CN108799374A - A kind of airplane wheel disk type brake wear indicating device - Google Patents
A kind of airplane wheel disk type brake wear indicating device Download PDFInfo
- Publication number
- CN108799374A CN108799374A CN201810425910.2A CN201810425910A CN108799374A CN 108799374 A CN108799374 A CN 108799374A CN 201810425910 A CN201810425910 A CN 201810425910A CN 108799374 A CN108799374 A CN 108799374A
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- CN
- China
- Prior art keywords
- displacement transducer
- linear displacement
- cylinder block
- airplane wheel
- disk type
- 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.)
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D66/00—Arrangements for monitoring working conditions, e.g. wear, temperature
- F16D66/02—Apparatus for indicating wear
- F16D66/021—Apparatus for indicating wear using electrical detection or indication means
- F16D66/028—Apparatus for indicating wear using electrical detection or indication means with non-electrical sensors or signal transmission, e.g. magnetic, optical
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- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Braking Arrangements (AREA)
Abstract
The invention belongs to airplane wheel brake control technologies, are related to a kind of airplane wheel disk type brake wear indicating device.The present invention includes linear displacement transducer, cylinder block, indicating arm, brake disc component；The linear displacement transducer is the movable transformer of iron core, and the linear displacement transducer is in integrally hollow cylindrical, and the linear displacement transducer center is through-hole, and there are screw threads for the linear displacement transducer outer surface；The cylinder block is a part for airplane wheel brake device assembly, and the cylinder block is arranged mounting hole, is provided with and the matched internal thread of linear displacement transducer in the mounting hole；The linear displacement transducer is installed in the mounting hole of cylinder block；The brake disc component is fastenedly connected with indicating arm.
Description
Technical field
The invention belongs to airplane wheel brake control technologies, are related to a kind of airplane wheel disk type brake wear indicating device.
Background technology
In airplane wheel brake control system, brake disc is the critical component for influencing aircraft landing safety, brake disc
Performance and state of wear will directly affect whether aircraft normally landing and can ensure the safety of personnel and aircraft, work as brake disc
When may wear to certain thickness, it is necessary to replace brake disc.Therefore, brake disc state of wear is ground crew after aircraft lands every time
The inspection item that must carry out.
However, the airplane wheel disk type brake wear indicating device overwhelming majority is mechanical instruction form at present, then brake disc
State of wear need to rely on artificial visual inspection, and this hand inspection increases the work load of ground crew, and is not easy to be stopped
Hull wear data, need by manual measurement brake disc thickness and adopt by some way carry out data inputting and etc. record
Brake disc wear data is brought inconvenience for the course line of brake disc using analysis.
Invention content
The purpose of the present invention is in view of the foregoing drawbacks, provide a kind of airplane wheel disk type brake wear indicating device.
The technical scheme is that：A kind of airplane wheel disk type brake wear indicating device, including straight-line displacement sensing
Device, cylinder block, indicating arm, brake disc component；The linear displacement transducer is the movable transformer of iron core, and the straight-line displacement passes
Sensor is in integrally hollow cylindrical, and the linear displacement transducer center is through-hole, and the linear displacement transducer outer surface is deposited
In screw thread,；The cylinder block is a part for airplane wheel brake device assembly, and mounting hole, the peace is arranged in the cylinder block
Dress is provided with and the matched internal thread of linear displacement transducer in hole；The linear displacement transducer is installed on the peace of cylinder block
It fills in hole；The indicating arm includes pull rod, iron core；The indicating arm is matched with linear displacement transducer, and indicating arm is through straight
Linear movement pick-up through-hole；The iron core is located in linear displacement transducer through-hole；The indicating arm is straight through cylinder block simultaneously
Linear movement pick-up mounting hole, and stretches out cylinder seat outer end face；The brake disc component is fastenedly connected with indicating arm.
Further, there are fuse holes, the cylinder block outer end face there is insurance for the linear displacement transducer outer end
Wire hole.
Further, fuse by the fuse hole of linear displacement transducer and cylinder block by linear displacement transducer with
Cylinder block is attached.
Further, the indicating arm further includes adjusting washer (disk), and the adjusting washer (disk) is for adjusting plunger position.
The invention has the advantages that：The automatic inspection for airplane wheel brake mill damage state can be achieved in the present invention；
The present invention can export the abrasion variable quantity that brake disc is fallen from the aircraft period, convenient for brake control system to brake disc performance and
The analysis of use state；Present invention preserves traditional mechanical wears to indicate form, when linear displacement transducer failure, still
Provide a convenient the mode of ground crew's check brakes mill damage state；The configuration of the present invention is simple can carry out module metaplasia
Production has prodigious engineering promotional value.
Description of the drawings
Fig. 1 is the sectional structure chart of the present invention；
In figure：1, linear displacement transducer, 2, cylinder block, 3, indicating arm, 4, brake disc component.
Fig. 2 is indicating arm sectional structure chart of the present invention；
In figure：31, pull rod, 32, iron core, 33, adjusting washer.
