CN112606754B

CN112606754B - Road transport aircraft device

Info

Publication number: CN112606754B
Application number: CN202011465805.5A
Authority: CN
Inventors: 王丽杰; 刘晓雪; 丁立民; 李建军; 李晓兰
Original assignee: Avic Shijiazhuang Aircraft Industry Group Corp ltd
Current assignee: Avic Shijiazhuang Aircraft Industry Group Corp ltd
Priority date: 2020-12-14
Filing date: 2020-12-14
Publication date: 2022-04-12
Anticipated expiration: 2040-12-14
Also published as: CN112606754A

Abstract

The invention relates to a road transport airplane device, which comprises a bracket device A, a bracket device B and a bracket device C which are horizontally arranged in sequence; the bracket device A and the bracket device B are provided with a fuselage, a horizontal tail wing and an upper wing; the lower wing, the rudder and the vertical stabilizing surface are arranged on the bracket device B and the bracket device C; the parts of the bracket device A, the bracket device B and the bracket device C, which are contacted with the corresponding parts of the airplane, are provided with polyester ethylene foam materials; the invention ensures that all parts of the airplane are firmly fixed and absorb shock during transportation, fully utilizes the three-dimensional space of one vehicle, reasonably arranges the length, the fatness and the thinness of all the parts of the airplane on the bracket device A, the bracket device B and the bracket device C, and ensures that all the parts of one airplane are transported by utilizing one transport vehicle, thereby saving space, manpower and material resources.

Description

Road transport aircraft device

Technical Field

The invention relates to a road transport airplane device, and belongs to the field of air transport equipment.

Background

When the five transport/five transport B series aircraft (Y5/Y5B series) cannot realize the complete aircraft transition, the aircraft transition is generally divided into parts firstly, and then the road transport or water transport mode is adopted, so that the limitation of the road width and the height of obstacles on the road need to be considered during transportation, and the measures of fixing, locking, shock resistance and the like of the aircraft parts in the transportation process need to be considered. During present transportation, need transport two cars with wing each part and fuselage partial shipment, collision between each part often can appear when marcing, makes the part impaired, and two cars transport has increased the cost of transportation moreover.

Disclosure of Invention

The invention aims to solve the technical problem of providing a road transport airplane device which can firmly fix each part of an airplane on an automobile with the existing specification and size, reasonably utilize the space within the limit of minimum height and width and finish the transportation by using one automobile.

The invention adopts the following technical scheme:

the invention comprises a bracket device A, a bracket device B and a bracket device C which are horizontally arranged in sequence; the bracket device A and the bracket device B are provided with a fuselage, a horizontal tail wing and an upper wing; the lower wing, the rudder and the vertical stabilizing surface are arranged on the bracket device B and the bracket device C; the contact parts of the bracket device A, the bracket device B and the bracket device C with the corresponding parts of the airplane are provided with polyester ethylene foam materials.

The bracket device A comprises an upper bracket A and a lower bracket A which correspond to each other up and down; the upper bracket A comprises an upper bracket frame A, a first two-fork support A arranged below one end of the upper bracket frame A and a second two-fork support A arranged below the other end of the upper bracket frame A, the first two-fork support A and the second two-fork support A are respectively provided with a first clamping groove A, the two first clamping grooves A are respectively correspondingly clamped on the upper parts of one ends of the corresponding upper wings, and the upper bracket frame A is provided with a first through groove A inserted with one end of the horizontal tail wing; the lower bracket A comprises a lower bracket A connecting frame, a third support A which is arranged on the lower bracket A connecting frame and corresponds to the first two-fork support A, and a fourth support A which corresponds to the second two-fork support A, and second clamping grooves A which are used for clamping the lower part of one end of the upper wing are respectively arranged on the third support A and the fourth support A; the upper part of the front end of the machine body is clamped between the first two-fork support A and the second two-fork support A; the lower part of the front end of the machine body is clamped between the third support A and the fourth support A.

