CN107993514B - Special simulation parking control mechanism for aircraft simulator - Google Patents
Special simulation parking control mechanism for aircraft simulator Download PDFInfo
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- CN107993514B CN107993514B CN201810037454.4A CN201810037454A CN107993514B CN 107993514 B CN107993514 B CN 107993514B CN 201810037454 A CN201810037454 A CN 201810037454A CN 107993514 B CN107993514 B CN 107993514B
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- main shaft
- bracket
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- parking
- shaft
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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
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- 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)
- Instructional Devices (AREA)
Abstract
The invention discloses a special simulation parking control mechanism for an aircraft simulator, wherein: including support, main shaft and parking handle, a linear sensor is fixed to the support front end, the main shaft passes support and linear sensor, the front portion of main shaft sets up a pressure spring, the pressure spring cover is on the main shaft, be equipped with gear card structure on the support, gear card structure is including the card axle of frame on the support, the left and right sides of card axle is equipped with the extension spring, be provided with the tooth's socket of a plurality of axial arrangement on the main shaft, tooth's socket and card axle circumference stagger 90, the parking handle can drive the main shaft for support rotation 90 for tooth's socket and card axle are in same axial plane, linear sensor can respond to the circumference rotation angle and rotation speed and axial sliding length and the sliding speed of main shaft. The simulation system has the advantages of high simulation degree and capability of collecting operation data of a trainee when the trainee uses the simulation parking control mechanism.
Description
Technical Field
The invention belongs to the technical field of aircraft simulators, and particularly relates to a special simulation parking control mechanism for an aircraft simulator.
Background
With the implementation of the low-altitude open policy in China, the national navigation industry will be increased in an explosive manner in the next 20 years, and the navigation flight simulator has considerable market prospect and great development potential. The current domestic navigation simulator market is basically monopolized by foreign imported equipment, and the price is high. In view of this situation, it is highly desirable to autonomously develop a flight simulator of its own. The parking control mechanism is one of important control components for controlling the aircraft, and is very important for ground stability control of the aircraft. However, the simulation parking control mechanism for the aircraft simulator cannot be purchased in the market, and the mounting parking control mechanism on the aircraft cannot be directly used on the simulator, so that in order to develop a complete flight simulator, a special simulation parking control mechanism for the flight simulator needs to be developed first.
Disclosure of Invention
The technical problem to be solved by the invention is to provide the special simulation parking control mechanism for the aircraft simulator, which has high simulation degree and can collect operation data when a trainee uses the simulation parking control mechanism, aiming at the defects in the prior art.
In order to achieve the technical purpose, the invention adopts the following technical scheme:
Special emulation parking operating device of aircraft simulator, wherein: the device comprises a support, a main shaft and a parking handle, wherein a fixing frame is arranged on the support, the support is fixed on an instrument board of an aircraft simulator through the fixing frame, a linear sensor is fixed at the front end of the support, the main shaft penetrates through the support and the linear sensor, a pressure spring is arranged at the front part of the main shaft, the pressure spring is sleeved on the main shaft, one end of the pressure spring is fixedly connected with the front end of the main shaft, the other end of the pressure spring is fixedly connected with a shell of the linear sensor, the parking handle is fixed at the rear end of the main shaft, a gear clamping structure is arranged on the support and comprises a clamping shaft which is arranged on the support, tension springs are arranged on the left side and the right side of the clamping shaft, one end of each tension spring is fixedly connected with the support, the other end of each tension spring is fixedly connected with the clamping shaft, the tension springs can push the clamping shaft to the main shaft, a plurality of tooth grooves which are axially arranged are staggered by 90 degrees in the circumferential direction of the main shaft relative to the support, the tooth grooves and the clamping shaft are in the same axial plane, when the parking handle drives the main shaft to slide backwards relative to the support, the clamping shaft can be clamped into the tooth grooves under the action of the elasticity of the tension springs, the clamping shaft can not slide forwards relative to the support, the main shaft can not slide relative to the rotating angle and the rotating speed of the main shaft and the rotation angle and the axial sliding speed of the main shaft and the aircraft can control the sliding speed of the aircraft.
