CN218751403U

CN218751403U - Aviation side pedal support with composite coating

Info

Publication number: CN218751403U
Application number: CN202222911681.XU
Authority: CN
Inventors: 郭娇尔卿
Original assignee: Zhejiang Jiahang Technology Co ltd
Current assignee: Zhejiang Jiahang Technology Co ltd
Priority date: 2022-11-02
Filing date: 2022-11-02
Publication date: 2023-03-28
Anticipated expiration: 2032-11-02

Abstract

The utility model discloses an aviation side pedal support with composite coating, which comprises a side pedal, wherein the composite coating is sprayed on the outer side of the side pedal, the top and the bottom of the inner side of the side pedal are both provided with elastic sheets, one side of the side pedal is provided with a mounting plate, the top and the bottom of one side of the mounting plate, which is far away from the side pedal, are both provided with clamping grooves, the insides of the two groups of clamping grooves are both clamped with internal thread sleeves, and the insides of the two groups of internal thread sleeves are both provided with threaded rods in a threaded sleeve manner; the utility model discloses a magnet, gag lever post, cardboard, threaded rod, mounting panel, internal thread sleeve and draw-in groove mutually support, can realize the installation work of this side footboard, still can make things convenient for the quick detach work in operating personnel later stage simultaneously for the operating personnel later stage only needs to carry out screw thread rotation, demolishs work when just can realize two sets of internal thread sleeves, in order to reduce operating personnel work step, improves its work efficiency.

Description

Aviation side pedal support with composite coating

Technical Field

The utility model relates to a side footboard support technical field specifically is an aviation side footboard support with composite coating.

Background

The pedal is a treading-assisted part which is arranged for facilitating passengers and drivers to get on and off the bus, along with the continuous improvement of aviation production technology and the continuous development of markets, the requirements of people on aviation are more and more refined, and not only performance but also details are required, so that more humanized aviation is more competitive, and an aviation side pedal bracket with a composite coating needs to be designed;

the prior side pedal bracket has the following inconveniences in the using process: 1. the existing side pedal has a single internal structure, most surfaces of the existing side pedal are not coated with the composite coating, so that the side pedal is rusted and damaged after being used for a long time, the service life of the existing side pedal is shortened, meanwhile, the existing side pedal is not provided with a buffer mechanism, so that the side pedal is deformed after being used for a long time, and the damage efficiency is reduced; 2. when the existing side pedal is detached and overhauled, the operation mode is relatively complex because the operation personnel needs to twist a plurality of groups of threads to remove the operation, so that the complexity of detaching the side pedal is reduced, and the working steps of the operation personnel are increased.

SUMMERY OF THE UTILITY MODEL

An object of the utility model is to provide an aviation side pedal support with composite coating to propose current side pedal support in the use among the solution above-mentioned background art, can meet following inconvenient part: 1. the existing side pedal has a single internal structure, and most surfaces of the existing side pedal are not coated with a composite coating, so that the side pedal is rusted and damaged after being used for a long time, the service life of the existing side pedal is shortened, and meanwhile, the side pedal can be deformed after being used for a long time, and the damage efficiency is reduced; 2. when the existing side pedal is detached and overhauled, the operation mode is relatively complex because the operation personnel needs to twist a plurality of groups of threads to remove the operation, so that the complexity of detaching the side pedal is reduced, and the working steps of the operation personnel are increased.

In order to achieve the above object, the utility model provides a following technical scheme: the utility model provides an aviation side footboard support with composite coating, includes the side footboard, the outside spraying of side footboard has composite coating, the inboard top and the bottom of side footboard all are equipped with the flexure strip, one side of side footboard is equipped with the mounting panel, the top and the bottom that side footboard one side was kept away from to the mounting panel all are equipped with the draw-in groove, and are two sets of the inside all blocks of draw-in groove have the internal thread sleeve, and are two sets of the internal thread telescopic inside all thread bush is equipped with the threaded rod, and is two sets of the threaded rod is kept away from internal thread telescopic one side and all is equipped with the cardboard, the inside of mounting panel is run through and is equipped with through the inside gag lever post of two sets of internal thread sleeves, the bottom and the top of mounting panel one side and the top and the bottom of gag lever post all are equipped with the magnet, and two sets of magnet mutual absorption.

Preferably, the inside of mounting panel and the inside one side that is close to the mounting panel of two sets of internal thread sleeves all are equipped with logical groove, and lead to the groove and mutually support with the spacing cardboard of gag lever post top and bottom design, and spacing cardboard and gag lever post interconnect.

