging point supporting and fixing seat component, 12-wing surface rear hanging point component, 13-axle-holding seat, 14-pressing plate and 15-radial pressing plate, 16-radial jacking screw rods, 17-axial jacking plates, 18-axial jacking screw rods, 19-connecting shafts, 191-left connecting shafts, 192-right connecting shafts, 20-upper wing body joint pieces, 21-joint pin shafts, 22-universal rotating lifting rings, 23-lower wing body joint pieces, 24-bolt connectors, 25-lifting point joints, 26-inserting rods, 27-inserting rod piece joints, 28-small triangular support frames, 29-wing surface clamping pieces, 30-lifting points, 31-mooring rings, 32-sleepers, 33-reinforced U-shaped frames, 34-reinforced frames and 35-wings.

Detailed Description

In order to make the present application solution better understood by those skilled in the art, the following description will be made in detail and with reference to the accompanying drawings in the embodiments of the present application, it is apparent that the described embodiments are only some embodiments of the present application, not all embodiments. All other embodiments, which can be made by one of ordinary skill in the art based on the embodiments herein without making any inventive effort, shall fall within the scope of the present application.

It should be noted that the terms "first," "second," and the like in the description and claims of the present application and the above figures are used for distinguishing between similar objects and not necessarily for describing a particular sequential or chronological order. It is to be understood that the data so used may be interchanged where appropriate in order to describe the embodiments of the present application described herein. Furthermore, the terms "comprises," "comprising," and "having," and any variations thereof, are intended to cover a non-exclusive inclusion, such that a process, method, system, article, or apparatus that comprises a list of steps or elements is not necessarily limited to those steps or elements expressly listed but may include other steps or elements not expressly listed or inherent to such process, method, article, or apparatus.

In the present application, the terms "upper", "lower", "left", "right", "front", "rear", "top", "bottom", "inner", "outer", "middle", "vertical", "horizontal", "lateral", "longitudinal" and the like indicate an azimuth or a positional relationship based on that shown in the drawings. These terms are used primarily to better describe the present application and its embodiments and are not intended to limit the indicated device, element or component to a particular orientation or to be constructed and operated in a particular orientation.

Also, some of the terms described above may be used to indicate other meanings in addition to orientation or positional relationships, for example, the term "upper" may also be used to indicate some sort of attachment or connection in some cases. The specific meaning of these terms in this application will be understood by those of ordinary skill in the art as appropriate.

Furthermore, the terms "mounted," "configured," "provided," "connected," "coupled," and "sleeved" are to be construed broadly. For example, it may be a fixed connection, a removable connection, or a unitary construction; may be a mechanical connection, or an electrical connection; may be directly connected, or indirectly connected through intervening media, or may be in internal communication between two devices, elements, or components. The specific meaning of the terms in this application will be understood by those of ordinary skill in the art as the case may be.

It should be noted that, in the case of no conflict, the embodiments and features in the embodiments may be combined with each other. The present application will be described in detail below with reference to the accompanying drawings in conjunction with embodiments.

Example 1

As shown in fig. 1-11, the wing transportation bracket of the present utility model is used for placing disassembled aircraft components during transition transportation, has the capability of carrying out highway and waterway transportation in a vehicle loading mode, and comprises a rectangular supporting frame 1, an upper wing body joint fixing assembly 2, a lower wing body joint fixing assembly 3 and a rear hanging point supporting and fixing assembly 4, wherein the rectangular supporting frame 1 adopts a rectangular frame structure, the rectangular frame 1 adopts steel profile welding, and the external dimension is as follows: 6460mm multiplied by 1960mm multiplied by 2835mm, weight is 1700kg (without wings), a wing placing frame strip groove 5 is arranged on the rectangular supporting frame 1, and a pair of large triangular supporting frames 6 are arranged on two side frames at one end part of the wing placing frame strip groove 5; the outer bottom corner positions of the pair of large triangular supports 6 are provided with lower wing body joint fixing assemblies 3, the inner bottom corner positions of the pair of large triangular supports 6 are provided with rear hanging point supporting and fixing assemblies 4, and the apex corner positions of the pair of large triangular supports 6 are provided with upper wing body joint fixing assemblies 2; the upper wing body joint fixing assembly 2 comprises an upper wing body joint fixing seat assembly 7 and an upper wing body joint assembly 8 for connecting an upper wing joint; the lower wing body joint fixing assembly 3 comprises a lower wing body joint fixing seat assembly 9 and a lower wing body joint assembly 10 for connecting with a lower wing joint; the rear hanging point supporting and fixing assembly 4 comprises a rear hanging point supporting and fixing seat assembly 11 and a wing surface rear hanging point assembly 12 used for connecting the wing surface hanging points. The utility model relates to a wing transportation bracket, which is designed to ensure the safe transportation of wings, and mainly ensures the safety hidden trouble of the wings in the hoisting and transportation processes through the safe fixation of three fixed points of an upper wing body joint fixing component 2, a lower wing body joint fixing component 3 and a rear hanging point supporting and fixing component 4 and the hoisting installation; the upper wing body joint fixing assembly 2, the lower wing body joint fixing assembly 3 and the rear hanging point supporting and fixing assembly 4 adopt a movably mounted connection mode, so that the wing can be conveniently assembled and disassembled, the whole transportation bracket is simple in design, and the safety of the wing in the transportation process is fully ensured.

