CN114743430B - Pedal mechanism capable of simulating position of aircraft - Google Patents

Pedal mechanism capable of simulating position of aircraft Download PDF

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Publication number
CN114743430B
CN114743430B CN202210252745.1A CN202210252745A CN114743430B CN 114743430 B CN114743430 B CN 114743430B CN 202210252745 A CN202210252745 A CN 202210252745A CN 114743430 B CN114743430 B CN 114743430B
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spring
rudder
pedal
sliding block
bracket
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CN114743430A (en
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吕洪亮
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Harbin Laite Brothers Technology Development Co ltd
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Harbin Laite Brothers Technology Development Co ltd
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    • G—PHYSICS
    • G09—EDUCATION; CRYPTOGRAPHY; DISPLAY; ADVERTISING; SEALS
    • G09B—EDUCATIONAL OR DEMONSTRATION APPLIANCES; APPLIANCES FOR TEACHING, OR COMMUNICATING WITH, THE BLIND, DEAF OR MUTE; MODELS; PLANETARIA; GLOBES; MAPS; DIAGRAMS
    • G09B9/00—Simulators for teaching or training purposes
    • G09B9/02—Simulators for teaching or training purposes for teaching control of vehicles or other craft
    • G09B9/08—Simulators for teaching or training purposes for teaching control of vehicles or other craft for teaching control of aircraft, e.g. Link trainer
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction

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  • Engineering & Computer Science (AREA)
  • Theoretical Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Business, Economics & Management (AREA)
  • Physics & Mathematics (AREA)
  • Educational Administration (AREA)
  • Educational Technology (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Control Devices (AREA)

Abstract

The invention discloses a pedal mechanism with adjustable pedal position for an analog aircraft, which solves the problem that a pedal operating mechanism for the analog aircraft in the prior art is not adjustable, and further provides the pedal mechanism with adjustable pedal position for the analog aircraft, through which the front and rear positions of pedals can be adjusted to meet the needs of pilots with different heights. The invention realizes the compatibility of the combination of the brake function, the rudder function and the pedal position adjustable function of the pedal mechanism, and the mechanisms run smoothly without interference, and the control process meets the requirement of simulated flight training. In addition, each part structure connected form is simple, simple to operate and easy maintenance, can reduce training use cost.

