CN105035331A - Soft trainer engine control system clutch device - Google Patents
Soft trainer engine control system clutch device Download PDFInfo
- Publication number
- CN105035331A CN105035331A CN201510506426.9A CN201510506426A CN105035331A CN 105035331 A CN105035331 A CN 105035331A CN 201510506426 A CN201510506426 A CN 201510506426A CN 105035331 A CN105035331 A CN 105035331A
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- clutch
- arrangement
- clutch device
- soft
- deck
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Abstract
The invention provides a soft trainer engine control system clutch device. One end of a clutch device body is provided with a forecabin connection steel cable for being connected with a forecabin accelerator control table, and the other end of the clutch device body is provided with a rear-cabin connection steel cable for being connected with a rear-cabin accelerator control table. The clutch device body is internally provided with front clutch device pulleys, rear clutch device pulleys and guide pulleys, wherein the front clutch device pulleys and the rear clutch device pulleys are symmetrically arranged. Meanwhile, one side of each front clutch device pulley is provided with a spring for compressing a clutch bolt, and the clutch bolts are inserted into the rear clutch device pulleys. In a normal state, the front clutch device pulleys and the rear clutch device pulleys form a rigid body, and at the moment a forecabin engine accelerator table and a rear-cabin engine accelerator table are in a mechanical linkage state; in case of emergency, pilots in a rear cabin separate the front clutch device pulleys from the rear clutch device pulleys by operating a clutch control interface, the safety coefficient of pilots in the rear cabin is increased effectively, and the soft trainer engine control system clutch device is easy to operate.
Description
Technical field
The present invention relates to aviation machine control technology field, particularly relate to a kind of soft Trainer Engines maneuvering system arrangement of clutch.
Background technology
The engine oil-valve operation system of current schoolaeroplane is mainly divided into rigid control and flexible control two kinds, wherein, the arrangement of clutch of typical rigid connecting rod engine accelerator operating system primarily of arrangement of clutch support, the pull bar connecting rear deck throttle platform, the pull bar connecting front deck throttle platform, arrangement of clutch handle, handle cable wire, the pull bar of connecting engine fuel controller and rear deck throttle platform composition; And in soft engine oil-valve operation system, also do not adopt arrangement of clutch, realize the mechanical linkage between front deck and rear deck and disconnection, when being in an emergency, backseat pilot's front seat man can only be relied on to handle disconnection that rear deck throttle platform realizes front deck and rear deck, if front seat man does not handle rear deck throttle platform, dangerous following for backseat pilot.
Summary of the invention
Technical matters solved by the invention is to provide a kind of soft Trainer Engines maneuvering system arrangement of clutch, to solve the shortcoming in above-mentioned background technology.
Technical matters solved by the invention realizes by the following technical solutions:
A kind of soft Trainer Engines maneuvering system arrangement of clutch, comprises front deck and connects cable wire, rear deck connection cable wire, clutch manipulation interface, arrangement of clutch front wheel, arrangement of clutch back pulley, leading sheave, spring, on-of bolt and arrangement of clutch main body; Wherein, the front deck that arrangement of clutch main body one end is provided with for connecting front deck power control platform connects cable wire, and the rear deck that the other end is provided with for connecting rear deck power control platform connects cable wire; Arrangement of clutch front wheel, arrangement of clutch back pulley, leading sheave is separately installed with in arrangement of clutch main body, and arrangement of clutch front wheel and arrangement of clutch back pulley symmetry are installed, be provided with the spring for compressing on-of bolt in arrangement of clutch front wheel side, on-of bolt inserts in arrangement of clutch back pulley simultaneously; In addition, interface is handled in clutch arrangement of clutch main body is also provided with for connecting rear deck clutch bar handle.
In the present invention, outside arrangement of clutch main body, arrangement of clutch housing is installed.
In the present invention, arrangement of clutch housing is provided with leading sheave.
In the present invention, the leading sheave in arrangement of clutch main body is arranged between two arrangement of clutch front wheels.
In the present invention, clutch manipulation interface is connected with arrangement of clutch main body by clutch cable wire.
In the present invention, clutch manipulation interface is arranged in rear deck.