In order to optimize the technical scheme, the specific measures adopted further comprise:
The number of the fixing frames is two, one fixing frame is arranged in the middle of the support, the other fixing frame is arranged at the rear of the support, the middle of the fixing frame is a butterfly-shaped frame, the fixing frame and the support are fixed into a whole, threaded holes are formed in butterfly wings of the fixing frame, and the fixing frame is fixed on an instrument board of the aircraft simulator through fasteners penetrating through the threaded holes.
The number of the tooth grooves is five, one side surface of the tooth groove, which is close to the parking handle, is a vertical surface, one side surface of the tooth groove, which is far away from the parking handle, is a slope surface, and a clamping shaft in the tooth groove can be clamped by the vertical surface, so that the main shaft cannot move forwards, and the clamping shaft can slide out of the tooth groove from the slope surface, so that the main shaft can move backwards smoothly.
The front end of the main shaft is fixed with a front end fixing sheet, and the front end of the pressure spring is fixed on the front end fixing sheet.
The two ends of the clamping shaft are respectively fixed on the two fixing lugs, the bracket extends out of the bracket leg at the position corresponding to the tension spring, one end of the tension spring is fixedly connected with the fixing lugs, the other end of the tension spring is fixedly connected with the bracket leg, the tension spring is perpendicular to the main shaft, and the tension spring vertically pulls the clamping shaft to the main shaft.
The parking handle is an L-shaped handle.
The linear sensor described above is composed of a linear velocity sensor and an angular velocity sensor.
The bracket, the main shaft and the parking handle are all made of stainless steel materials.
The invention can clearly park the aircraft in the control by researching the parking mechanism on the real aircraft. The parking handle operating mechanism has the functions of different operations, and the different operations have influence on the airplane. A loop is formed from the pilot operation input to the feedback of the parking control mechanism and the feedback of the aircraft flight performance. The special simulation parking control mechanism for the flight simulator is basically the same as the real aircraft parking control mechanism in appearance and operation, and the parking mechanism feedback and the aircraft performance feedback are basically the same as the real aircraft performance feedback, so that the use requirement of the flight simulator can be met. The aircraft performance feedback part is realized by simulator flight performance simulation software, and does not belong to the scope of the invention, and the invention only needs to feed back the position of the parking handle to the performance simulation software in real time. The hand feeling and the appearance of the parking control mechanism are the same as those of a real airplane parking handle, but the internal structure has obvious differences, and the front end of the parking control mechanism generates the linked hand feeling between the bracket and the main shaft through the tension spring structure, but not the transmission structure of the real airplane parking handle. According to the invention, the operation information of the driver is collected through the linear sensor and is transmitted to the control chip of the aircraft simulator, so that the operation style of the driver, whether the operation is wrong or not and the like are conveniently analyzed.
The invention has the advantages of high simulation degree, capability of collecting operation data of a trainee when using the simulation parking control mechanism, and capability of teaching and training.
Drawings
FIG. 1 is a schematic diagram of the structure of the present invention;
FIG. 2 is a top view of FIG. 1;
Fig. 3 is a left side view of fig. 1.
Wherein the reference numerals are as follows: the parking device comprises a bracket 1, a fixing frame 11, a main shaft 2, tooth grooves 21, a front end fixing piece 22, a parking handle 3, a linear sensor 4, a pressure spring 5, a gear clamping structure 6, a clamping shaft 61, a tension spring 62, a fixing lug 63 and a bracket foot 64.
Detailed Description
Embodiments of the present invention are described in further detail below with reference to the accompanying drawings.