Two wing placing frame strip grooves 5 are symmetrically formed in the rectangular supporting frame 1, and each wing placing frame strip groove 5 can be used for placing one wing. One set of transport brackets can transport two wings at a time.

When the wing transportation bracket is used, the transportation bracket is fixed on a transportation vehicle, as shown in fig. 3-4, an upper wing body joint fixing component 2 is connected with an upper wing body joint (an installation joint of a wing and a fuselage) of the wing to form a hanging point, a rear hanging point supporting and fixing component 4 is connected with the outer end part of a wing surface, the rear hanging point supporting and fixing component 4 is inserted on the wing surface, two hanging points are arranged on the left side and the right side of the rear hanging point supporting and fixing component 4, the wing is lifted and installed on the transportation bracket through the three hanging points, and after the wing is placed, the wing is fixed on the transportation bracket through the upper wing body joint fixing component 2, the lower wing body joint fixing component 3 and the rear hanging point supporting and fixing component 4, and a large triangular support frame 6 on the rectangular support frame 1 in a matched and fixed mode, and other auxiliary fixing devices are adopted to fix the wing on the transportation bracket completely and safely.

According to the structural characteristics of the wing, the rectangular supporting frame 1 is provided with the wing placing frame strip groove 5, two side frames at one end part of the wing placing frame strip groove 5 are provided with the pair of large triangular supports 6, the wing is placed in a pair through the wing placing frame strip groove 5 and the large triangular supports 6, the design matched with the wing structure is adopted, the design is realized by adopting the technology of minimizing the bracket, the long-distance wing transportation is facilitated, the double-wing transportation bracket is adopted, the transportation efficiency is improved, and the transportation cost is saved.

Example 2

As shown in fig. 1-10, on the basis of the embodiment, as shown in fig. 5-10, the upper wing body joint fixing seat assembly 7, the lower wing body joint fixing seat assembly 9 and the rear hanging point supporting fixing seat assembly 11 have the same structure and all comprise a shaft holding seat 13 and a pressing plate 14, wherein the shaft holding seat 13 is arranged on a frame through a bottom plate, radial pressing plates 15 are respectively arranged on the left side and the right side of the shaft holding seat 13, and radial pressing screws 16 are arranged on the radial pressing plates 15; an axial jacking plate 17 is arranged on the outer side of the axle-holding seat 13, an axial jacking screw 18 is arranged on the axial jacking plate 17, the pressing plate 14 is buckled and installed on the axle-holding seat 13, and a transfer shaft 19 on the upper wing body joint fixing seat assembly 7, the lower wing body joint fixing seat assembly 9 or the rear hanging point supporting fixing seat assembly 11 is limited in the axle-holding seat assembly.

As shown in fig. 6, the upper wing body joint assembly 8 includes a transfer shaft 19 and an upper wing body joint member 20, wherein the transfer shaft 19 is inserted into the upper portion of the upper wing body joint member 20, and a joint pin 21 connected with the wing is inserted into the lower portion of the upper wing body joint member 20. The joint pin 21 is inserted into the upper wing body joint of the wing, and two ends of the joint pin 21 are fixedly arranged on the upper wing body joint piece 20, so that the upper wing body joint assembly 8 is connected with the wing.

The universal rotary hanging ring 22 is arranged on the adapter shaft 19 of the upper wing body joint assembly 8. The universal rotary hanging ring 22 is a lifting point of the wing, and the wing can be placed and adjusted through the universal rotary hanging ring 22, so that the wing can be conveniently placed on the transportation bracket.

As shown in fig. 8, the lower wing-body joint assembly 10 includes a transfer shaft 19 and a lower wing-body joint member 23, wherein the transfer shaft 19 is inserted in the upper portion of the lower wing-body joint member 23, and two sides of the lower portion of the lower wing-body joint member 23 are provided with bolt connectors 24 connected with the wings. The lower wing body joint assembly 10 is connected with the lower wing body joint of the wing, and the lower wing body joint assembly 10 does not need to serve as a lifting point, so that the universal rotary lifting ring 22 is not needed in the structure, the lower wing body joint assembly 10 is connected with a wing mounting bolt structure for mounting, a movable point is not needed, and the wing is convenient to fixedly mount.

