CN206029735U - Installation director of aircraft carbon brake disc - Google Patents
Installation director of aircraft carbon brake disc Download PDFInfo
- Publication number
- CN206029735U CN206029735U CN201620658725.4U CN201620658725U CN206029735U CN 206029735 U CN206029735 U CN 206029735U CN 201620658725 U CN201620658725 U CN 201620658725U CN 206029735 U CN206029735 U CN 206029735U
- Authority
- CN
- China
- Prior art keywords
- guide rail
- brake disc
- base
- handle
- carbon brake
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Withdrawn - After Issue
Links
Landscapes
- Braking Arrangements (AREA)
Abstract
The utility model discloses an installation director of aircraft carbon brake disc belongs to the aviation equipment technological field, include: adjust guide rail, base, handle seat and handle well, number and the size of adjusting the guide rail well respectively with aircraft main wheel wheel hub in the number and the size of guide rail unanimous, adjust the guide rail well and evenly fix on the up end of base along the circumferencial direction, just adjust the position of guide rail and the position one -to -one of the interior guide rail of aircraft main wheel wheel hub well, the handle passes through the handle seat to be fixed on the lower terminal surface of base, this director can guarantee that the installation of carbon brake disc is convenient, and the atress of carbon brake block is even, improves the installation effectiveness, reduce because of the maintenance reassembles the damage unneccessary loss that the brake disc brought, and simple structure, light, stable performance, use is reliable, can not cause the damage to the carbon brake disc in the use.
Description
Technical field
The utility model belongs to aircraft equipment technical field, and in particular to a kind of installation guider of airplane carbon brake disc.
Background technology
The brake disc of aircraft main wheel is carbon brake disc, is made up of multigroup dynamic and static carbon brake, is also carbon-carbon composite
Brake disc.After maintenance terminates, needs are reinstalled carbon brake disc in main wheel wheel hub.
The features such as carbon brake disc has lightweight and high specific heat, high-melting-point, good impulsive force and higher thermal conductivity.
In installation, due to carbon brake disc material be C-base composte material, when assemble with main wheel again, if due to assembly force inequality and
It is likely to result in damaging if guide effect is bad.
The carbon brake disc of certain model aircraft includes multigroup dynamic and static carbon brake, be all provided with every group of brake block pilot hole with
Guide rail correspondence in wheel hub, so as to after installing each group brake block can circumference it is spacing accurately.If when ressembling without guiding dress
Put, each brake block circumferential opening present position arbitrarily, is that installation increased difficulty, simultaneously because the material problem pole of carbon brake
Stress damage is easily caused, the loss of whole carbon brake disc is directly resulted in.In order to ensure carbon brake disc brake block and wheel when mounted
Guide rail in hub align and installation process in each group brake block uniform force, need design it is a kind of practical, be reliably oriented to work
Tool.
Utility model content
In view of this, the utility model provides a kind of installation guider of airplane carbon brake disc, ensure that carbon brakes
The install convenient of disk, the uniform force of carbon brake improve installation effectiveness, reduce and ressemble damage brake disc institute band because of maintenance
The unnecessary loss for coming, and simple structure, light, stable performance, use reliability, will not be made to carbon brake disc in use
Into damage.
The utility model is achieved through the following technical solutions：
A kind of installation guider of airplane carbon brake disc, including：Align guide rail, base, handle base and handle；
The number and size for aligning guide rail number and consistent size respectively with guide rail in aircraft main wheel wheel hub；
Align guide rail to be along the circumferential direction uniformly fixed on the upper surface of base, and align position and the aircraft main wheel of guide rail
In wheel hub, the position of guide rail corresponds；Handle is fixed on the lower surface of base by handle base.
Further, one end of the handle base is welded and fixed with handle, and the other end is connected with whorl of base.
Further, align guide rail to be fixedly connected with base by screw described in each.
Further, it is described to align guide rail and base is made using aluminum.
Further, the handle base is made using mild steel.
Further, the handle is made using the light-wall pipe of Steel material.
Beneficial effect：The utility model passes through the guide effect for respectively aligning guide rail, it is ensured that each group brake block is when mounted
To positivity and uniformity, reduce installation difficulty, while it also avoid easily causing to receive due to the material problem of carbon brake
Power is damaged, and is reduced and is brought the risk of loss because of maintenance refitting.
Description of the drawings
Fig. 1 is structure composition figure of the present utility model.
Wherein, 1- aligns guide rail, 2- bases, 3- handle bases, 4- handles, screw under 5-, 6- screwings.
Specific embodiment
Develop simultaneously embodiment below in conjunction with the accompanying drawings, and the utility model is described in detail.
The utility model provides a kind of installation guider of airplane carbon brake disc, referring to accompanying drawing 1, including：Align guide rail
1st, base 2, handle base 3, handle 4, lower screw 5 and screwing 6；
The number and size (length and width) for aligning guide rail 1 respectively with the number of guide rail in aircraft main wheel wheel hub and
Consistent size, the length for aligning guide rail 1 in the present embodiment are 240mm, a diameter of 500mm of the base 2；Align guide rail 1
Made using aluminum with base 2 so that the guider is lighter；
The handle base 3 is made using mild steel；
The handle 4 is made using the light-wall pipe of Steel material；
Align guide rail 1 to be distributed uniformly and circumferentially in the upper surface of base 2 described in nine, each aligns guide rail 1 and passes through
Lower screw 5 and screwing 6 are fixedly connected with base 2；And nine positions for aligning guide rail 1 and nine guide rails in aircraft main wheel wheel hub
Position correspond；Handle 4 is fixed on the another lower surface of base 2 by handle base 3, wherein, one end point of two handle bases 3
4 two ends of handle are not weldingly fixed on, the other end is threaded connection with base 2；
Operation principle：When deployed, by the opening of each group brake block on brake disc and guider respectively align guide rail 1 carry out it is right
Just install, it is ensured that each group brake block opening is consistent, be then directed to device and respectively align guide rail 1 and the guide rail pair in aircraft main wheel wheel hub
Connect, brake disc is installed by promoting handle 4 carbon brake disc slowly to be pushed in main wheel wheel hub, it is ensured that the carbon in installation process
Brake disc intact and install align accuracy, be directed to device after brake disc installation and exit；Simple structure, light, property
Can stablize, use reliability, will not carbon brake disc be caused to damage in use.
