CN213393032U

CN213393032U - Supporting tool for integrated rack bonding reinforcing rib

Info

Publication number: CN213393032U
Application number: CN202020931193.3U
Authority: CN
Inventors: 黄浩; 朱国杰
Original assignee: Guizhou General Aviation Co ltd
Current assignee: Guizhou General Aviation Co ltd
Priority date: 2020-05-28
Filing date: 2020-05-28
Publication date: 2021-06-08
Anticipated expiration: 2030-05-28

Abstract

The utility model discloses a supporting tool for an integrated frame bonding reinforcing rib, which comprises a vertical plate (1), wherein the lower part of the vertical plate (1) is provided with a bayonet (2) of a main beam of an airplane, the upper end of the vertical plate (1) is provided with a clip placing rack (3), and a clip (4) capable of sliding left and right on the clip placing rack (3) is arranged on the clip placing rack; the utility model discloses can be convenient for support the stiffening rib.

Description

Supporting tool for integrated rack bonding reinforcing rib

Technical Field

The utility model relates to an integral type frame bonding supporting tool for stiffening rib belongs to aircraft frame body production and uses the instrument field.

Background

In the production of wings, reinforcing ribs need to be added on two sides of a main girder, the reinforcing ribs are bonded between the main girder and a wing shell, in the bonding process of the bonding of the reinforcing ribs, because the reinforcing ribs need to be vertically arranged until viscose is condensed and fastened, an auxiliary supporting device needs to be used in the process, the two sides of the reinforcing ribs are respectively supported by supporting rods through the existing auxiliary supporting devices, and therefore the supporting effect can be achieved, the supporting is troublesome, and the supporting is scattered.

Namely: there is a need for a bracing tool for a stiffener that facilitates bracing of the stiffener.

Disclosure of Invention

The utility model aims to solve the technical problem of providing a supporting tool for an integrated frame bonding reinforcing rib, which can be convenient for supporting the reinforcing rib; the defects of the prior art can be overcome.

The technical scheme of the utility model is that: the utility model provides an integral type frame bonding bracing tool for stiffening rib, it includes vertical board, is equipped with the bayonet socket of aircraft girder at vertical board lower part, is equipped with the clip rack on vertical board, is equipped with the clip that can slide about on the clip rack.

And horizontal plates extending to the two sides of the vertical plate are arranged on the top surfaces of the bayonets.

The clamp placing rack comprises a horizontal rod arranged along the longitudinal direction of a vertical plate, a vertical rod connected with the vertical plate is arranged at one end of the horizontal rod, and a limiting rod is arranged at the other end of the horizontal rod.

The clamp comprises a left clamp body and a right clamp body which are hinged, arc-shaped elastic iron sheets are arranged on the left clamp body and the right clamp body, and the clamp placing frame is located between the upper end of the left clamp body and the upper end of the right clamp body and the arc-shaped elastic iron sheets.

Compared with the prior art, the utility model discloses a supporting tool for an integrated frame bonding reinforcing rib, which comprises a vertical plate, wherein the lower part of the vertical plate is provided with a bayonet of an airplane girder, the upper end of the vertical plate is provided with a clip placing rack, and a clip capable of sliding left and right on the clip placing rack is arranged on the clip placing rack; in the structure, when the reinforcing rib is used, after the reinforcing rib is bonded, the vertical plate is closely attached to and limited on one side of the reinforcing rib, the bayonet is clamped on the airplane main beam, the vertical plate on the other side of the bayonet can also simultaneously fix the reinforcing rib on the other side of the airplane main beam, and then the vertical plate and the reinforcing rib are simultaneously clamped through the clamp to realize the positioning and supporting functions; meanwhile, the clamp placing frame is beneficial to limiting the clamp, and the clamp is prevented from falling down in an integrated structure; the top surface of the bayonet is provided with the horizontal plates extending towards the two sides of the vertical plate, so that when the horizontal plates are placed, the horizontal plates are attached to the plate surface of the airplane main beam, and the vertical plates are prevented from inclining; the clamp placing rack comprises a horizontal rod arranged along the longitudinal direction of a vertical plate, the vertical rod is connected with the vertical plate in one end of the horizontal rod, a limiting rod is arranged at the other end of the horizontal rod, and the clamp placing rack can limit the clamp and prevent the clamp from falling off.