In the present invention, under normal circumstances, the pressure of spring impels on-of bolt to insert arrangement of clutch back pulley, and arrangement of clutch front wheel and arrangement of clutch back pulley form a rigid body, and now front deck engine throttle platform and rear deck engine throttle platform are mechanical linkage state;
When meeting emergency situation, interface is handled in the clutch that backseat pilot is positioned at rear deck by operation, when backseat pilot's applied force overcome spring pressure and after making on-of bolt move certain stroke laterally, on-of bolt and arrangement of clutch back pulley disconnect, now arrangement of clutch front wheel and arrangement of clutch back pulley disconnect, and namely throw off the mechanical linkage of rear deck and front deck; Effective raising backseat pilot safety factor.
Beneficial effect: in the present invention, front deck power control platform, rear deck power control platform connect cable wire be connected with arrangement of clutch respectively by front deck throttle platform connection cable wire, rear deck throttle platform, rear deck clutch bar handle is handled interface by clutch and is connected with arrangement of clutch, normal condition arrangement of clutch front wheel and arrangement of clutch back pulley form a rigid body, and now front deck engine throttle platform and rear deck engine throttle platform are mechanical linkage state; When meeting emergency situation, backseat pilot handles interface by operation clutch and arrangement of clutch front wheel and arrangement of clutch back pulley is disconnected, and effectively improves backseat pilot's safety factor, and simple to operate.
Accompanying drawing explanation
Fig. 1 is the structural representation of preferred embodiment of the present invention.
Fig. 2 is the operation schematic diagram of preferred embodiment of the present invention.
Detailed description of the invention
The technological means realized to make the present invention, creation characteristic, reaching object and effect is easy to understand, below in conjunction with concrete diagram, setting forth the present invention further.
One see Fig. 1 ~ Fig. 2 soft Trainer Engines maneuvering system arrangement of clutch, comprises front deck and connects cable wire 1, rear deck connection cable wire 2, clutch manipulation interface 3, arrangement of clutch front wheel 4, arrangement of clutch back pulley 5, arrangement of clutch housing 6, leading sheave 7, spring 8, clutch cable wire 9, on-of bolt 10 and arrangement of clutch main body; Wherein, be provided with arrangement of clutch housing 6 outside arrangement of clutch main body, and the front deck be provided with in arrangement of clutch main body one end for connecting front deck power control platform connects cable wire 1, the rear deck that the other end is provided with for connecting rear deck power control platform connects cable wire 2; Arrangement of clutch front wheel 4, arrangement of clutch back pulley 5, leading sheave 7 is separately installed with in arrangement of clutch main body, and leading sheave 7 is arranged between two arrangement of clutch front wheels 4, arrangement of clutch front wheel 4 is installed with arrangement of clutch back pulley 5 symmetry, be provided with the spring 8 for compressing on-of bolt 10 in arrangement of clutch front wheel 4 side, on-of bolt 10 inserts in arrangement of clutch back pulley 5 simultaneously; In addition, interface 3 is handled in clutch arrangement of clutch main body is also provided with for connecting rear deck clutch bar handle, and clutch is handled interface 3 and is connected with arrangement of clutch main body by clutch cable wire 9.
In the present embodiment, arrangement of clutch housing 6 is provided with leading sheave 7.
In the present embodiment, under normal circumstances, the pressure of spring 8 impels on-of bolt 10 to insert arrangement of clutch back pulley 5, arrangement of clutch front wheel 4 and arrangement of clutch back pulley 5 form a rigid body, now front deck engine throttle platform and rear deck engine throttle platform are mechanical linkage state, i.e. T state in Fig. 2;
When meeting emergency situation, interface 3 is handled in the clutch that backseat pilot is positioned at rear deck by operation, when backseat pilot's applied force overcome spring 5 pressure and after making on-of bolt 10 move certain stroke laterally, i.e. S state in Fig. 2, on-of bolt 10 and arrangement of clutch back pulley 5 disconnect, now arrangement of clutch front wheel 4 and arrangement of clutch back pulley 5 disconnect, and namely throw off the mechanical linkage of rear deck and front deck; Effective raising backseat pilot safety factor.