As shown in fig. 10-11, the rear hanging point assembly 12 of the wing surface comprises a left switching shaft 191, a right switching shaft 192 and a hanging point joint 25, wherein the inner end of the left switching shaft 191 is provided with a plug rod piece 26, the inner end of the right switching shaft 192 is provided with a plug rod piece joint 27, the plug rod piece 26 is connected to the plug rod piece joint 27 through threads, and the hanging point joint 25 is sleeved on each of the left switching shaft 191 and the right switching shaft 192.

The utility model designs a rear hanging point component 12 of the wing surface by utilizing the mounting through hole, the rear hanging point component 12 of the wing surface is connected by adopting two left connecting shafts 191 and right connecting shafts 192 in a connecting rod threaded manner, and the contact part with the hanging point hole is separated by adopting a copper bush and a copper gasket, so that the abrasion of the hole surface is avoided; on both sides are arranged hoisting point joints 25 for hoisting and are provided with lock nuts preventing rotation of the hoisting point joints 25.

As shown in fig. 5-10, the upper wing body joint fixing seat assembly 7, the lower wing body joint fixing seat assembly 9 and the rear hanging point supporting fixing seat assembly 11 are installed on the rectangular supporting frame 1 in advance, the upper wing body joint assembly 8, the lower wing body joint assembly 10 and the wing surface rear hanging point assembly 12 are all provided with switching shaft structural members, when the upper wing body joint assembly 8, the lower wing body joint assembly 10 and the wing surface rear hanging point assembly 12 are installed in a matched manner with the corresponding upper wing body joint fixing seat assembly 7, the lower wing body joint fixing seat assembly 9 and the rear hanging point supporting fixing seat assembly 11, the switching shaft structural members are placed on the axle holding seat 13 and fastened and fixed through the pressing plates 14, the pressing plates 14 are pressed through radial pressing screws 16 on the radial pressing plates 15 on the left side and the right side of the axle holding seat 13 respectively, the pressing plates 14 are limited, the axial pressing screws 18 on the axial pressing plates 17 limit the ends of the switching shaft structure, and the switching shaft structure comprises a left switching shaft 191 and a right switching shaft 192.

Example 3

As shown in fig. 1-10, based on the above embodiments, the present embodiment mainly includes a pair of small triangular supports 28 on two side frames at the other end of the wing placement frame strip groove 5; a pair of wing surface clamping pieces 29 are arranged at the top of the pair of small triangular support frames 28; a pair of wing clamping members 29 are also provided on the inner side frames of the pair of large triangular supports 6. The airfoil clamping piece 29 adopts a screw rod structure, and the clamping blocks are clamped on the airfoil surface by rotating the screw rod structure, so that the airfoil fixing function is realized.

Lifting points 30 are arranged at four corners of the rectangular supporting frame 1, mooring rings 31 are arranged around the rectangular supporting frame 1, the mooring rings 31 are mainly used for fixing brackets on a vehicle, sleepers 32 are arranged at the bottom of the rectangular supporting frame 1, and the rectangular supporting frame has a damping effect in the transportation process.

The outer side inclined frames of the paired large triangular support frames 6 are provided with reinforced U-shaped frames 33; a reinforcing frame 34 is arranged between two pairs of large triangular supports 6 and between two adjacent sets of large triangular supports 6. The rectangular supporting frame 1 is a base structure, a large vertical triangular support frame 6 is arranged on the rectangular supporting frame 1, and a U-shaped frame 33 and a reinforcing frame 34 are arranged for the installation stability of the large triangular support frame 6, so that the rectangular supporting frame 1, the U-shaped frame 33 and the reinforcing frame 34 form a stable integral structure.

The arrangement of the large triangular support frame 6 and the small triangular support frame 28 is mainly based on the structural characteristics of the wings, and when the wings are transported and placed, one end of each wing is kept high, the other end of each wing is kept low, and safe transportation is facilitated. In addition, for the purpose of the shipping safety of the wing, an auxiliary wing surface supporting block is arranged at the bottom of the wing placement frame strip groove 5, and the auxiliary wing surface supporting block is made of EPE foam and is used for supporting the tail of the wing.

After the wings are hoisted on the bracket, the body is covered by pearl wool, rainproof tarpaulin and a net bag from bottom to top in sequence, and finally the net bag is fixed on the bracket; the transport carrier is suspended from the transport vehicle bed using flat straps and secured to the vehicle using straps or tighteners.

The foregoing description of the embodiments has been provided for the purpose of illustrating the general principles of the utility model, and is not meant to limit the scope of the utility model, but to limit the utility model to the particular embodiments, and any modifications, equivalents, improvements, etc. that fall within the spirit and principles of the utility model are intended to be included within the scope of the utility model.