The invention relates to a special simulation parking control mechanism for an aircraft simulator, wherein: comprises a bracket 1, a main shaft 2 and a parking handle 3, wherein a fixing frame 11 is arranged on the bracket 1, the bracket 1 is fixed on an instrument board of an airplane simulator through the fixing frame 11, a linear sensor 4 is fixed at the front end of the bracket 1, the main shaft 2 passes through the bracket 1 and the linear sensor 4, a pressure spring 5 is arranged at the front part of the main shaft 2, the pressure spring 5 is sleeved on the main shaft 2, one end of the pressure spring is fixedly connected with the front end of the main shaft 2, the other end of the pressure spring is fixedly connected with a shell of the linear sensor 4, the parking handle 3 is fixed at the rear end of the main shaft 2, a gear clamping structure 6 is arranged on the bracket 1, the gear clamping structure 6 comprises a clamping shaft 61 which is arranged on the bracket 1, tension springs 62 are arranged at the left side and the right side of the clamping shaft 61, one end of each tension spring 62 is fixedly connected with the bracket 1, the other end of each tension spring is fixedly connected with the clamping shaft 61, the tension spring 62 can pull the clamping shaft 61 to prop against the main shaft 2, a plurality of tooth grooves 21 which are axially arranged are arranged on the main shaft 2, the tooth grooves 21 are circumferentially staggered with the clamping shaft 61 by 90 degrees, the parking handle 3 can drive the main shaft 2 to rotate 90 degrees relative to the bracket 1, the tooth grooves 21 and the clamping shaft 61 are in the same axial plane, when the parking handle 3 drives the main shaft 2 to slide backwards relative to the bracket 1, the clamping shaft 61 can be clamped into the tooth grooves 21 under the elastic force of the tension spring 62, the main shaft 2 cannot slide forwards relative to the bracket 1, and the linear sensor 4 can sense the circumferential rotation angle, the rotation speed, the axial sliding length and the sliding speed of the main shaft 2 and transmit signals to an aircraft simulator control chip.
In the embodiment, the number of the fixing frames 11 is two, one is arranged in the middle of the bracket 1, the other is arranged at the rear of the bracket 1, the fixing frames 11 are butterfly frames, the middle of the fixing frames 11 and the bracket 1 are fixed into a whole, threaded holes are formed in the butterfly wings of the fixing frames 11, and the fixing frames 11 are fixed on an instrument board of the aircraft simulator through fasteners penetrating through the threaded holes.
In the embodiment, the number of tooth grooves 21 is five, one side surface of the tooth groove 21, which is close to the parking handle 3, is a vertical surface, one side surface of the tooth groove 21, which is far away from the parking handle 3, is a slope surface, and the clamping shaft 61 in the tooth groove 21 can be clamped by the vertical surface, so that the spindle 2 cannot move forward, and the clamping shaft 61 can slide out of the tooth groove 21 from the slope surface, so that the spindle 2 can move backward smoothly.
In the embodiment, the front end of the main shaft 2 is fixed with a front end stator 22, and the front end of the compression spring 5 is fixed on the front end stator 22.
In the embodiment, two ends of the clamping shaft 61 are respectively fixed on two fixing lugs 63, the bracket 1 extends out of a bracket leg 64 at a position corresponding to the tension spring 62, one end of the tension spring 62 is fixedly connected with the fixing lugs 63, the other end of the tension spring 62 is fixedly connected with the bracket leg 64, the tension spring 62 is perpendicular to the main shaft 2, and the tension spring 62 vertically pulls the clamping shaft 61 to the main shaft 2.
In an embodiment, the parking handle 3 is an L-shaped handle.
In the embodiment, the linear sensor 4 is composed of a linear velocity sensor and an angular velocity sensor.
In the embodiment, the bracket 1, the spindle 2 and the parking handle 3 are all made of stainless steel materials.
The special simulation parking control mechanism for the aircraft simulator mainly comprises a pressure spring 5, a linear sensor 4, a main shaft 2, a bracket 1, a tension spring 62, a parking handle 3, screws used for installing the device on an instrument board of the aircraft simulator and the like. The bracket 1 has the functions of supporting, connecting and fixing the whole mechanism and can be integrally mounted on an instrument panel of the aircraft simulator. The parking handle 3 is the only operating part of the mechanism, and the operating method and the operating angle are basically the same as those of a real airplane parking operating handle. The action of the tension spring 62 ensures that the spindle 2 is locked when the parking handle is in the stowed angle and position. The function of the pressure spring 5 is to give forward tension to the parking handle, ensuring that the parking handle can rebound to the correct position normally when the handle is released. The linear sensor 4 is used for collecting the current position of the main shaft 2 in real time and feeding back to flight performance simulation software.