More than show and describe groundwork of the present invention and principal character and advantage of the present invention.The technical personnel of the industry should be understood; the present invention is not restricted to the described embodiments; what describe in above-described embodiment and specification sheets just illustrates principle of the present invention; without departing from the spirit and scope of the present invention; the present invention also has various changes and modifications, and these changes and improvements all fall in the claimed scope of the invention.Application claims protection domain is defined by appending claims and equivalent thereof.
Claims (7)
1. a soft Trainer Engines maneuvering system arrangement of clutch, comprises front deck and connects cable wire, rear deck connection cable wire, clutch manipulation interface, arrangement of clutch front wheel, arrangement of clutch back pulley, leading sheave, spring, on-of bolt and arrangement of clutch main body; It is characterized in that, the front deck that arrangement of clutch main body one end is provided with for connecting front deck power control platform connects cable wire, and the rear deck that the other end is provided with for connecting rear deck power control platform connects cable wire; Arrangement of clutch front wheel, arrangement of clutch back pulley, leading sheave is separately installed with in arrangement of clutch main body, and arrangement of clutch front wheel and arrangement of clutch back pulley symmetry are installed, be provided with the spring for compressing on-of bolt in arrangement of clutch front wheel side, on-of bolt inserts in arrangement of clutch back pulley simultaneously; In addition, interface is handled in clutch arrangement of clutch main body is also provided with for connecting rear deck clutch bar handle.
2. one according to claim 1 soft Trainer Engines maneuvering system arrangement of clutch, is characterized in that, is provided with arrangement of clutch housing outside arrangement of clutch main body.
3. one according to claim 2 soft Trainer Engines maneuvering system arrangement of clutch, is characterized in that, arrangement of clutch housing is provided with leading sheave.
4. one according to claim 1 soft Trainer Engines maneuvering system arrangement of clutch, is characterized in that, the leading sheave in arrangement of clutch main body is arranged between two arrangement of clutch front wheels.
5. one according to claim 1 soft Trainer Engines maneuvering system arrangement of clutch, is characterized in that, clutch is handled interface and is connected with arrangement of clutch main body by clutch cable wire.
6. one according to claim 1 soft Trainer Engines maneuvering system arrangement of clutch, is characterized in that, clutch is handled interface and is arranged in rear deck.
7. one according to claims 1 to 6 soft Trainer Engines maneuvering system arrangement of clutch, it is characterized in that, under normal circumstances, the pressure of spring impels on-of bolt to insert arrangement of clutch back pulley, arrangement of clutch front wheel and arrangement of clutch back pulley form a rigid body, and now front deck engine throttle platform and rear deck engine throttle platform are mechanical linkage state; When meeting emergency situation, interface is handled in the clutch that backseat pilot is positioned at rear deck by operation, when backseat pilot's applied force overcome spring pressure and after making on-of bolt move certain stroke laterally, on-of bolt and arrangement of clutch back pulley disconnect, now arrangement of clutch front wheel and arrangement of clutch back pulley disconnect, and namely throw off the mechanical linkage of rear deck and front deck.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510506426.9A CN105035331B (en) | 2015-08-18 | 2015-08-18 | Soft trainer engine control system clutch device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510506426.9A CN105035331B (en) | 2015-08-18 | 2015-08-18 | Soft trainer engine control system clutch device |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105035331A true CN105035331A (en) | 2015-11-11 |
| CN105035331B CN105035331B (en) | 2017-04-26 |
