CN215622787U

CN215622787U - Aircraft starting power supply automobile body stabilizing mean

Info

Publication number: CN215622787U
Application number: CN202122006295.1U
Authority: CN
Inventors: 江炎聪; 邓甲礼
Original assignee: Shanghai Ruiheng Electromechanical Co ltd
Current assignee: Shanghai Ruiheng Electromechanical Co ltd
Priority date: 2021-08-24
Filing date: 2021-08-24
Publication date: 2022-01-25
Anticipated expiration: 2031-08-24

Abstract

The utility model discloses an aircraft starting power supply vehicle body stabilizing mechanism in the technical field of stabilizing mechanisms, which comprises a main body assembly and a stabilizing assembly, wherein the main body assembly comprises a bottom plate, the bottom of the bottom plate is movably connected with a rear wheel, and the bottom of the bottom plate is connected with a middle rod through a bolt. The bottom plate is used for fixing the support rods, the cross rods are fixedly connected among the support rods, the connection strength of the support rods is enhanced through the cross rods, the damping rods are connected to the upper end of the bottom plate, the support springs are connected to the damping rods, the moving ends of the damping rods are connected to the mounting plate, the mounting plate is used for mounting and connecting a power supply, the upper end of each support rod is movably connected with the upper turning plate, the upper turning plate is connected with the lower pressing plate through the limiting rods, the lower pressing plate is in abutting connection with the upper end of the power supply, elasticity is provided through the support springs and the compression springs, the power supply is stably placed in the support rods, and the damping rods are matched with the support springs for damping, so that the stability of the whole power supply vehicle is maintained.

Description

Aircraft starting power supply automobile body stabilizing mean

Technical Field

The utility model relates to the technical field of stabilizing mechanisms, in particular to a vehicle body stabilizing mechanism of an airplane starting power supply.

Background

The aircraft starting power supply is a guarantee power supply for aircraft starting, fully considers the characteristic of being capable of meeting the use requirements under various environmental conditions, is convenient to operate, use and transition, and is designed into a movable structure, the aircraft starting power supply is of a movable traction pulling type and fully-closed metal box type structure, can work under the condition of no power supply in the field, has the operation capacity under the conditions of night and complex weather, an operation switch, an indicator light, various instruments and the like are arranged on a control panel, the operation and performance monitoring are convenient, the starting power supply needs to be stably placed on a vehicle body of a power supply vehicle, and the stable use of the power supply is guaranteed.

SUMMERY OF THE UTILITY MODEL

The utility model aims to provide a vehicle body stabilizing mechanism of an airplane starting power supply, which solves the problems in the background technology.

In order to achieve the purpose, the utility model provides the following technical scheme: the aircraft starting power supply vehicle body stabilizing mechanism comprises a main body component and a stabilizing component, wherein the main body component comprises a bottom plate, the bottom of the bottom plate is movably connected with a rear wheel, the bottom of the bottom plate is connected with a middle rod through a bolt, one end of the middle rod is movably connected with a pull rod, the bottom end of the pull rod is movably connected with a front wheel, the stabilizing component comprises a plurality of supporting rods and a damping rod, the supporting rods are fixedly connected with the upper end of the bottom plate, the upper end of the supporting rod is movably connected with an upper turning plate, the inner part of the upper turning plate is movably clamped with a limiting rod, a compression spring is arranged on the limiting rod, one end of the limiting rod is fixedly connected with a lower pressing plate, the upper turning plate is connected with a fixed plate through bolts, the damping rod is fixedly connected to the upper end of the bottom plate, a supporting spring is mounted on the damping rod, and the movable end of the damping rod is connected with a mounting plate.

Preferably, the middle rod is arranged on the central axis of the bottom plate, and the middle rod and the pull rod are arranged on the same vertical plane.

Preferably, the pull rod is L-shaped, and a front wheel and a rear wheel at the bottom end of the pull rod are arranged on the same horizontal plane.

Preferably, a plurality of transverse cross rods are connected among the support rods and are arranged in a hollow mode.

Preferably, a plurality of groups of mounting holes are formed in the mounting plate, and the upper end of the mounting plate is connected with the rubber layer.

Preferably, the mounting plate is arranged right opposite to the lower pressing plate, and the width of the mounting plate is larger than that of the lower pressing plate.

Preferably, the inside laminating of bracing piece is connected with the guard bar, the guard bar is the preparation of elastic rubber.

Compared with the prior art, the utility model has the beneficial effects that:

(1) the bottom plate is used for fixing a plurality of supporting rods, cross rods are fixedly connected among the supporting rods, the connecting strength of the supporting rods is enhanced through the cross rods, the supporting rods form a frame body for limiting and placing a power supply, the upper end of the bottom plate is connected with a damping rod, a supporting spring is connected onto the damping rod, the moving end of the damping rod is connected with a mounting plate, the mounting plate is used for mounting and connecting the power supply, the upper end of each supporting rod is movably connected with an upper turning plate, the upper turning plate is connected with a lower pressing plate through a limiting rod, the lower pressing plate is in abutting connection with the upper end of the power supply, the power supply is stably placed in the supporting rods, the damping rods are matched with the supporting springs for damping, and the stability of the whole power supply vehicle is maintained;

(2) the bottom of the bottom plate is connected with the two rear wheels, the central part of the bottom plate is connected with the middle rod through the bolt, one end of the middle rod is movably connected with the pull rod, the pull rod is convenient to pull by hands, the bottom end of the pull rod is movably connected with the front wheels, the whole movement of the device is convenient through the front wheels and the rear wheels, the power supply is convenient to move through the moving device, and the whole movement of the power supply vehicle is convenient and fast.