The bracket device B comprises an upper bracket B and a lower bracket B which correspond to each other up and down; the rear end of the machine body is arranged between the upper bracket B and the lower bracket B; the upper bracket B comprises an upper bracket frame, a first three-fork support B arranged below one end of the upper bracket frame and a second three-fork support B arranged below the other end of the upper bracket frame, the first three-fork support B and the second three-fork support B are respectively provided with an outer clamping groove and an inner clamping groove, the outer clamping grooves are respectively clamped on the upper parts of the other ends of the corresponding upper wings, the inner clamping grooves are respectively clamped on the upper parts of one ends of the corresponding lower wings, and the upper bracket frame is provided with a through groove B inserted with the other end of the horizontal tail wing; the lower bracket B comprises a lower bracket B connecting plate, a third support B and a fourth support B, the third support B is arranged on the lower bracket B connecting plate and corresponds to the first three-fork support B, the fourth support B corresponds to the second three-fork support B, a first clamping groove B is arranged on the outer side of the third support B and is clamped at the lower part of the other end of one of the upper wings, a third clamping groove B is arranged on the inner side of the third support B and is clamped at one end of the rudder, and a second clamping groove B is arranged between the first clamping groove B and the third clamping groove B and is clamped at the lower part of one end of one of the lower wings; and a fourth clamping groove B clamped at the lower part of the other end of the other upper wing is arranged on the outer side of the fourth support B, and a fifth clamping groove B clamped at the lower part of one end of the other lower wing is arranged on the inner side of the fourth support B.

The bracket device C comprises an upper bracket C and a lower bracket C which correspond to each other up and down; the upper bracket C comprises an upper bracket C connecting frame, a first support C arranged below one end of the upper bracket C connecting frame and a second support C arranged below the other end of the upper bracket C connecting frame, and V-shaped clamping grooves C with downward openings are formed in the first support C and the second support C; the two V-shaped clamping grooves C are correspondingly clamped at the upper parts of the other ends of the corresponding lower wings respectively; the lower bracket C comprises a lower bracket C connecting plate, a third support C and a fourth support C, the third support C is arranged on the lower bracket C connecting plate and corresponds to the first support C, the fourth support C corresponds to the second support C, clamping grooves B corresponding to the V-shaped clamping grooves C are respectively arranged on the outer sides of the third support C and the fourth support C, and the two clamping grooves B are respectively correspondingly clamped on the lower parts of the other ends of the corresponding lower wings; the inner side of the third support C is provided with a clamping groove C for clamping the other end of the rudder, the inner side of the fourth support C is provided with a clamping groove D for clamping one end of the vertical settling surface, and a bracket groove for clamping the other end of the vertical settling surface is arranged between the lower bracket C and the lower bracket B.

The inner side of the bracket slot is provided with a polyester ethylene foam material at the contact part with the vertical stabilizing surface.

The invention has the following positive effects: the bracket device A, the bracket device B and the bracket device C are matched with the actual overall dimensions of each part of the airplane to firmly fix the airplane parts, and the parts of the bracket device A, the bracket device B, the bracket device C and the bracket groove, which are contacted with the corresponding parts of the airplane, are provided with the polyester ethylene foam material which has small density, stable chemical performance, good processability, friction resistance and easy forming, so that each part is firmly fixed and is damped in transportation, the three-dimensional space of a vehicle is fully utilized, the length, the thinness and the thinness of each part of the airplane on the bracket device A, the bracket device B and the bracket device C are reasonably matched, all parts of the airplane are transported by using one transport vehicle, the space is saved, and the manpower and the material resources are saved.

Drawings

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a schematic structural view of a bracket device A of the present invention;

FIG. 3 is a schematic structural view of a bracket device B of the present invention;

FIG. 4 is a schematic structural view of a bracket device C according to the present invention;

fig. 5 is a schematic view of a structure in which the fuselage is placed on the structure of the present invention.