Claims

1. The utility model provides a wing transportation bracket, includes rectangle support frame (1), goes up wing body joint fixed subassembly (2), lower wing body joint fixed subassembly (3) and back hanging point support fixed subassembly (4), its characterized in that: the rectangular support frame (1) is provided with a wing placement frame strip groove (5), and a pair of large triangular support frames (6) are arranged on frames on two sides of one end part of the wing placement frame strip groove (5); the outer bottom corner positions of the pair of large triangular supports (6) are provided with lower wing body joint fixing assemblies (3), the inner bottom corner positions of the pair of large triangular supports (6) are provided with rear hanging point supporting and fixing assemblies (4), and the top corner positions of the pair of large triangular supports (6) are provided with upper wing body joint fixing assemblies (2);

the upper wing body joint fixing assembly (2) comprises an upper wing body joint fixing seat assembly (7) and an upper wing body joint assembly (8) used for connecting an upper wing joint;

the lower wing body joint fixing assembly (3) comprises a lower wing body joint fixing seat assembly (9) and a lower wing body joint assembly (10) used for connecting a lower wing joint;

the rear hanging point supporting and fixing assembly (4) comprises a rear hanging point supporting and fixing seat assembly (11) and a wing surface rear hanging point assembly (12) used for connecting an aircraft surface hanging point.

2. A wing transport carrier according to claim 1, wherein: two wing placing frame strip grooves (5) are symmetrically formed in the rectangular supporting frame (1), and each wing placing frame strip groove (5) can be used for placing one wing.

3. A wing transport carrier according to claim 1, wherein: the upper wing body joint fixing seat assembly (7), the lower wing body joint fixing seat assembly (9) and the rear hanging point supporting fixing seat assembly (11) are identical in structure and comprise a shaft holding seat (13) and a pressing plate (14), the shaft holding seat (13) is installed on a frame through a bottom plate, radial pressing plates (15) are respectively arranged on the left side and the right side of the shaft holding seat (13), and radial pressing screws (16) are arranged on the radial pressing plates (15); an axial jacking plate (17) is arranged on the outer side of the axle holding seat (13), an axial jacking screw (18) is arranged on the axial jacking plate (17), the pressing plate 14 is buckled and installed on the axle holding seat (13), and an adapter shaft (19) on the upper wing body joint fixing seat assembly (7), the lower wing body joint fixing seat assembly (9) or the rear hanging point supporting fixing seat assembly (11) is limited in the axle holding seat assembly.

4. A wing transport carrier according to claim 1, wherein: the upper wing body joint assembly (8) comprises a switching shaft (19) and an upper wing body joint piece (20), wherein the switching shaft (19) is inserted into the upper part of the upper wing body joint piece (20), and a joint pin shaft (21) connected with the wing is also inserted into the lower part of the upper wing body joint piece (20).

5. A wing transport carrier according to claim 4, wherein: the universal rotary hanging ring (22) is arranged on the adapter shaft (19) of the upper wing body joint assembly (8).

6. A wing transport carrier according to claim 1, wherein: the lower wing body joint assembly (10) comprises a switching shaft (19) and a lower wing body joint piece (23), wherein the switching shaft (19) is inserted into the upper part of the lower wing body joint piece (23), and bolt connecting pieces (24) connected with wings are arranged on two sides of the lower part of the lower wing body joint piece (23).

7. A wing transport carrier according to claim 1, wherein: the wing surface rear hanging point assembly (12) comprises a left switching shaft (191), a right switching shaft (192) and a hanging point connector (25), wherein a plug rod piece (26) is arranged at the inner end of the left switching shaft (191), a plug rod piece connector (27) is arranged at the inner end of the right switching shaft (192), the plug rod piece (26) is connected to the plug rod piece connector (27) through threads, and the hanging point connector (25) is sleeved on the left switching shaft (191) and the right switching shaft (192).

8. A wing transport carrier according to claim 1, wherein: a pair of small triangular support frames (28) are arranged on the frames on two sides of the other end part of the wing placement frame strip groove (5); a pair of wing surface clamping pieces (29) are arranged at the top of the pair of small triangular support frames (28);

a pair of wing surface clamping pieces (29) are also arranged on the inner side frames of the paired large triangular support frames (6).

9. A wing transport carrier according to claim 1, wherein: lifting points (30) are arranged at four corners of the rectangular supporting frame (1), mooring rings (31) are arranged around the rectangular supporting frame (1), and sleepers (32) are arranged at the bottom of the rectangular supporting frame (1) to play a role in shock absorption in the transportation process.

10. A wing transport carrier according to claim 1, wherein: the outer side inclined frames of the paired large triangular support frames (6) are provided with reinforced U-shaped frames (33); a reinforcing frame (34) is arranged between two pairs of large triangular supports (6) and between two adjacent sets of large triangular supports (6).