Drawings

In order to more clearly illustrate the technical solutions of the embodiments of the present invention, the drawings used in the description of the embodiments will be briefly introduced below, and it is obvious that the drawings in the following description are only some embodiments of the present invention, and it is obvious for those skilled in the art that other drawings can be obtained according to the drawings without creative efforts.

FIG. 1 is a perspective view of a vehicle body stabilizing mechanism for an aircraft starting power supply of the present invention;

FIG. 2 is a bottom perspective view of the aircraft starting power supply body stabilizing mechanism of the present invention;

FIG. 3 is a side view block diagram of the aircraft starting power supply body stabilizing mechanism of the present invention;

fig. 4 is an overall sectional structural view of the aircraft starting power supply body stabilizing mechanism of the utility model.

In the drawings, the components represented by the respective reference numerals are listed below:

1. a body assembly; 11. a base plate; 12. a rear wheel; 13. a middle rod; 14. a pull rod; 15. a front wheel; 2. a stabilizing assembly; 21. a support bar; 22. a cross bar; 23. a damping lever; 24. a support spring; 25. mounting a plate; 26. an upper turning plate; 27. a restraining bar; 28. a compression spring; 29. a lower pressing plate; 210. a fixing plate; 211. and (4) a protective strip.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

Referring to fig. 1-4, the present invention provides a technical solution: aircraft starting power automobile body stabilizing mean, including main part subassembly 1 and stabilizing component 2, main part subassembly 1 includes bottom plate 11, the bottom swing joint of bottom plate 11 has rear wheel 12, the bottom bolted connection of bottom plate 11 has well pole 13, the one end swing joint of well pole 13 has pull rod 14, the bottom swing joint of pull rod 14 has a front wheel 15, well pole 13 sets up on the center axis of bottom plate 11, well pole 13 sets up on same perpendicular with pull rod 14, pull rod 14 is L shape, the front wheel 15 and the rear wheel 12 setting of pull rod 14 bottom are on same horizontal plane.

Wherein, the bottom of bottom plate 11 is connected with two rear wheels 12, and the central point bolted connection of bottom plate 11 has well pole 13, and the one end swing joint of well pole 13 has pull rod 14, and pull rod 14 is convenient for the pulling of hand, and the bottom swing joint of pull rod 14 has front wheel 15, and the device's of being convenient for overall movement is convenient for through front wheel 15 and rear wheel 12, and the mobile device is convenient for remove the power, and supply vehicle overall movement is convenient.

Referring to fig. 1-4, the stabilizing assembly 2 includes a plurality of support rods 21 and damping rods 23, the support rods 21 are fixedly connected to the upper end of the bottom plate 11, the upper end of the support rods 21 is movably connected to an upper turning plate 26, the inner portion of the upper turning plate 26 is movably clamped to a limiting rod 27, a pressing spring 28 is mounted on the limiting rod 27, a lower pressing plate 29 is fixedly connected to one end of the limiting rod 27, a fixing plate 210 is bolted to the upper turning plate 26, the damping rod 23 is fixedly connected to the upper end of the bottom plate 11, a support spring 24 is mounted on the damping rod 23, a mounting plate 25 is connected to the movable end of the damping rod 23, a transverse cross rod 22 is connected between the support rods 21, the cross rod 22 is hollow, a plurality of sets of mounting holes are formed in the mounting plate 25, a rubber layer is connected to the upper end of the mounting plate 25, the mounting plate 25 is disposed opposite to the lower pressing plate 29, the width of the mounting plate 25 is greater than that of the lower pressing plate 29, a protective strip 211 is attached to the inner portion of the support rods 21, the guard bars 211 are made of elastic rubber.

Wherein, carry out the fixed of a plurality of bracing pieces 21 through bottom plate 11, fixedly connected with horizontal pole 22 between a plurality of bracing pieces 21, strengthen the joint strength of a plurality of bracing pieces 21 through horizontal pole 22, a plurality of bracing pieces 21 form the framework, carry out the spacing placing of power, be connected with damping rod 23 in the upper end of bottom plate 11, be connected with supporting spring 24 on the damping rod 23, the removal end of damping rod 23 is connected with mounting panel 25, mounting panel 25 carries out the erection joint of power, bracing piece 21 upper end swing joint has upward turning plate 26, upward turn plate 26 is last to connect holding down plate 29 through limiting rod 27, holding down plate 29 is contradicted with the power upper end and is connected, provide elasticity through supporting spring 24 and pressure spring 28, let the power stably place inside bracing piece 21, carry out the shock attenuation through damping rod 23 cooperation supporting spring 24, maintain the holistic stability of supply vehicle, excellent in use effect.