Detailed Description

As shown in the attached drawings 1 and 5, the invention comprises a bracket device A, a bracket device B and a bracket device C which are horizontally arranged in sequence and fixed on a transport vehicle; the bracket device A and the bracket device B are provided with a machine body 1, a horizontal tail wing 2 and an upper wing 3; the lower wing 4, the rudder 5 and the vertical stabilizing surface 6 are placed on the bracket device B and the bracket device C, and then the bracket device A, the bracket device B and the bracket device C are fixed by using binding bands respectively; the contact parts of the bracket device A, the bracket device B and the bracket device C with the corresponding parts of the airplane are provided with polyester ethylene foam materials.

As shown in FIG. 2, the bracket device A of the present invention comprises an upper bracket A11 and a lower bracket A12 which correspond to each other up and down; the upper bracket A11 comprises an upper bracket frame A111, a first two-fork support A112 installed below one end of the upper bracket frame A111 and a second two-fork support A113 installed below the other end of the upper bracket frame A111, wherein first clamping grooves A114 are respectively formed in the first two-fork support A112 and the second two-fork support A113, the two first clamping grooves A114 are respectively clamped on the upper parts of one ends of the corresponding upper wings 3 correspondingly, and a first through groove A115 inserted with one end of the horizontal tail wing 2 is formed in the upper bracket frame A111; the two first clamping grooves A114 are symmetrically arranged, and the first clamping grooves A114 are in a V shape with a downward opening; the lower bracket A12 comprises a lower bracket A connecting frame 121, a third support A122 which is arranged on the lower bracket A connecting frame 121 and corresponds to the first two-fork support A112, and a fourth support A123 which corresponds to the second two-fork support A113, wherein a second clamping groove A124 for clamping the lower part of one end of the upper wing 3 is respectively arranged on the third support A122 and the fourth support A123; the two second clamping grooves A124 are symmetrically arranged, and the second clamping grooves A124 are in a V shape with an upward opening; the upper part of the front end of the fuselage 1 is clamped between the first two-fork support A112 and the second two-fork support A113, and the lower part of the front end of the fuselage 1 is clamped between the third support A122 and the fourth support A123, so that the fuselage and the wing empennage are skillfully and reasonably arranged on a transport truck.

As shown in FIG. 3, the bracket device B of the invention comprises an upper bracket B9 and a lower bracket B10 which correspond to each other up and down; the rear end of the machine body 1 is arranged between an upper bracket B9 and a lower bracket B10; the upper bracket B9 comprises an upper bracket frame 91, a first three-fork support B92 arranged below one end of the upper bracket frame 91 and a second three-fork support B93 arranged below the other end of the upper bracket frame 91, wherein the first three-fork support B92 and the second three-fork support B93 are respectively provided with an outer clamping groove and an inner clamping groove which are provided with downward openings and are V-shaped, the outer clamping grooves are respectively clamped on the upper parts of the other ends of the corresponding upper wings 3 correspondingly, the inner clamping grooves are respectively clamped on the upper parts of one ends of the corresponding lower wings 4 correspondingly, and the upper bracket frame 91 is provided with a through groove B94 inserted with the other end of the horizontal tail wing 2; one end of each of the first through groove A115 and the through groove B94 is arc-shaped, and the other end of each of the first through grooves A115 and the through grooves B94 is V-shaped; the lower bracket B10 comprises a lower bracket B connecting plate 100, a third support B101 which is arranged on the lower bracket B connecting plate 100 and corresponds to the first three-fork support B92, and a fourth support B102 which corresponds to the second three-fork support B93, wherein a first clamping groove B103 which is clamped at the lower part of the other end of one of the upper wings 3 is arranged at the outer side of the third support B101, a third clamping groove B105 which is clamped at one end of the rudder 5 is arranged at the inner side of the third support B101, and a second clamping groove B104 which is clamped at the lower part of one end of one of the lower wings 4 is arranged between the first clamping groove B103 and the third clamping groove B105; a fourth clamping groove B106 clamped at the lower part of the other end of the other upper wing 3 is arranged on the outer side of the fourth support B102, and a fifth clamping groove B107 clamped at the lower part of one end of the other lower wing 4 is arranged on the inner side; the first card slot B103, the fourth card slot B106, the second card slot B104, and the fifth card slot B107 are symmetrically disposed.