Description

Pedal mechanism capable of simulating position of aircraft
Technical Field
The invention relates to a pedal mechanism with adjustable simulated aircraft position, and belongs to the technical field of simulated aircraft equipment.
Background
Simulated aircraft is a specialized device for pilot training, where the foot pedal mechanism is a key subsystem in the simulated aircraft maneuvering system whose performance directly affects the level of flight training. With the development of domestic aviation industry, the demand level of the flight simulator is gradually increased, and the demand for developing a high-standard pedal operating mechanism is urgent. At present, the pedal operating mechanism, particularly the composite mechanism with adjustable position, can meet the requirements of pilots with different heights in China, has less analysis and design, and the pedal mechanism comprises a braking function and a rudder function, can realize front and back adjustment of pedal positions, and can meet the requirements of pilots with different heights.
Disclosure of Invention
The invention aims to solve the problem that a pedal operating mechanism of a simulated aircraft in the prior art is not adjustable, and further provides a pedal mechanism with adjustable simulated aircraft position, through which the front and back positions of pedals can be adjusted, so that the requirements of pilots with different heights can be met.
The invention provides an adjustable pedal mechanism for simulating the position of an aircraft, which comprises a left pedal system, a right pedal system, a head swing rod rotating shaft, a head swing rod, a position adjusting pin, a brake cable spring, a brake cable pulling plate, a head sliding block, two vertical pins, two return springs, a left sliding block with a rudder pin, a rudder differential limiting plate, a rudder spring I, a rudder spring lower bracket, a right sliding block with a rudder pin, a rudder spring II and a rudder spring upper bracket; the brake line pulling plate is connected with the position adjusting pin through a brake line, the position adjusting pin slides in a cylindrical hole of the head slider, a brake line spring is arranged between the brake line and the position adjusting pin, a head swing rod rotating shaft vertically penetrates through the head swing rod, the head swing rod rotating shaft is connected with a front panel of the bracket, a plurality of round holes longitudinally arranged are formed in the front side of the upper part of the head swing rod, the position adjusting pin penetrates through a through hole of the head slider to be matched with the round holes of the head swing rod for position adjustment, two vertical pins penetrate through two sides of the head slider, a return spring is sleeved on the outer side of the vertical pins and is located above the head slider, a left pedal system is connected to the left side of the head slider, and a right pedal system is connected to the right side of the head slider; the left pedal system comprises a left pedal, a left slider, a left pedal rotating shaft, a left slider guide rail, a left brake spring, a left spring bracket guide shaft, a left spring bracket, a left connecting rod mechanism and a left screw rod; the left pedal is rotationally connected with a left sliding block through a left pedal rotating shaft, the left sliding block horizontally moves along a left sliding block guide rail, one end of a left brake spring is connected with the left sliding block, the other end of the left brake spring is connected with a left spring support, the left pedal is connected with the left spring support, a long slot hole is formed in the left spring support, a left spring support guide shaft is fixed on the left sliding block and is matched with the long slot hole, one end of a left connecting rod mechanism is rotationally connected with the left sliding block, the other end of the left connecting rod mechanism is rotationally connected with a left screw rod, a right pedal system is in mirror symmetry and the same structure with the left pedal system, the left pedal system is connected with a head sliding block through a left screw rod, and the right pedal system is connected with the head sliding block through a right screw rod; the upper support of the rudder spring is fixed on the upper portion of the left slider, the lower support of the rudder spring is fixed on the lower portion of the right slider, the lower end of the first rudder spring is connected with one end of the lower support of the rudder spring in the horizontal direction, the other end of the first rudder spring is connected with the upper support of the rudder spring, the lower end of the second rudder spring is connected with the other end of the lower support of the rudder spring in the horizontal direction, the other end of the second rudder spring is connected with the upper support of the rudder spring, the left slider belt rudder pin is vertically fixed on the upper support of the rudder spring, the right slider belt rudder pin is vertically fixed on the lower support of the rudder spring, the upper long slot hole of the differential limiting plate of the rudder penetrates through the left slider belt rudder pin, and the lower long slot hole of the differential limiting plate of the rudder penetrates through the right slider belt rudder pin.
Preferably, the left link mechanism comprises a left link, a left U-shaped link and a left U-shaped link rotating shaft, one end of the left link is connected with the left slider, the other end of the left link is connected with the left U-shaped link, the left U-shaped link rotating shaft is fixed on the support, the left U-shaped link rotates around the left U-shaped link rotating shaft, and the left U-shaped link is rotationally connected with the left screw through a U-shaped link and a left screw connecting shaft.
The pedal mechanism capable of simulating the position of the aircraft has the beneficial effects that: the invention provides a new design idea of a pedal mechanism with adjustable position, realizes the compatibility of the combination of the brake function, the rudder function and the pedal position adjustable function of the pedal mechanism, ensures smooth and interference-free operation among the mechanisms, and meets the requirement of simulated flight training in the control process. In addition, each part structure connected form is simple, simple to operate and easy maintenance, can reduce training use cost.
Drawings
FIG. 1 is a front view of a simulated aircraft position adjustable foot pedal mechanism according to the present invention;