Preferably, the composite coating consists of a phosphate coating and a rust-proof layer.

Preferably, the top of side footboard evenly is equipped with the antislip strip, and the outside of antislip strip evenly is equipped with anti-skidding line.

Preferably, two sets of cardboard keep away from one side of threaded rod all is equipped with the handle, and the outside cover of handle is equipped with anti-skidding cover.

Preferably, through holes are uniformly formed in the side pedal.

Compared with the prior art, the beneficial effects of the utility model are that: the aviation side pedal bracket provided with the composite coating;

1. through the mutual matching of the magnet, the limiting rod, the clamping plate, the threaded rod, the mounting plate, the internal thread sleeves and the clamping groove, the mounting work of the side pedal can be realized, and meanwhile, the later-stage quick-dismantling work of an operator can be facilitated, so that the operator can realize the simultaneous dismantling work of the two groups of internal thread sleeves only by performing one-time thread rotation in the later stage, the working steps of the operator are reduced, and the working efficiency of the operator is improved;

2. through the design of flexure strip, can effectually alleviate the pressure when this side footboard uses to slow down its deformation phenomenon, improve its life, can realize the guard work in the offside footboard outside through composite biocoating's design simultaneously, effectually prevent that it from producing corrosion damage phenomenon, improve its life once more, and this structural design is simple reasonable to be suitable for the popularization.

Drawings

Fig. 1 is a front sectional view of the present invention;

fig. 2 is a schematic perspective view of a side pedal of the present invention;

fig. 3 is a front view of the present invention.

In the figure: 1. a side pedal; 2. a composite coating; 3. a magnet; 4. a limiting rod; 5. clamping a plate; 6. a threaded rod; 7. mounting a plate; 8. an internally threaded sleeve; 9. a card slot; 10. an elastic sheet.

Detailed Description

The technical solutions in the embodiments of the present invention will be described clearly and completely with reference to the accompanying drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only some embodiments of the present invention, not all embodiments. Based on the embodiments in the present invention, all other embodiments obtained by a person skilled in the art without creative efforts all belong to the protection scope of the present invention.

Referring to fig. 1-3, the present invention provides an embodiment: the utility model provides an aviation side footboard support with composite coating, including side footboard 1, the outside spraying of side footboard 1 has composite coating 2, 1 inboard top and the bottom of side footboard all are equipped with flexure strip 10, one side of side footboard 1 is equipped with mounting panel 7, the top and the bottom that 1 one side of side footboard was kept away from to mounting panel 7 all are equipped with draw-in groove 9, the inside block of two sets of draw-in grooves 9 has internal thread sleeve 8 all, the inside all thread bush of two sets of internal thread sleeve 8 is equipped with threaded rod 6, one side that internal thread sleeve 8 was kept away from to two sets of threaded rod 6 all is equipped with cardboard 5, the inside of mounting panel 7 is run through and is equipped with through the inside gag lever post 4 of two sets of internal thread sleeve 8, the bottom and the top of gag lever post 4 and the top and the bottom of mounting panel 7 one side all are equipped with magnet 3, and two sets of magnet 3 adsorb each other, be convenient for realize the block phenomenon of inserting of gag lever post 4.

Further, the inside of mounting panel 7 and the inside one side that is close to mounting panel 7 of two sets of internal thread sleeves 8 all are equipped with logical groove, and lead to the groove and mutually support with the spacing cardboard of 4 tops of gag lever post and bottom designs, and spacing cardboard and 4 interconnect of gag lever post, are convenient for realize the block phenomenon of inserting of gag lever post 4.

Furthermore, the composite coating 2 consists of a phosphating layer and an antirust layer, so that the service life of the side pedal is prolonged, and the phenomenon of corrosion damage is reduced.

Further, the top of side footboard 1 evenly is equipped with the antislip strip, and the outside of antislip strip evenly is equipped with anti-skidding line, is convenient for increase friction and prevents the slip phenomenon.

Further, one side that threaded rod 6 was kept away from to two sets of cardboard 5 all is equipped with the handle, and the outside cover of handle is equipped with anti-skidding cover, is convenient for rotate.

Furthermore, through holes are uniformly formed in the side pedal 1, so that the anti-skidding effect is further improved.