As shown in fig. 4 and 5, the bracket device C of the present invention comprises an upper bracket C7 and a lower bracket C8 corresponding to each other; the upper bracket C7 comprises an upper bracket C connecting frame 71, a first support C72 arranged below one end of the upper bracket C connecting frame 71 and a second support C73 arranged below the other end of the upper bracket C connecting frame 71, and V-shaped clamping grooves C74 with downward openings are formed in the first support C72 and the second support C73; the two V-shaped clamping grooves C74 are correspondingly clamped at the upper part of the other end of the corresponding lower wing 4 respectively; the lower bracket C8 comprises a lower bracket C connecting plate 81, a third support C82 which is arranged on the lower bracket C connecting plate 81 and corresponds to the first support C72, and a fourth support C83 which corresponds to the second support C73, wherein the outer sides of the third support C82 and the fourth support C83 are respectively provided with a clamping groove B84 which corresponds to the V-shaped clamping groove C74, the two clamping grooves B84 are symmetrically arranged, and the two clamping grooves B84 are respectively and correspondingly clamped at the lower part of the other end of the corresponding lower wing 4; a clamping groove C85 for clamping the other end of the rudder 5 is arranged on the inner side of the third support C82, a clamping groove D86 for clamping one end of the vertical fixing surface 6 is arranged on the inner side of the fourth support C83, and a bracket groove 13 for clamping the other end of the vertical fixing surface 6 is arranged between the lower bracket C8 and the lower bracket B10; the inner side of the bracket slot 13 is provided with a polyester vinyl foam material at the contact part with the vertical stabilizing surface 6.

The bracket device A, the bracket device B and the bracket device C are matched with the actual overall dimensions of each part of the airplane to firmly fix the airplane parts, and the parts of the bracket device A, the bracket device B, the bracket device C and the bracket groove, which are contacted with the corresponding parts of the airplane, are provided with the polyester ethylene foam material which has small density, stable chemical performance, good processability, friction resistance and easy forming, so that each part is safely and firmly fixed and can absorb shock in transportation, the three-dimensional space of a vehicle is fully utilized, the upper wing and the lower wing are vertically placed, the horizontal plane is horizontally placed, the length and the slimness are reasonably arranged, all the parts of one airplane are transported by using one vehicle, the space is saved, and the manpower and material resources are saved.

Finally, the above description is only for the purpose of illustrating the preferred embodiments of the present invention and should not be taken as limiting the invention, so that any modification, equivalent replacement or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

Claims

1. A road transport airplane device is characterized by comprising a bracket device A, a bracket device B and a bracket device C which are horizontally arranged in sequence; the bracket device A and the bracket device B are provided with a machine body (1), a horizontal tail wing (2) and an upper wing (3);

the lower wing (4), the rudder (5) and the vertical stabilizer (6) are arranged on the bracket device B and the bracket device C;

the parts of the bracket device A, the bracket device B and the bracket device C, which are contacted with the corresponding parts of the airplane, are provided with polyester ethylene foam materials;

the bracket device A comprises an upper bracket A (11) and a lower bracket A (12) which correspond to each other up and down;

the upper bracket A (11) comprises an upper supporting frame A (111), a first two-fork support A (112) arranged below one end of the upper supporting frame A (111) and a second two-fork support A (113) arranged below the other end of the upper supporting frame A (111), first clamping grooves A (114) are respectively formed in the first two-fork support A (112) and the second two-fork support A (113), the two first clamping grooves A (114) are correspondingly clamped on the upper parts of one ends of the corresponding upper wings (3), and first through grooves A (115) inserted with one ends of the horizontal tail wings (2) are formed in the upper supporting frame A (111);