the pedal mechanism shown in fig. 1 is arranged in the cabin of the simulated aircraft, the direction of the aircraft nose of the simulated aircraft is the front direction, the pedal mechanism consists of a left pedal mechanism and a right pedal mechanism, the front view of fig. 1 shows the left pedal mechanism, the left pedal mechanism and the right pedal mechanism realize the differential motion of the left pedal and the right pedal when the rudder is stepped through a connecting rod of the pedal head, a head swing rod and a rudder spring mechanism, and the right pedal mechanism and the left pedal mechanism are completely similar and are not repeated hereinafter.
FIG. 2 is an A-direction view of a simulated aircraft position adjustable foot pedal mechanism according to the present invention;
FIG. 3 is a B-B cross-sectional view of a simulated aircraft position adjustable foot pedal mechanism according to the present invention;
in the figure: 1-left pedal; 2-left slide block; 3-a left pedal rotation shaft; 4-left slider guide rail; 5-a left brake spring connecting shaft; 6-a left connecting rod rotating shaft; 7-a left brake spring; 8-a left pedal and left brake spring bracket connecting shaft; 9-left spring support guide shaft; 10-left spring support; 11-left connecting rod; 12-left U-shaped connecting rod; 13-a left U-shaped connecting rod and a left connecting rod connecting shaft; 14-a left U-shaped connecting rod rotating shaft; a 15-U-shaped connecting rod and a left screw rod connecting shaft; 16-connecting the left screw with the head slider; 17-left screw; 18-right screw; 19-a head swing stem rotating shaft; 20-head swing rod; 21-a position adjustment pin; 22-a brake line spring; 23-gate lines; 24-a brake line pulling plate; 25-head slider; 26-a return spring; 27-rudder differential limiting plates; 28-left slider with rudder pintle; 29-right slider; 30-rudder spring one; 31-a rudder spring lower connecting shaft; 32-rudder spring subframe; 33-right slider with rudder pintle; 34-a second rudder spring lower connecting shaft; 35-rudder spring II; 36-rudder spring upper mount.
Detailed Description
The following describes the embodiments of the present invention in further detail with reference to the accompanying drawings:
the first embodiment is as follows: the present embodiment is described with reference to fig. 1 to 3. The pedal mechanism capable of simulating the position of the aircraft comprises a left pedal system, a right pedal system, a head swing rod rotating shaft 19, a head swing rod 20, a position regulating pin 21, a brake line spring 22, a brake line 23, a brake line pulling plate 24, a head sliding block 25, two vertical pins, two return springs 26, a left sliding block rudder carrying pin 28, a rudder differential limiting plate 27, a first rudder spring 30, a lower rudder spring bracket 32, a right sliding block rudder carrying pin 33, a second rudder spring 35 and an upper rudder spring bracket 36;
the brake line pulling plate 24 is connected with the position adjusting pin 21 through a brake line 23, a brake line spring 22 is arranged between the brake line 23 and the position adjusting pin 21, the head swing rod 20 vertically penetrates through the head sliding block 25, a plurality of round holes which are longitudinally arranged are formed in the front side of the upper part of the head swing rod 20, the position adjusting pin 21 penetrates through a through hole of the head sliding block 25 and is matched with the round holes of the head swing rod 20 for position adjustment, the head swing rod 20 vertically penetrates through a head swing rod rotating shaft 19, the head swing rod rotating shaft 19 is connected with a front panel of the bracket, two vertical pins penetrate through two sides of the head sliding block 25, the return spring 26 is sleeved on the outer sides of the vertical pins and is positioned above the head sliding block 25, the left side of the head sliding block 25 is connected with a left pedal system, and the right side of the head sliding block 25 is connected with a right pedal system;
the left pedal system comprises a left pedal 1, a left sliding block 2, a left pedal rotating shaft 3, a left sliding block guide rail 4, a left brake spring 7, a left spring support guide shaft 9, a left spring support 10, a left connecting rod mechanism and a left screw rod 17; the left slider guide rail 4 is arranged between the brackets and is parallel to the bottom surface of the brackets, the left pedal 1 is rotationally connected with the left slider 2 through a left pedal rotating shaft 3, the left slider 2 horizontally moves along the left slider guide rail 4, one end of the left brake spring 7 is connected with the left slider 2 through a left brake spring connecting shaft 5, the other end of the left brake spring 7 is connected with the left spring bracket 10, the left pedal 1 is rotationally connected with the left spring bracket 10 through a left pedal and a left brake spring bracket connecting shaft 8, a long slot hole is formed in the left spring bracket 10, a left spring bracket guide shaft 9 is fixed on the left slider 2 and is matched with the long slot hole, one end of the left connecting rod mechanism is rotationally connected with the left slider 2, the other end of the left connecting rod mechanism is rotationally connected with the left screw 17, and the right pedal system is in mirror symmetry with the left pedal system and has the same structure;
the left pedal system is rotationally connected with the head slider 25 through a left screw rod 17 and a head slider connecting shaft 16 through the left screw rod, and the right pedal system is connected with the head slider 25 through a right screw rod 18; the upper bracket 36 of the rudder spring is fixed on the upper part of the left slider 2, the lower bracket 32 of the rudder spring is fixed on the lower part of the right slider 29, the lower end of the first 30 of the rudder spring is rotationally connected with one end of the lower bracket 32 of the rudder spring in the horizontal direction through a lower connecting shaft 31 of the rudder spring, the other end of the first 30 of the rudder spring is rotationally connected with the upper bracket 36 of the rudder spring through a lower connecting shaft 34 of the second of the rudder spring, the lower end of the second 35 of the rudder spring is connected with the other end of the lower bracket 32 of the rudder spring in the horizontal direction, the other end of the second 35 of the rudder spring is connected with the upper bracket 36 of the rudder spring, the left slider belt rudder pin 28 is vertically fixed on the upper bracket 36 of the rudder spring, the right slider belt rudder pin 33 is vertically fixed on the lower bracket 32 of the rudder spring, the upper long slot hole of the differential limiting plate 27 of the rudder passes through the left slider belt rudder pin 28, and the lower long slot hole of the differential limiting plate 27 of the rudder passes through the right slider belt rudder pin 33.
