CN202189480U - General simulation pedal - Google Patents

General simulation pedal Download PDF

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Publication number
CN202189480U
CN202189480U CN2011202719266U CN201120271926U CN202189480U CN 202189480 U CN202189480 U CN 202189480U CN 2011202719266 U CN2011202719266 U CN 2011202719266U CN 201120271926 U CN201120271926 U CN 201120271926U CN 202189480 U CN202189480 U CN 202189480U
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CN
China
Prior art keywords
pedal
service brake
fixed
rocking arm
rotating shaft
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Expired - Fee Related
Application number
CN2011202719266U
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Chinese (zh)
Inventor
张帆
曹靖
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Beijing Bluesky Aviation Technology Co Ltd
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Beijing Bluesky Aviation Technology Co Ltd
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Priority to CN2011202719266U priority Critical patent/CN202189480U/en
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Publication of CN202189480U publication Critical patent/CN202189480U/en
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Abstract

The utility model provides a general simulation pedal, comprising symmetrically installed pedal plates, rudder channels and foot brake channels, wherein the pedal plates are replaceable; the simulation pedal also comprises symmetrically installed rotation rocking arms on which the pedal plates are installed; a mounting base which is a base of the simulation pedal and can be used for external installation; and a gear mechanism housing, a bearing support, symmetrically installed rocking arm rotating shafts, symmetrically installed fixed arms and an angular displacement sensor. The gear mechanism housing and the bearing support are respectively fixed on the mounting base; one ends of the fixed arms are in connection with the bearing support through the rocking arm rotating shafts, and the other ends are in connection with a foot brake force loading mechanism through a connecting joint. The general simulation pedal employs a modularization structure design, has a high integrated level and is convenient and fast to install; the transmission gap is small, and the linkage effect is good; thus the general simulation pedal has wide actual use value on flight simulators.