The working principle is as follows: the electric parts of the device are all supplied with power by a storage battery, during work, an operator directly takes the side pedal 1 and the parts above the side pedal, then drives the threaded rod 6 to rotate in the inner threaded sleeve 8 through the clamping plate 5, so that the clamping plate 5 is in a horizontal state, later-stage insertion is facilitated, then the inner threaded sleeve 8 is inserted to a position to be installed, at the moment, the clamping plate 5 is in a vertical state through reverse rotation of the clamping plate 5, installation clamping work of the side pedal 1 and the parts above the side pedal can be realized, then when the side pedal 1 needs to be disassembled, the operator only needs to rotate the limiting rod 4 to drive the two groups of magnet stones 3 to be away from each other to remove adsorption work, and then the limiting rod 4 can be pulled to be separated from the inner threaded sleeve 8 and the installation plate 7, so that quick disassembling work of the side pedal 1 can be realized;

through the design of flexure strip 10, can effectually alleviate the pressure when this side footboard uses to slow down its deformation phenomenon, improve its life, the protection work in 1 outside of offside footboard can be realized through composite coating 2's design simultaneously, effectually prevents that it from producing the corrosion damage phenomenon, improves its life once more.

It is obvious to a person skilled in the art that the invention is not restricted to details of the above-described exemplary embodiments, but that it can be implemented in other specific forms without departing from the spirit or essential characteristics of the invention. The present embodiments are therefore to be considered in all respects as illustrative and not restrictive, the scope of the invention being indicated by the appended claims rather than by the foregoing description, and all changes which come within the meaning and range of equivalency of the claims are therefore intended to be embraced therein. Any reference sign in a claim should not be construed as limiting the claim concerned.

In the description of the present invention, "a plurality" means two or more unless otherwise specified; the terms "upper", "lower", "left", "right", "inner", "outer", "front", "rear", "head", "tail", and the like indicate orientations or positional relationships based on the orientations or positional relationships shown in the drawings, and are merely for convenience of description and simplicity of description, and do not indicate or imply that the device or element being referred to must have a particular orientation, be constructed and operated in a particular orientation, and thus, should not be construed as limiting the present invention. Furthermore, the terms "first," "second," "third," and the like are used for descriptive purposes only and are not to be construed as indicating or implying relative importance.

In the description of the present invention, it is to be noted that, unless otherwise explicitly specified or limited, the terms "connected" and "connected" are to be interpreted broadly, e.g., as either a fixed connection or a detachable connection; can be mechanically or electrically connected; may be directly connected or indirectly connected through an intermediate. The specific meaning of the above terms in the present invention can be understood in specific cases to those skilled in the art.

Claims

1. The utility model provides an aviation side footboard support with composite coating, includes side footboard (1), its characterized in that: the outside spraying of side footboard (1) has composite coating (2), the top and the bottom of side footboard (1) inboard all are equipped with flexure strip (10), one side of side footboard (1) is equipped with mounting panel (7), top and bottom that side footboard (1) one side was kept away from in mounting panel (7) all are equipped with draw-in groove (9), and are two sets of the inside of draw-in groove (9) all blocks female thread sleeve (8), and is two sets of the inside all thread bush of female thread sleeve (8) is equipped with threaded rod (6), and is two sets of one side that female thread sleeve (8) were kept away from in threaded rod (6) all is equipped with cardboard (5), the inside of mounting panel (7) is run through and is equipped with through inside gag lever post (4) of two sets of female thread sleeve (8), the top and the top of mounting panel (7) one side of gag lever post (4) all are equipped with magnet (3), and two sets of magnet (3) adsorb each other.

2. The aviation side pedal bracket provided with the composite coating according to claim 1, characterized in that: the inside of mounting panel (7) and two sets of internal thread sleeve (8) inside one side that is close to mounting panel (7) all are equipped with logical groove, and lead to the groove and mutually support with the spacing cardboard of gag lever post (4) top and bottom design, and spacing cardboard and gag lever post (4) interconnect.

3. The aviation side pedal bracket provided with the composite coating according to claim 1, characterized in that: the composite coating (2) consists of a phosphating layer and an anti-rust layer.

4. The aviation side pedal bracket provided with the composite coating according to claim 1, characterized in that: the top of side footboard (1) evenly is equipped with the antislip strip, and the outside of antislip strip evenly is equipped with anti-skidding line.

5. The aviation side pedal bracket provided with the composite coating according to claim 1, characterized in that: two sets of cardboard (5) keep away from one side of threaded rod (6) and all are equipped with the handle, and the outside cover of handle is equipped with anti-skidding cover.

6. The aviation side pedal bracket provided with the composite coating according to claim 1, characterized in that: through holes are uniformly formed in the side pedal (1).