The left link mechanism comprises a left link 11, a left U-shaped link 12 and a left U-shaped link rotating shaft 14, one end of the left link 11 is connected with the left slider 2 through the left link rotating shaft 6, the other end of the left link is connected with the left U-shaped link 12 through the left U-shaped link connecting shaft 13, the left U-shaped link rotating shaft 14 is fixed on a support, the left U-shaped link 12 rotates around the left U-shaped link rotating shaft 14, and the left U-shaped link 12 is rotationally connected with the left screw 17 through a U-shaped link and the left screw connecting shaft 15.
The operation method of the pedal mechanism capable of simulating the position of the aircraft comprises the following steps:
1. braking action
Taking a left pedal brake as an example to explain how the mechanism acts when braking, the state shown in fig. 1 is the initial state of the mechanism when the pedal is fixed at a specific position after the front and rear positions of the pedal are adjusted. At this time, the left slider 2 is fixed at a certain fixed position on the left slider guide rail 4; when the left pedal 2 is stepped on, the left pedal 1 rotates around the left pedal rotating shaft 3, meanwhile, the left spring support 10 is driven by the left brake spring support connecting shaft 8, so that a self-length slotted hole moves under the constraint of the left spring support guide shaft 9, the slotted hole is used for limiting the angle of pedal rotating motion, simulating the actual rotating angle of the aircraft pedal, meanwhile, the left brake spring 7 is stretched, at the moment, the left pedal 1 can feel the force feeling of the left brake spring, the braking action is simulated, the larger the stepping angle of the left pedal 1 is, the longer the left brake spring 7 is stretched, and the force feeling fed back to the sole is larger, so that the whole braking process is simulated. The annular tooth piece is arranged on the pedal rotating shaft, and the gear potentiometer is arranged on the slide block at the same side, so that the brake electric signal can be detected and transmitted.
2. Pedal position adjustment action
Taking fig. 3 as an example, when the pedal position is to be adjusted, both feet are simultaneously stepped on the left pedal and the right pedal, the brake cable pulling plate 24 is pulled back around the rotation axis at the bottom of the pedal, the brake cable pulling plate 24 drives the brake cable 23 to pull out the position adjusting pin 21, at this time, the position adjusting pin 21 and the head slider 25 are released, under the action of stepping on the left pedal and the right pedal by both feet, the left pedal, the right slider, the brake spring mechanism and the rudder spring mechanism which are connected on the left slider and the right slider slide together forward along the slider guide rail, at this time, the left connecting rod 11 pushes the left U-shaped connecting rod 12 to rotate around the left U-shaped connecting rod rotation axis 14 which is fixed on the pedal bracket, so that the left screw 17 is driven to move the head slider 25 and the position adjusting pin 21 upward along the head swing rod 20, the return spring 26 is compressed, the sole feels the pressure of the return spring, at this time, when the left pedal and the right pedal moves to a comfortable position, the brake cable pulling plate 24 is released, the conical head of the position adjusting pin 21 falls into a certain round hole of the head 20, at this time, the pedal is fixed at the target adjusting position, at this time, and the rudder operation direction can be achieved.
3. Steering rudder action
Rudder springs are 2 in total: a first rudder spring 30 and a second rudder spring 35; the lower ends of the first rudder spring 30 and the second rudder spring 35 are connected with the lower rudder spring bracket 32, the lower rudder spring bracket 32 is fixed on the right slider 29, the upper ends of the first rudder spring 30 and the second rudder spring 35 are connected with the upper rudder spring bracket 36, and the upper rudder spring bracket 36 is fixed on the left slider 2. The upper long slot of the rudder differential limiting plate 27 passes through the left slider belt rudder pin 28 fixed on the rudder spring upper bracket 36, and the lower long slot of the rudder differential limiting plate 27 passes through the right slider belt rudder pin 33 fixed on the right slider 29.
When the left pedal 1 slides forwards, the left slider 2 slides forwards along the left slider guide rail 4 to drive the left connecting rod 11, the left U-shaped connecting rod 12 and the left screw rod 17 to move, so that the head swing rod 20 rotates around the head swing rod rotating shaft 19, the right screw rod 18 and the left screw rod 17 form a differential motion, the motion is transmitted to the right slider 29, the right slider 29 moves backwards, and the rudder swing action is simulated, at the moment, the first rudder spring 30 and the second rudder spring 35 are stretched, and the left sole and the right sole can feel the force sense of the rudder spring. The larger the rudder angle, the stronger the force sense. When the rudder swing is stopped, the left pedal and the right pedal return to the middle under the action of the rudder spring and are kept at the same position. The rack is arranged at the lower end of the head swing rod rotating shaft 19, and the gear potentiometer is arranged on the pedal bracket below, so that the rudder electric signal can be detected and transmitted.
The above specific embodiments are used for further detailed description of the objects, technical solutions and advantageous effects of the present invention. It should be understood that the foregoing description is only a specific example of the present invention, and is not intended to limit the invention, but rather is a reasonable combination of features described in the foregoing embodiments, and any modifications, equivalents, improvements, etc. that fall within the spirit and principles of the present invention are intended to be included within the scope of the present invention.