In sum, preferred embodiment of the present utility model is these are only, is not intended to limit of the present utility model
Protection domain.It is all it is of the present utility model spirit and principle within, any modification, equivalent substitution and improvements made etc. all should be wrapped
It is contained within protection domain of the present utility model.
Claims (6)
1. the installation guider of a kind of airplane carbon brake disc, it is characterised in that include：Align guide rail (1), base (2), handle base
And handle (4) (3)；
The number and size for aligning guide rail (1) number and consistent size respectively with guide rail in aircraft main wheel wheel hub；
Align guide rail (1) to be along the circumferential direction uniformly fixed on the upper surface of base (2), and align the position of guide rail (1) and fly
In owner's wheel wheel hub, the position of guide rail corresponds；Handle (4) is fixed on the lower surface of base (2) by handle base (3).
2. a kind of installation guider of airplane carbon brake disc as claimed in claim 1, it is characterised in that the handle base (3)
One end be welded and fixed with handle (4), the other end is threadedly coupled with base (2).
3. the installation guider of a kind of airplane carbon brake disc as claimed in claim 1, it is characterised in that align described in each and lead
Rail (1) is fixedly connected with base (2) by screw.
4. the installation guider of a kind of airplane carbon brake disc as claimed in claim 1, it is characterised in that described to align guide rail
(1) made using aluminum with base (2).
5. a kind of installation guider of airplane carbon brake disc as claimed in claim 1, it is characterised in that the handle base (3)
Made using mild steel.
6. the installation guider of a kind of airplane carbon brake disc as claimed in claim 1, it is characterised in that the handle (4) is adopted
Made with the light-wall pipe of Steel material.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620658725.4U CN206029735U (en) | 2016-06-29 | 2016-06-29 | Installation director of aircraft carbon brake disc |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201620658725.4U CN206029735U (en) | 2016-06-29 | 2016-06-29 | Installation director of aircraft carbon brake disc |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206029735U true CN206029735U (en) | 2017-03-22 |
Family
ID=58313150
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201620658725.4U Withdrawn - After Issue CN206029735U (en) | 2016-06-29 | 2016-06-29 | Installation director of aircraft carbon brake disc |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206029735U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105922190A (en) * | 2016-06-29 | 2016-09-07 | 中国人民解放军第五七〇六工厂 | Mounting guider of aircraft carbon brake disc |
-
2016
- 2016-06-29 CN CN201620658725.4U patent/CN206029735U/en not_active Withdrawn - After Issue
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105922190A (en) * | 2016-06-29 | 2016-09-07 | 中国人民解放军第五七〇六工厂 | Mounting guider of aircraft carbon brake disc |
| CN105922190B (en) * | 2016-06-29 | 2018-01-23 | 中国人民解放军第五七〇六工厂 | A kind of installation guider of airplane carbon brake disc |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN201679646U (en) | Lightning shielding receiver of lightning shielding system of fan blade | |
| CN206029735U (en) | Installation director of aircraft carbon brake disc | |
| CN106143881B (en) | A kind of unmanned plane deceleration damping undercarriage | |
| CN106438192A (en) | Sectional type wind power generation blade connecting structure and method | |
| CN105883508A (en) | Take-up device of low-smoke halogen-free electric wire | |
| CN105922190B (en) | A kind of installation guider of airplane carbon brake disc | |
| CN103586835A (en) | Replacing tool for high-speed shaft bearing outer ring of wind generating set gearbox and using method | |
| CN104128792B (en) | A kind of the Worker's Stadium vertical locating device and assembly method thereof | |
| CN202811232U (en) | Lightning protection device for pitch bearing of permanent magnetic direct drive wind force generator unit | |
| CN206742766U (en) | A kind of mountain area distribution transformer low-pressure line-outgoing cable stationary barrier | |
| CN203273014U (en) | Communication base station angle steel tower vent pipe fastening device | |
| CN109877726A (en) | A kind of automotive wheel maintenance fixture | |
| CN205414457U (en) | Activity clamping head | |
| CN204565594U (en) | A kind of synchronous pre-tightening apparatus of the bolt group for end-tooth shaft coupling | |
| CN207521959U (en) | Trolley coach bogie frame Multi-stage regulating type auxiliary locator | |
| CN104131521B (en) | A kind of corrugated tube unit spliced folder and application thereof | |
| CN206059098U (en) | A kind of erecting device of adjustment fan of dry type transformer angle | |
| CN202628403U (en) | Integrated lightning protection device for fan blade | |
| CN203883339U (en) | Installation pedestal for distribution box | |
| CN202363811U (en) | Cross arm clamping device for replacing insulator of direct-current 500kv straight-line string | |
| CN202441193U (en) | General adjustable column of shield door of subway platform | |
| CN104493475A (en) | Synchronous pre-tightening device for bolt group of end surface gear shaft coupling | |
| CN204828397U (en) | Brake disc that heat dispersion is good | |
| CN203494946U (en) | Wire inlet guide wheel component on elephant trunk type wire-rewinding machine | |
| CN205274862U (en) | Card formula chuck is installed and removed fast to axle head |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20170322 Effective date of abandoning: 20180123 |