Specific implementation mode
The following further describes the specific embodiments of the present invention with reference to the drawings.
Referring to Fig.1, Fig. 2, a kind of airplane wheel disk type brake wear indicating device is by linear displacement transducer 1, cylinder block
2, indicating arm 3, brake disc component 4 form.
Whole linear displacement transducer 1 is in hollow cylindrical, and there are screw threads for outer surface, and pass through screw thread and cylinder block 2
On sensor mounting hole be fastenedly connected.The outer end face of linear displacement transducer 1 is limited step, realizes linear displacement transducer
1 with cylinder block 2 install when limit function.
Further, there are fuse holes on the limited step of linear displacement transducer 1 and cylinder block 2, pass through fuse
Ensure that loose phenomenon will not occur after linear displacement transducer 1 is installed.
Indicating arm 3 is hinged with brake disc component 4.Indicating arm 3 runs through 1 central through hole of linear displacement transducer, and stretches out straight
The state of wear of hand inspection brake disc component 4 is convenient in 2 end face of limited step end face and cylinder block of linear movement pick-up 1.
Further, indicating arm is made of pull rod 31, iron core 32, adjusting washer 33.In whole assembly of the invention, pass through
The adjusting washer 33 for increasing different number, different length on pull rod 31, adjusts 32 position of iron core, it is ensured that after whole assembly, iron
32 position of core is in inside 1 central through hole of linear displacement transducer.
In aircraft operational process, due to the use of wheel braking, 4 thickness of brake assemblies is caused to gradually reduce, indicating arm 3
On iron core 32 reduce synchronizing moving to the right with the thickness of brake disc component 4.Ultimately cause the output on linear displacement transducer 1
Corresponding variation occurs for signal.
The operation principle of the present invention is that the linear displacement transducer is installed on the cylinder block, and by fuse into
Row loosens connection, it is ensured that linear displacement transducer will not loosen.The indicating arm is installed on the brake assemblies, when winged
After machine wheel brake is completed, the indicating arm runs through the linear displacement transducer central through hole, and the instruction
The iron core of bar is located in the linear displacement transducer through-hole.After airplane wheel brake mill damage, due to brake disc thickness
Reduce, the indicating arm plunger position changes in the linear displacement transducer through-hole, to make the straight-line displacement
Sensor generates different output signals.Present invention is mainly used for all types of aircrafts using disk type brake wheel to carry out brake disc
Abrasion instruction and analysis.
Claims (5)
1. a kind of airplane wheel disk type brake wear indicating device, it is characterized in that：The airplane wheel disk type brake abrasion instruction
Device includes linear displacement transducer, cylinder block, indicating arm, brake disc component；The linear displacement transducer is that iron core is movable
Transformer, the linear displacement transducer are in integrally hollow cylindrical, and the linear displacement transducer center is through-hole, described straight
There are screw threads for linear movement pick-up outer surface；The cylinder block is a part for airplane wheel brake device assembly, the cylinder
Mounting hole is arranged in seat, is provided with and the matched internal thread of linear displacement transducer in the mounting hole；The straight-line displacement passes
Sensor is installed in the mounting hole of cylinder block；The indicating arm includes pull rod, iron core；The indicating arm and linear displacement transducer
It matches, indicating arm runs through linear displacement transducer through-hole；The iron core is located in linear displacement transducer through-hole；The instruction
Bar runs through cylinder block linear displacement transducer mounting hole, and stretches out cylinder seat outer end face simultaneously；The brake disc component and instruction
Bar is fastenedly connected.
2. airplane wheel disk type brake wear indicating device according to claim 1, it is characterized in that：The straight-line displacement passes
There are fuse holes for sensor outer end, and there are fuse holes for the cylinder block outer end face.
3. airplane wheel disk type brake wear indicating device according to claim 2, it is characterized in that：The airplane wheel disk
Formula brake wear indicating device further includes fuse, the fuse hole that the fuse passes through linear displacement transducer and cylinder block
Linear displacement transducer and cylinder block are attached.
4. airplane wheel disk type brake wear indicating device according to claim 1, it is characterized in that：The indicating arm also wraps
Adjusting washer (disk) is included, the adjusting washer (disk) is for adjusting plunger position.