Description

The common simulation pedal
Technical field
The utility model relates to the aviation flight emulation technology, especially relates to aviation flight simulator emulation pedal, is mainly used in the pedal simulation component on the aviation flight simulator, but the while expanded application is in the simulation of relevant artificial product pedal.
Background technology
Actual aboard pedal is the complicated linkage assembly of a cover, rotate the rocking arm bottom through many connecting rods respectively with spring strut, position transducer, the middle part of rotating rocking arm has installation accessories such as pull bar and interlock rocking arm to be connected, realization left-right rotation rocking arm links.These parts reference for installation are not quite similar; But must satisfy service condition; All must install such as the neutral angle of pedal, connecting rod gap, train of mechanism friction force, restoring force, sensor reliable operation condition etc. and to adjust to the right place; Thereby traditional emulation pedal scheme, assembly precision is high, and the difficulty of debugging work is very big.
In aviation emulation industry, the emulation solution of pedal is normally directly adopted the control system of aircraft.But also brought some problems, such as:
1) interlock of aircraft pedal is complicated, is difficult for debugging and installs;
2) simulator needs to be unfavorable for the modular design of flight simulator according to the aircaft configuration platform design;
3) can only be directed against specific model, not possess versatility;
4) system's power supply, signals collecting etc. must increase workload in order to dock with simulation system and to reequip;
5) the Design and Machining expense is high.
Summary of the invention
The purpose of the utility model is not enough to provide a kind of common simulation pedal what overcome prior art, and this emulation pedal adopts modular construction design, and integrated level is high; The response of pedal Displacement Feedback is rapid, and precision is high; The steering force sense is good, and handling quality is outstanding; Highly versatile is applicable to the emulation of various aircraft pedal.
In order to realize the purpose of the utility model, a kind of common simulation pedal of special proposition is made up of pedal, yaw rudder passage and service brake passage that symmetry is installed, and said pedal is removable pedal, and this emulation pedal also comprises:
The rotation rocking arm that symmetry is installed, said pedal are installed in and rotate on the rocking arm;
Mounting seat is the base of said emulation pedal, can externally install through it;
The gear mechanism outer cover, bearing spider, the rocker shaft that symmetry is installed; The fixed arm that symmetry is installed, angular displacement sensor, the flange surface of said angular displacement sensor is installed on the bearing spider; The turning axle of angular displacement sensor is installed on the gear; Said gear mechanism outer cover, bearing spider are fixedly mounted on respectively on the mounting seat, and fixed arm one end is connected with bearing spider through rocker shaft, and the other end is connected with service brake power load maintainer through jointing;
The gear drive of one cover yaw rudder passage, two ends are connected with bearing spider through rotating shaft respectively;
The pedal of one cover yaw rudder passage returns medi-spring power load maintainer, and the extension spring of being installed by symmetry constitutes with the symmetrical spring force load maintainer fixed arm of installing, and is fixed in the rotating shaft of said gear drive;
The service brake power load maintainer of two cover service brake passages, an end is fixed on the said pedal, and an end is fixed on the fixed arm, forms a parallelogram with said pedal, rotation rocking arm, fixed arm, thereby produces the restoring force of service brake direction.
The rotating shaft of said pedal and pedal are fixed together to be installed in and rotate on the rocking arm.
Its junction of said pedal is quick detaching structure, and quick-release pin is arranged in the said pedal rotating shaft, through said pin to the fast quick-detach of pedal.
Said gear drive is made up of pinion wheel, gear wheel, rotating shaft, bearing and the bearing spider that is installed on the base, changes the rotation direction of rotating rocking arm through rotating shaft rotation driving pinion, gear wheel.
The service brake power load maintainer that symmetry is installed is made up of compression spring, compression push rod, clamp ring, sleeve, jointing and displacement transducer, compression spring and displacement transducer, and it is connected with the compression push rod through sleeve.
The wiring of said emulation pedal is all inner at the gear mechanism outer cover with wiring, and said wiring is externally exported through the air plug that is installed on the gear mechanism outer cover with wiring.
The beneficial effect of the utility model is following:
Employing modular construction design, integral installation is convenient and swift, for the modular design of flight simulator provides very big facility;
Integrated level is high, has realized in small space, spring force being simulated, and the height in position feedback loop is integrated;
Adopt high-quality linear potentiometer as the position feedback element, the response of pedal Displacement Feedback is rapid, and precision is high;
The steering force sense is good, and handling quality is outstanding, adopts special spring force load maintainer that restoring force is provided, and steering force is adjustable, is convenient to the simulation to various aircraft models.
Highly versatile is applicable to the emulation of various aircraft pedal, and the pedal pedal is detachable, and it is convenient to change, and the pedal of different aircraft models can be installed, and is applicable to the simulation to various aircraft models;
The outward appearance fidelity is high, pedal part (pilot's visible part) and certain type aircraft pedal profile basically identical, with general aircraft pedal profile roughly the same, great to the common simulation design sense that solves pedal, wide practical value is arranged on flight simulator.