Drawings

In order to make the objects, technical solutions and advantages of the present invention clearer, the present invention will be further described in detail with reference to the accompanying drawings, in which:

fig. 1 is a schematic perspective view of the present invention.

Fig. 2 is a schematic diagram of the disassembled structure of fig. 1.

Fig. 3 is a schematic perspective view of another angle of the present invention.

Fig. 4 is a schematic perspective view of another angle of the present invention.

Fig. 5 is a schematic view of the connection structure of the clip of the present invention.

Wherein the vertical plate 1; a bayonet 2; a clip placing rack 3; a clip 4; a horizontal plate 5; a horizontal bar 6; a vertical rod 7; and a limiting rod 8.

Detailed Description

Hereinafter, preferred embodiments of the present invention will be described in detail with reference to the accompanying drawings. It should be understood that the preferred embodiments are for purposes of illustration only and are not intended to limit the scope of the present invention.

Embodiment 1. as shown in fig. 1, a supporting tool for an integrated rack bonding reinforcing rib comprises a vertical plate 1, wherein a bayonet 2 of an airplane main beam is arranged at the lower part of the vertical plate 1, and horizontal plates 5 extending to two sides of the vertical plate 1 are arranged on the top surface of the bayonet; the upper end of the vertical plate 1 is provided with a clamp placing frame 3, and the clamp placing frame 3 is provided with a clamp 4 capable of sliding left and right thereon.

The clip rack 3 include the horizon bar 6 that sets up along 1 lengthwise direction of vertical board, be equipped with the vertical pole 7 with 1 interconnect of vertical board in the one end of horizon bar 6, be equipped with gag lever post 8 at the other end. The clamp 4 include about articulated folder, be equipped with arc elasticity iron sheet on controlling the folder, the clamp rack 3 be located about between folder upper end and the arc elasticity iron sheet.

When the aircraft main beam fixing device is used, after the reinforcing ribs are bonded, the vertical plate 1 is closely attached to and limited on one side of the reinforcing ribs, the bayonet 2 is clamped on the aircraft main beam, the vertical plate on the other side of the bayonet 2 can also simultaneously fix the reinforcing ribs on the other side of the aircraft main beam, and then the vertical plate 1 and the reinforcing ribs are simultaneously clamped through the clamp 4 to realize the positioning and supporting functions; simultaneously, clip rack 3 is favorable to spacing clip 4 to the structure of integration avoids dropping of clip 4.

Finally, the above embodiments are only used for illustrating the technical solutions of the present invention and not for limiting, and although the present invention has been described in detail with reference to the preferred embodiments, it should be understood by those skilled in the art that modifications or equivalent substitutions may be made to the technical solutions of the present invention without departing from the spirit and scope of the technical solutions, and all of them should be covered by the scope of the claims of the present invention.

Claims

1. The utility model provides an integral type frame bonding bracing tool for stiffening rib which characterized in that: the aircraft main beam clamp comprises a vertical plate (1), wherein a bayonet (2) of an aircraft main beam is arranged at the lower part of the vertical plate (1), a clamp placing frame (3) is arranged at the upper end of the vertical plate (1), and a clamp (4) capable of sliding left and right is arranged on the clamp placing frame (3).

2. The support tool for an integral type frame bonding stiffener according to claim 1, wherein: and horizontal plates (5) extending towards the two sides of the vertical plate (1) are arranged on the top surfaces of the bayonets.

3. The support tool for an integral type frame bonding stiffener according to claim 1, wherein: the clamp placing rack (3) comprises a horizontal rod (6) arranged along the longitudinal direction of the vertical plate (1), a vertical rod (7) connected with the vertical plate (1) is arranged at one end of the horizontal rod (6), and a limiting rod (8) is arranged at the other end of the horizontal rod.

4. The support tool for an integral type frame bonding stiffener according to claim 1, wherein: the clamp (4) comprises a left clamp and a right clamp which are hinged, an arc elastic iron sheet is arranged on the left clamp and the right clamp, and the clamp placing frame (3) is positioned between the upper end of the left clamp and the upper end of the right clamp and the arc elastic iron sheet.