Claims (2)

1. The pedal mechanism capable of simulating the position of the aircraft is characterized by comprising a bracket, a left pedal system, a right pedal system, a head swing rod rotating shaft (19), a head swing rod (20), a position regulating pin (21), a brake line spring (22), a brake line (23), a brake line pulling plate (24), a head sliding block (25), two vertical pins, two return springs (26), a left sliding block rudder carrying pin (28), a rudder differential limiting plate (27), a first rudder spring (30), a lower rudder spring bracket (32), a right sliding block rudder carrying pin (33), a second rudder spring (35) and an upper rudder spring bracket (36);
the brake line pulling plate (24) is connected with the position adjusting pin (21) through a brake line (23), the position adjusting pin (21) slides in a cylindrical hole of the head sliding block (25), a brake line spring (22) is arranged between the brake line (23) and the position adjusting pin (21), the head swinging rod (20) vertically penetrates through the head sliding block (25), a plurality of round holes which are longitudinally arranged are formed in the front side of the head swinging rod (20), the position adjusting pin (21) is matched with the round holes and used for adjusting the position, a head swinging rod rotating shaft (19) vertically penetrates through the head swinging rod (20), the head swinging rod rotating shaft (19) is connected with a front panel of the bracket, two vertical pins penetrate through two sides of the head sliding block (25), a return spring (26) is sleeved on the outer side of the vertical pins and is positioned above the head sliding block (25), the left side of the head sliding block (25) is connected with a left pedal system, and the right side of the head sliding block (25) is connected with a right pedal system;
the left pedal system comprises a left pedal (1), a left sliding block (2), a left pedal rotating shaft (3), a left sliding block guide rail (4), a left brake spring (7), a left spring support guide shaft (9), a left spring support (10), a left connecting rod mechanism and a left screw rod (17); the left slider guide rail (4) is arranged between the brackets and is parallel to the bottom surface of the brackets, the left pedal (1) is rotationally connected with the left slider (2) through a left pedal rotating shaft (3), the left slider (2) horizontally moves along the left slider guide rail (4), one end of the left brake spring (7) is connected with the left slider (2), the other end of the left brake spring is connected with the left spring bracket (10), the left pedal (1) is rotationally connected with the left spring bracket (10), a long slot hole is formed in the left spring bracket (10), a left spring bracket guide shaft (9) is fixed on the left slider (2) and is matched with the long slot hole, one end of the left connecting rod mechanism is rotationally connected with the left slider (2), the other end of the left connecting rod mechanism is rotationally connected with the left screw (17), and the right pedal system is in mirror symmetry and has the same structure as the left pedal system.
The left pedal system is rotationally connected with the head slider (25) through a left screw (17), and the right pedal system is connected with the head slider (25) through a right screw (18); the upper bracket (36) of the rudder spring is fixed on the upper part of the left sliding block (2), the lower bracket (32) of the rudder spring is fixed on the lower part of the right sliding block (29), the lower end of the first (30) of the rudder spring is connected with one end of the horizontal direction of the bottom of the lower bracket (32) of the rudder spring, the other end of the first (30) of the rudder spring is connected with the upper bracket (36) of the rudder spring, the lower end of the second (35) of the rudder spring is rotationally connected with the other end of the horizontal direction of the bottom of the lower bracket (32) of the rudder spring, the other end of the second (35) of the rudder spring is rotationally connected with the upper bracket (36) of the rudder spring, the left sliding block belt rudder pin (28) is vertically fixed on the upper bracket (36) of the rudder spring, the upper hole of the rudder differential limiting plate (27) passes through the left sliding block belt rudder pin (28), and the lower long slot hole of the rudder differential limiting plate (27) passes through the right sliding block belt rudder pin (33).
2. The pedal mechanism with adjustable position for a simulated aircraft according to claim 1, wherein the left link mechanism comprises a left link (11), a left U-shaped link (12) and a left U-shaped link rotating shaft (14), one end of the left link (11) is connected with a left slider (2), the other end of the left link is connected with the left U-shaped link (12), the left U-shaped link rotating shaft (14) is fixed at the upper end of a bracket, the left U-shaped link (12) rotates around the left U-shaped link rotating shaft (14), and the left U-shaped link (12) is rotationally connected with a left screw (17) through a U-shaped link and a left screw connecting shaft (15).
CN202210252745.1A 2022-03-15 2022-03-15 Pedal mechanism capable of simulating position of aircraft Active CN114743430B (en)