the lower bracket A (12) comprises a lower bracket A connecting frame (121), a third support A (122) which is arranged on the lower bracket A connecting frame (121) and corresponds to the first two-fork support A (112), and a fourth support A (123) which corresponds to the second two-fork support A (113), and second clamping grooves A (124) which are used for clamping the lower part of one end of the upper wing (3) are respectively arranged on the third support A (122) and the fourth support A (123);

the upper part of the front end of the machine body (1) is clamped between a first two-fork support A (112) and a second two-fork support A (113); the lower part of the front end of the machine body (1) is clamped between a third support A (122) and a fourth support A (123);

the bracket device B comprises an upper bracket B (9) and a lower bracket B (10) which correspond to each other up and down; the rear end of the machine body (1) is arranged between an upper bracket B (9) and a lower bracket B (10);

the upper bracket B (9) comprises an upper supporting frame (91), a first three-fork support B (92) installed below one end of the upper supporting frame (91) and a second three-fork support B (93) installed below the other end of the upper supporting frame (91), the first three-fork support B (92) and the second three-fork support B (93) are respectively provided with an outer clamping groove and an inner clamping groove, the outer clamping grooves are respectively clamped on the upper parts of the other ends of the corresponding upper wings (3) correspondingly, the inner clamping grooves are respectively clamped on the upper parts of one ends of the corresponding lower wings (4) correspondingly, and the upper supporting frame (91) is provided with a through groove B (94) inserted on the other end of the horizontal tail wing (2);

the lower bracket B (10) comprises a lower bracket B connecting plate (100), a third support B (101) which is arranged on the lower bracket B connecting plate (100) and corresponds to the first three-fork support B (92), and a fourth support B (102) which corresponds to the second three-fork support B (93), wherein a first clamping groove B (103) which is clamped at the lower part of the other end of one of the upper wings (3) is arranged at the outer side of the third support B (101), a third clamping groove B (105) which is clamped at one end of the rudder (5) is arranged at the inner side of the third support B (101), and a second clamping groove B (104) which is clamped at the lower part of one end of one of the lower wings (4) is arranged between the first clamping groove B (103) and the third clamping groove B (105);

and a fourth clamping groove B (106) clamped at the lower part of the other end of the other upper wing (3) is arranged at the outer side of the fourth support B (102), and a fifth clamping groove B (107) clamped at the lower part of one end of the other lower wing (4) is arranged at the inner side.

2. A road transport aircraft unit as claimed in claim 1, characterised in that said carrier means C comprises upper (7) and lower (8) carriers which correspond up and down;

the upper bracket C (7) comprises an upper bracket C connecting frame (71), a first support C (72) arranged below one end of the upper bracket C connecting frame (71) and a second support C (73) arranged below the other end of the upper bracket C connecting frame (71), and V-shaped clamping grooves C (74) with downward openings are formed in the first support C (72) and the second support C (73); the two V-shaped clamping grooves C (74) are symmetrically arranged and are correspondingly clamped at the upper parts of the other ends of the corresponding lower wings (4) respectively;

the lower bracket C (8) comprises a lower bracket C connecting plate (81), a third support C (82) which is arranged on the lower bracket C connecting plate (81) and corresponds to the first support C (72), and a fourth support C (83) which corresponds to the second support C (73), clamping grooves B (84) which correspond to the V-shaped clamping grooves C (74) are respectively arranged on the outer sides of the third support C (82) and the fourth support C (83), and the lower parts of the other ends of the corresponding lower wings (4) are correspondingly clamped on the two clamping grooves B (84);

a clamping groove C (85) for clamping the other end of the rudder (5) is formed in the inner side of the third support C (82), a clamping groove D (86) for clamping one end of the vertical stabilizing surface (6) is formed in the inner side of the fourth support C (83), and a bracket groove (13) for clamping the other end of the vertical stabilizing surface (6) is formed between the lower bracket C (8) and the lower bracket B (10).

3. A road transport aircraft unit as claimed in claim 2, characterised in that the location of the inside of the bracket slot (13) in contact with the vertical stabilizer (6) is provided with a polyester vinyl foam.