Description of drawings
Fig. 1 is the utility model common simulation pedal one-piece construction synoptic diagram;
Fig. 2 is a service brake power load maintainer synoptic diagram;
Fig. 3 is that pedal returns medi-spring power load maintainer synoptic diagram;
Fig. 4 is the gear drive synoptic diagram.
Among the figure:
1 pedal, 9 fixed arms
2 rotate rocking arm 10 service brake power load maintainers
3 angular displacement sensors, 101 compression push rods
102 clamp rings of 4 gear drives
41 pinion wheels, 103 displacement transducers
42 rotating shafts, 104 compression springs
43 gear wheels, 105 sleeves
44 bearings, 106 jointings
5 gear drive outer covers, 11 pedals return medi-spring power load maintainer
6 mounting seat, 111 extension springs
7 bearing spiders, 112 spring force load maintainer fixed arms
The 12 pedal rotating shafts of 8 rocker shafts
Embodiment
For making the object of the invention, technical scheme and advantage clearer, below in conjunction with specific embodiment and conjunction with figs., to further explain of the present invention.
Fig. 1 is the utility model common simulation pedal one-piece construction synoptic diagram; As shown in the figure, this emulation pedal has adopted modular design, and overall appearance is succinct, and is easy for installation.
A kind of common simulation pedal of the utility model is made up of pedal 1, yaw rudder passage and service brake passage that symmetry is installed, and said pedal 1 is removable pedal, and this emulation pedal also comprises:
The rotation rocking arm 2 that symmetry is installed, said pedal 1 are installed in and rotate on the rocking arm 2;
Mounting seat 6 is the base of said emulation pedal, can externally install through it;
Gear mechanism outer cover 5, bearing spider 7, the rocker shaft 8 that symmetry is installed; The fixed arm 9 that symmetry is installed, angular displacement sensor 3, the flange surface of said angular displacement sensor 3 are installed on the bearing spider 7; The turning axle of angular displacement sensor 3 is installed on the gear 41; Said gear mechanism outer cover 5, bearing spider 7 are fixedly mounted on respectively on the mounting seat 6, and fixed arm 9 one ends are connected with bearing spider 7 through rocker shaft 8, and the other end passes through jointing 106 and is connected with service brake power load maintainer 10;
The utility model pedal returns service brake power load maintainer 10, gear drive 4, pedal all parts such as medi-spring load maintainer 11, position feedback element, angular displacement sensor 3 and all is integrated on the mounting seat 6, becomes as a whole pedal module.Mounting hole and simulator platform through base 6 are installed, and be simple and convenient, need not debug.
Pedal 1 be generally independent Design and Machining with the identical parts of the true pedal of aircraft model that will simulate.Its junction is designed to quick detaching structure, can change pedal 1 easily, only need the taper pin in the pedal rotating shaft 12 be tightened when needing to install to get final product; During dismounting take out taper pin, withdraw from getting final product vertically.
Fig. 2 is a service brake power load maintainer structural representation; As shown in the figure; Service brake power load maintainer 10 mainly is made up of compression spring 104, compression push rod 101, clamp ring 102, sleeve 105, jointing 106 and displacement transducer 103, and in service brake power load maintainer 10, service brake power load maintainer 10 1 ends are fixed on the pedal 1; One end is fixed on the fixed arm 9, makes service brake power load maintainer 10, pedal 1, rotation rocking arm 2 and fixed arm 9 form a parallelogram.When pedal 1 when pedal rotating shaft 12 is rotated, the constrictor 101 in the service brake power load maintainer 10 promotes compression springs 104 and does linear slide with displacement transducer 103 along sleeve 105, has realized the power sense of service brake and the transmission of displacement signal.
Fig. 3 is that pedal returns medi-spring power load maintainer structural representation; As shown in the figure; Pedal returns medi-spring power load maintainer 11 and is made up of two extension springs 111 and two fixed arms 112, and spring force load maintainer fixed arm 112 is fixed in the rotating shaft 42 of gear drive 4.Rotate towards a certain direction when gear 41 drives rotating shaft 42, the fixed arm 112 that is fixed in the rotating shaft 42 rotates along same direction, drives one of them extension spring 111 simultaneously, and extension spring 111 produces Hui Zhongli under making.
Fig. 4 is the gear drive synoptic diagram, and is as shown in the figure, and gear drive 4 is made up of pinion wheel 41, rotating shaft 42, gear wheel 43, bearing 44 and the bearing spider 7 that is installed on the base.When one of them rotates one of them gears rotation of rocking arm 2 drives, through said gear drive 4, make another one rotate rocking arm 2, thereby realized the function of pedal along opposite direction rotation.
Major function:
Realize the output function of pedal position loop signal through integrated angular displacement sensor; Through integrated service brake power load maintainer, realize the simulation of service brake power and the collection and the output of displacement signal; Through gear drive, realize the function of pedal and the simulation of power.
Main performance index
Figure BDA0000079457390000051
The key technical indexes
Angular displacement sensor precision :≤± 0.1%
Displacement transducer :≤± 0.2%
Yaw rudder passage mechanical clearance :≤0.5 °
Service brake passage mechanical clearance :≤0.2 °
The reliable manipulation life-span: ≮ 10000 total travels
Working environment: indoor
Though the utility model with preferred embodiment openly as above, they are not to be used for limiting the utility model, and the content that the protection domain of the utility model should be defined with the application's claim protection domain is as the criterion.Anyly have the knack of present technique field person, in spirit that does not break away from the utility model and scope, various variations of being done or be equal to replacement all should belong to the protection domain of the utility model.