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CN114743430B true CN114743430B (en) 2023-05-16

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Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20010094107A (en) * 2000-04-04 2001-10-31 최동환 Aircraft's rudder and brake pedal device
CN207149120U (en) * 2017-05-19 2018-03-27 中仿智能科技（上海）股份有限公司 A kind of aircraft rides analogue means
CN109326170A (en) * 2018-10-15 2019-02-12 中仿智能科技（上海）股份有限公司 A kind of foot-operated simulator of aircraft
WO2021133347A1 (en) * 2019-12-27 2021-07-01 Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi A pedal adjustment system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8353484B2 (en) * 2009-11-10 2013-01-15 Textron Innovations, Inc. Cockpit rudder control mechanism for an aircraft
CN203858777U (en) * 2014-04-02 2014-10-01 中国人民解放军93199部队飞行仿真技术研究所 Distance-regulating pedal mechanism of flight simulator
CN105857581B (en) * 2016-05-19 2018-10-02 中国商用飞机有限责任公司北京民用飞机技术研究中心 A kind of aircraft cockpit steerable system and method for operating

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
KR20010094107A (en) * 2000-04-04 2001-10-31 최동환 Aircraft's rudder and brake pedal device
CN207149120U (en) * 2017-05-19 2018-03-27 中仿智能科技（上海）股份有限公司 A kind of aircraft rides analogue means
CN109326170A (en) * 2018-10-15 2019-02-12 中仿智能科技（上海）股份有限公司 A kind of foot-operated simulator of aircraft
WO2021133347A1 (en) * 2019-12-27 2021-07-01 Tusas- Turk Havacilik Ve Uzay Sanayii Anonim Sirketi A pedal adjustment system

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