Family
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510506426.9A Active CN105035331B (en) | 2015-08-18 | 2015-08-18 | Soft trainer engine control system clutch device |
Country Status (1)
| Country | Link |
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| CN (1) | CN105035331B (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105366061A (en) * | 2015-11-17 | 2016-03-02 | 江西洪都航空工业集团有限责任公司 | Electronically-controlled stopping device for rear cabin control engine throttle |
| CN109533354A (en) * | 2018-12-07 | 2019-03-29 | 贵州华阳电工有限公司 | Two position clutch friction damping units |
| CN110758750A (en) * | 2019-11-25 | 2020-02-07 | 华中科技大学 | Transmission mechanism for manual and automatic switching of airplane accelerator |
| CN111762335A (en) * | 2020-07-06 | 2020-10-13 | 中国人民解放军空军军医大学 | Pilot control system mounting fixture |
| CN116153167A (en) * | 2023-04-10 | 2023-05-23 | 北京天翼创展航空科技有限公司 | Flight simulator accelerator table follow-up device |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0657350B1 (en) * | 1993-12-13 | 1997-07-23 | Sextant Avionique | Manual throttle control device for operating both enzymes of an aircraft |
| EP1588942A1 (en) * | 2004-04-21 | 2005-10-26 | AIRBUS France | Throttle lever for controlling the operation of at least one engine of an aircraft |
| CN202863773U (en) * | 2012-08-12 | 2013-04-10 | 肖志军 | Control device of overwater air vehicle |
| CN103115081A (en) * | 2013-03-07 | 2013-05-22 | 宁波市海誉机电科技有限公司 | Tubular motor outer-opening clutch |
| CN103407920A (en) * | 2013-08-22 | 2013-11-27 | 中国地质装备总公司 | Intelligent deep hole rope winch driven by variable frequency motor |
| CN103507964A (en) * | 2012-06-16 | 2014-01-15 | 姜汝诚 | Aircraft catapult-assisted take-off device and aircraft landing stopping device |
| CN103640703A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Clutch device for link type engine throttle control system |
| CN203486133U (en) * | 2013-09-17 | 2014-03-19 | 无锡振华机械有限公司 | Aircraft operating mechanism |
-
2015
- 2015-08-18 CN CN201510506426.9A patent/CN105035331B/en active Active
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| EP0657350B1 (en) * | 1993-12-13 | 1997-07-23 | Sextant Avionique | Manual throttle control device for operating both enzymes of an aircraft |
| EP1588942A1 (en) * | 2004-04-21 | 2005-10-26 | AIRBUS France | Throttle lever for controlling the operation of at least one engine of an aircraft |
| CN103507964A (en) * | 2012-06-16 | 2014-01-15 | 姜汝诚 | Aircraft catapult-assisted take-off device and aircraft landing stopping device |
| CN202863773U (en) * | 2012-08-12 | 2013-04-10 | 肖志军 | Control device of overwater air vehicle |
| CN103115081A (en) * | 2013-03-07 | 2013-05-22 | 宁波市海誉机电科技有限公司 | Tubular motor outer-opening clutch |
| CN103407920A (en) * | 2013-08-22 | 2013-11-27 | 中国地质装备总公司 | Intelligent deep hole rope winch driven by variable frequency motor |
| CN203486133U (en) * | 2013-09-17 | 2014-03-19 | 无锡振华机械有限公司 | Aircraft operating mechanism |
| CN103640703A (en) * | 2013-11-28 | 2014-03-19 | 江西洪都航空工业集团有限责任公司 | Clutch device for link type engine throttle control system |
Cited By (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105366061A (en) * | 2015-11-17 | 2016-03-02 | 江西洪都航空工业集团有限责任公司 | Electronically-controlled stopping device for rear cabin control engine throttle |
| CN109533354A (en) * | 2018-12-07 | 2019-03-29 | 贵州华阳电工有限公司 | Two position clutch friction damping units |
| CN109533354B (en) * | 2018-12-07 | 2022-01-25 | 贵州华阳电工有限公司 | Two-position clutch friction damping device |
| CN110758750A (en) * | 2019-11-25 | 2020-02-07 | 华中科技大学 | Transmission mechanism for manual and automatic switching of airplane accelerator |
| CN111762335A (en) * | 2020-07-06 | 2020-10-13 | 中国人民解放军空军军医大学 | Pilot control system mounting fixture |
| CN116153167A (en) * | 2023-04-10 | 2023-05-23 | 北京天翼创展航空科技有限公司 | Flight simulator accelerator table follow-up device |
| CN116153167B (en) * | 2023-04-10 | 2023-08-22 | 北京天翼创展航空科技有限公司 | Flight simulator accelerator table follow-up device |
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| Publication number | Publication date |
|---|---|
| CN105035331B (en) | 2017-04-26 |
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