Claims (6)

1. a common simulation pedal is made up of pedal (1), yaw rudder passage and service brake passage that symmetry is installed, it is characterized in that said pedal (1) is removable pedal, and this emulation pedal also comprises:
The rotation rocking arm (2) that symmetry is installed, said pedal (1) are installed in and rotate on the rocking arm (2);
Mounting seat (6) is the base of said emulation pedal, can externally install through it;
Gear mechanism outer cover (5); Bearing spider (7), the rocker shaft (8) that symmetry is installed, the fixed arm (9) that symmetry is installed; Angular displacement sensor (3); The flange surface of said angular displacement sensor (3) is installed on the bearing spider (7), and the turning axle of angular displacement sensor (3) is installed on the gear (41), and said gear mechanism outer cover (5), bearing spider (7) are fixedly mounted on respectively on the mounting seat (6); Fixed arm (9) one ends are connected with bearing spider (7) through rocker shaft (8), and the other end is connected with service brake power load maintainer (10) through jointing (106);
The gear drive (4) of one cover yaw rudder passage, two ends are connected with bearing spider (7) through rotating shaft (42) respectively;
The pedal of one cover yaw rudder passage returns medi-spring power load maintainer (11), and extension spring (111) and the symmetrical spring force load maintainer fixed arm of installing (112) installed by symmetry constitute, and are fixed in the rotating shaft (42) of said gear drive (4);
The service brake power load maintainer (10) of the service brake passage that two cover symmetries are installed; One end is fixed on the said pedal (1); One end is fixed on the fixed arm (9); Form a parallelogram with said pedal (1), rotation rocking arm (2), fixed arm (9), thereby produce the restoring force of service brake direction.
2. common simulation pedal according to claim 1 is characterized in that: the rotating shaft (12) of said pedal (1) is fixed together to be installed in pedal (1) and rotates on the rocking arm (2).
3. common simulation pedal according to claim 1 is characterized in that: its junction of said pedal (1) is quick detaching structure, and quick-release pin is arranged in the said pedal rotating shaft (12), through said pin to the fast quick-detach of pedal (1).
4. common simulation pedal according to claim 1; It is characterized in that: said gear drive (4) is made up of pinion wheel (41), gear wheel (43), rotating shaft (42), bearing (44) and the bearing spider (7) that is installed on the base, changes the rotation direction of rotating rocking arm (2) through rotating shaft (42) rotation driving pinion (41), gear wheel (43).
5. common simulation pedal according to claim 1; It is characterized in that: the service brake power load maintainer (10) that affiliated two cover symmetries are installed is made up of compression spring (104), compression push rod (101), clamp ring (102), sleeve (105), jointing (106) and displacement transducer (103); Compression spring (104) and displacement transducer (103), it is connected with compression push rod (101) through sleeve (105).
6. according to claim 1,2,3,4 or 5 described common simulation pedals; It is characterized in that: the wiring of said emulation pedal and wiring are all in gear mechanism outer cover (5) inside, and said wiring is externally exported through the air plug that is installed on the gear mechanism outer cover (5) with wiring.
CN2011202719266U 2011-07-28 2011-07-28 General simulation pedal Expired - Fee Related CN202189480U (en)

Priority Applications (1)