The integral working principle is that the bottom of the bottom plate 11 is connected with two rear wheels 12, the central part of the bottom plate 11 is connected with a middle rod 13 through a bolt, one end of the middle rod 13 is movably connected with a pull rod 14, the pull rod 14 is convenient for pulling hands, the bottom end of the pull rod 14 is movably connected with a front wheel 15, the front wheel 15 and the rear wheel 12 are convenient for the integral movement of the device, the moving device is convenient for moving a power supply, the power supply vehicle is convenient and quick to move integrally, the bottom plate 11 is used for fixing a plurality of support rods 21, a cross rod 22 is fixedly connected among the plurality of support rods 21, the cross rod 22 is used for strengthening the connection strength of the plurality of support rods 21, the plurality of support rods 21 form a frame body for limiting and placing the power supply, the damping rod 23 is connected with the upper end of the bottom plate 11, the supporting spring 24 is connected with the damping rod 23, the moving end of the damping rod 23 is connected with a mounting plate 25, and the mounting plate 25 is used for mounting and connecting the power supply, bracing piece 21 upper end swing joint has upward board 26, upward board 26 goes up and connects holding down plate 29 through limiting rod 27, and holding down plate 29 is contradicted with the power upper end and is connected, provides elasticity through supporting spring 24 and pressure spring 28, lets the power stably place inside bracing piece 21, cooperates supporting spring 24 through damping rod 23 to carry out the shock attenuation, maintains the holistic stability of supply vehicle, excellent in use effect.

In the description herein, references to the description of "one embodiment," "an example," "a specific example" or the like are intended to mean that a particular feature, structure, material, or characteristic described in connection with the embodiment or example is included in at least one embodiment or example of the utility model. In this specification, the schematic representations of the terms used above do not necessarily refer to the same embodiment or example. Furthermore, the particular features, structures, materials, or characteristics described may be combined in any suitable manner in any one or more embodiments or examples.

The preferred embodiments of the utility model disclosed above are intended to be illustrative only. The preferred embodiments are not intended to be exhaustive or to limit the utility model to the precise embodiments disclosed. Obviously, many modifications and variations are possible in light of the above teaching. The embodiments were chosen and described in order to best explain the principles of the utility model and the practical application, to thereby enable others skilled in the art to best utilize the utility model. The utility model is limited only by the claims and their full scope and equivalents.

Claims

1. Aircraft start power supply automobile body stabilizing mean, including main part subassembly (1) and stabilizing component (2), its characterized in that: the main body component (1) comprises a bottom plate (11), the bottom of the bottom plate (11) is movably connected with a rear wheel (12), the bottom of the bottom plate (11) is connected with a middle rod (13) through a bolt, one end of the middle rod (13) is movably connected with a pull rod (14), the bottom end of the pull rod (14) is movably connected with a front wheel (15), the stabilizing component (2) comprises a plurality of supporting rods (21) and damping rods (23), the supporting rods (21) are fixedly connected to the upper end of the bottom plate (11), the upper end of the supporting rods (21) is movably connected with an upper turning plate (26), the inner part of the upper turning plate (26) is movably clamped with a limiting rod (27), a compression spring (28) is installed on the limiting rod (27), one end of the limiting rod (27) is fixedly connected with a lower pressing plate (29), the upper turning plate (26) is connected with a fixing plate (210) through a bolt, damping rod (23) fixed connection is in bottom plate (11) upper end, install supporting spring (24) on damping rod (23), the expansion end of damping rod (23) is connected with mounting panel (25).

2. An aircraft starting power body stabilizing mechanism as claimed in claim 1, wherein: the middle rod (13) is arranged on the central axis of the bottom plate (11), and the middle rod (13) and the pull rod (14) are arranged on the same vertical plane.

3. An aircraft starting power body stabilizing mechanism as claimed in claim 1, wherein: the pull rod (14) is L-shaped, and a front wheel (15) and a rear wheel (12) at the bottom end of the pull rod (14) are arranged on the same horizontal plane.

4. An aircraft starting power body stabilizing mechanism as claimed in claim 1, wherein: transverse cross rods (22) are connected among the support rods (21), and the cross rods (22) are arranged in a hollow mode.

5. An aircraft starting power body stabilizing mechanism as claimed in claim 1, wherein: the mounting plate (25) is provided with a plurality of groups of mounting holes, and the upper end of the mounting plate (25) is connected with the rubber layer.

6. An aircraft starting power body stabilizing mechanism as claimed in claim 1, wherein: the mounting plate (25) is arranged right opposite to the lower pressing plate (29), and the width of the mounting plate (25) is larger than that of the lower pressing plate (29).

7. An aircraft starting power body stabilizing mechanism as claimed in claim 1, wherein: the inside laminating of bracing piece (21) is connected with protection strip (211), protection strip (211) are the preparation of elastic rubber.