5. airplane wheel disk type brake wear indicating device according to claim 1, it is characterized in that：The straight-line displacement passes
The outer end face of sensor 1 is limited step.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810425910.2A CN108799374A (en) | 2018-05-07 | 2018-05-07 | A kind of airplane wheel disk type brake wear indicating device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810425910.2A CN108799374A (en) | 2018-05-07 | 2018-05-07 | A kind of airplane wheel disk type brake wear indicating device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN108799374A true CN108799374A (en) | 2018-11-13 |
Family
ID=64091095
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810425910.2A Pending CN108799374A (en) | 2018-05-07 | 2018-05-07 | A kind of airplane wheel disk type brake wear indicating device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN108799374A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110805632A (en) * | 2019-10-28 | 2020-02-18 | 西安航空制动科技有限公司 | Abrasion loss indicating rod for evaluating remaining landing and landing number of airplane brakes and evaluation method |
| CN113669384A (en) * | 2021-10-21 | 2021-11-19 | 中车戚墅堰机车车辆工艺研究所有限公司 | Full-disc multi-disc dry-type adjustable parking brake |
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|---|---|---|---|---|
| US6047793A (en) * | 1996-03-19 | 2000-04-11 | Komatsu Ltd. | Device for detecting abrasion of brake for vehicle |
| CN201296382Y (en) * | 2008-03-14 | 2009-08-26 | 北京北摩高科摩擦材料有限责任公司 | Airplane brake wheel |
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| CN101649877A (en) * | 2009-08-27 | 2010-02-17 | 三一重机有限公司 | Complete-disc brake |
| CN201597753U (en) * | 2009-11-18 | 2010-10-06 | 北京北摩高科摩擦材料有限责任公司 | Brake airplane wheels of airplane |
| CN102767582A (en) * | 2012-07-05 | 2012-11-07 | 成都瑞迪机械实业有限公司 | Manual release type high torque electromagnetic brake |
| DE102012016089B4 (en) * | 2012-08-14 | 2014-11-20 | Sew-Eurodrive Gmbh & Co Kg | Sensor system for determining the wear of an electromagnetically actuated brake and brake with sensor system |
| CN205689641U (en) * | 2016-06-22 | 2016-11-16 | 西安科技大学 | Coal-winning machine multi-disc brake with work state monitoring function |
| CN205860977U (en) * | 2016-06-23 | 2017-01-04 | 无锡市河埒传感器有限公司 | A kind of differential transformer displacement transducer |
| CN106767951A (en) * | 2016-12-26 | 2017-05-31 | 北京曙光航空电气有限责任公司 | A kind of displacement transducer |
| CN107074228A (en) * | 2014-12-16 | 2017-08-18 | 索尤若驱动有限及两合公司 | Brake apparatus that can be Electromagnetically actuated |
| CN208519091U (en) * | 2018-05-07 | 2019-02-19 | 西安航空制动科技有限公司 | A kind of airplane wheel disk type brake wear indicating device |
-
2018
- 2018-05-07 CN CN201810425910.2A patent/CN108799374A/en active Pending
Patent Citations (12)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US6047793A (en) * | 1996-03-19 | 2000-04-11 | Komatsu Ltd. | Device for detecting abrasion of brake for vehicle |
| CN201296382Y (en) * | 2008-03-14 | 2009-08-26 | 北京北摩高科摩擦材料有限责任公司 | Airplane brake wheel |
| CN101532545A (en) * | 2009-04-23 | 2009-09-16 | 山东泰山天盾矿山机械有限公司 | Real-time detection and protection device for brake shoes and disc spring of disc brake |
| CN101649877A (en) * | 2009-08-27 | 2010-02-17 | 三一重机有限公司 | Complete-disc brake |
| CN201597753U (en) * | 2009-11-18 | 2010-10-06 | 北京北摩高科摩擦材料有限责任公司 | Brake airplane wheels of airplane |
| CN102767582A (en) * | 2012-07-05 | 2012-11-07 | 成都瑞迪机械实业有限公司 | Manual release type high torque electromagnetic brake |
| DE102012016089B4 (en) * | 2012-08-14 | 2014-11-20 | Sew-Eurodrive Gmbh & Co Kg | Sensor system for determining the wear of an electromagnetically actuated brake and brake with sensor system |
| CN107074228A (en) * | 2014-12-16 | 2017-08-18 | 索尤若驱动有限及两合公司 | Brake apparatus that can be Electromagnetically actuated |
| CN205689641U (en) * | 2016-06-22 | 2016-11-16 | 西安科技大学 | Coal-winning machine multi-disc brake with work state monitoring function |
| CN205860977U (en) * | 2016-06-23 | 2017-01-04 | 无锡市河埒传感器有限公司 | A kind of differential transformer displacement transducer |
| CN106767951A (en) * | 2016-12-26 | 2017-05-31 | 北京曙光航空电气有限责任公司 | A kind of displacement transducer |
| CN208519091U (en) * | 2018-05-07 | 2019-02-19 | 西安航空制动科技有限公司 | A kind of airplane wheel disk type brake wear indicating device |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110805632A (en) * | 2019-10-28 | 2020-02-18 | 西安航空制动科技有限公司 | Abrasion loss indicating rod for evaluating remaining landing and landing number of airplane brakes and evaluation method |
| CN113669384A (en) * | 2021-10-21 | 2021-11-19 | 中车戚墅堰机车车辆工艺研究所有限公司 | Full-disc multi-disc dry-type adjustable parking brake |
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| PB01 | Publication | ||
| PB01 | Publication | ||
| SE01 | Entry into force of request for substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20181113 |