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Cited By (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103057697A (en) * 2013-01-07 2013-04-24 中国商用飞机有限责任公司 Rudder pedal control apparatus for airplane, and control method thereof
RU173918U1 (en) * 2016-12-09 2017-09-19 Акционерное Общество "ТЕХНОФИНАНСТРЕЙД" MECHANISM OF PEDALS OF THE AIRCRAFT SIMULATOR
CN107507485A (en) * 2017-08-09 2017-12-22 上海工程技术大学 A kind of flight simulator and the gearing of A seating riding manipulation and loading device
CN108109473A (en) * 2018-02-02 2018-06-01 安徽英釜航空科技有限公司 A kind of flight simulator foot rudder linkage
CN108597296A (en) * 2018-06-05 2018-09-28 珠海高斯科技有限公司 The pedal manipulation device of flight simulator
CN110510106A (en) * 2018-05-22 2019-11-29 空中客车运营简化股份公司 Entirety and removable pedal module for aircraft pedals
CN110510107A (en) * 2018-05-22 2019-11-29 空中客车运营简化股份公司 The pedals for aircraft with single-piece and detachable main module
CN111429777A (en) * 2020-04-26 2020-07-17 奥瑞思智能科技(阜新)有限公司 Flight simulation cabin
CN112201114A (en) * 2020-10-12 2021-01-08 浙江大学 Big aircraft pedal analogue means based on rack and pinion motion
CN112793764A (en) * 2021-03-19 2021-05-14 昆山航理机载设备股份有限公司 Linkage mechanism for airplane pedal
CN113700812A (en) * 2021-08-25 2021-11-26 芜湖东旭光电装备技术有限公司 Synchronous rotation centering device
CN114141096A (en) * 2021-11-26 2022-03-04 昌河飞机工业(集团)有限责任公司 Helicopter simulator pedal brake simulation device

Cited By (17)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN103057697A (en) * 2013-01-07 2013-04-24 中国商用飞机有限责任公司 Rudder pedal control apparatus for airplane, and control method thereof
WO2014106428A1 (en) * 2013-01-07 2014-07-10 中国商用飞机有限责任公司 Rudder pedal control device and control method for airplane
CN103057697B (en) * 2013-01-07 2015-05-13 中国商用飞机有限责任公司 Rudder pedal control apparatus for airplane, and control method thereof
RU173918U1 (en) * 2016-12-09 2017-09-19 Акционерное Общество "ТЕХНОФИНАНСТРЕЙД" MECHANISM OF PEDALS OF THE AIRCRAFT SIMULATOR
CN107507485A (en) * 2017-08-09 2017-12-22 上海工程技术大学 A kind of flight simulator and the gearing of A seating riding manipulation and loading device
CN107507485B (en) * 2017-08-09 2019-08-30 上海工程技术大学 A kind of flight simulator and A seating riding manipulation interlocks and loading device
CN108109473A (en) * 2018-02-02 2018-06-01 安徽英釜航空科技有限公司 A kind of flight simulator foot rudder linkage
CN108109473B (en) * 2018-02-02 2024-06-04 安徽英釜航空科技有限公司 Foot rudder linkage device of flight simulator
CN110510106A (en) * 2018-05-22 2019-11-29 空中客车运营简化股份公司 Entirety and removable pedal module for aircraft pedals
CN110510107A (en) * 2018-05-22 2019-11-29 空中客车运营简化股份公司 The pedals for aircraft with single-piece and detachable main module
CN108597296B (en) * 2018-06-05 2024-04-05 珠海高斯科技有限公司 Pedal operating device of flight simulator
CN108597296A (en) * 2018-06-05 2018-09-28 珠海高斯科技有限公司 The pedal manipulation device of flight simulator
CN111429777A (en) * 2020-04-26 2020-07-17 奥瑞思智能科技(阜新)有限公司 Flight simulation cabin
CN112201114A (en) * 2020-10-12 2021-01-08 浙江大学 Big aircraft pedal analogue means based on rack and pinion motion
CN112793764A (en) * 2021-03-19 2021-05-14 昆山航理机载设备股份有限公司 Linkage mechanism for airplane pedal
CN113700812A (en) * 2021-08-25 2021-11-26 芜湖东旭光电装备技术有限公司 Synchronous rotation centering device
CN114141096A (en) * 2021-11-26 2022-03-04 昌河飞机工业(集团)有限责任公司 Helicopter simulator pedal brake simulation device

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GR01 Patent grant
CF01 Termination of patent right due to non-payment of annual fee
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20120411

Termination date: 20160728