The front and rear of the simulation parking control mechanism is divided into five gears. Representing different parking forces, when the parking handle is positioned at the put-down position, the parking handle can be pulled to the position of the corresponding gear when the parking handle is to be parked, then the handle is gently put away after rotating 90 degrees anticlockwise, or the handle can be rotated 90 degrees anticlockwise, and then the parking handle is gently put away after being pulled to the position of the corresponding gear. If the gear is insufficient, the handle can be pulled outwards to a higher gear and then the hand is gently released. When the parking handle is in the retracted position, the handle is only required to be put down by rotating 90 degrees clockwise, and then the hand is gently put down. If the gear is to be lowered, the user needs to rotate 90 degrees clockwise, push the gear to the corresponding gear position, then rotate the gear counterclockwise by 90 degrees, and then lightly release the hand. The operation is the same as for a real aircraft parking handle.
The above is only a preferred embodiment of the present invention, and the protection scope of the present invention is not limited to the above examples, and all technical solutions belonging to the concept of the present invention belong to the protection scope of the present invention. It should be noted that modifications and adaptations to the invention without departing from the principles thereof are intended to be within the scope of the invention as set forth in the following claims.
Claims (1)
1. The special simulation parking control mechanism for the aircraft simulator is characterized in that: comprises a bracket (1), a main shaft (2) and a parking handle (3), wherein a fixing frame (11) is arranged on the bracket (1), the bracket (1) is fixed on an instrument board of an aircraft simulator through the fixing frame (11), a linear sensor (4) is fixed at the front end of the bracket (1), the main shaft (2) penetrates through the bracket (1) and the linear sensor (4), a pressure spring (5) is arranged at the front part of the main shaft (2), the pressure spring (5) is sleeved on the main shaft (2), one end of the pressure spring is fixedly connected with the front end of the main shaft (2), the other end of the pressure spring is fixedly connected with a shell of the linear sensor (4), the parking handle (3) is fixed at the rear end of the main shaft (2), the support (1) is provided with a gear clamping structure (6), the gear clamping structure (6) comprises a clamping shaft (61) which is arranged on the support (1), tension springs (62) are arranged on the left side and the right side of the clamping shaft (61), one end of each tension spring (62) is fixedly connected with the support (1), the other end of each tension spring is fixedly connected with the clamping shaft (61), the tension springs (62) can pull the clamping shaft (61) to abut against the main shaft (2), a plurality of tooth grooves (21) which are axially arranged are formed in the main shaft (2), the tooth grooves (21) are circumferentially staggered by 90 degrees with the clamping shaft (61), the parking handle (3) can drive the main shaft (2) to rotate 90 degrees relative to the bracket (1) so that the tooth grooves (21) and the clamping shaft (61) are positioned on the same axial plane, when the parking handle (3) drives the main shaft (2) to slide backwards relative to the bracket (1), the clamping shaft (61) can be clamped into the tooth grooves (21) under the elastic force of the tension spring (62), so that the main shaft (2) cannot slide forwards relative to the bracket (1), and the linear sensor (4) can sense the circumferential rotation angle, the rotation speed, the axial sliding length and the sliding speed of the main shaft (2) and transmit signals to the aircraft simulator control chip; the number of the fixing frames (11) is two, one fixing frame is arranged in the middle of the bracket (1), the other fixing frame is arranged at the rear part of the bracket (1), the fixing frames (11) are butterfly frames, the middle of the fixing frames (11) and the bracket (1) are fixed into a whole, threaded holes are formed in wings of the fixing frames (11), and the fixing frames (11) are fixed on an instrument board of the aircraft simulator through fasteners passing through the threaded holes; the number of the tooth grooves (21) is five, one side surface of the tooth groove (21) close to the parking handle (3) is a vertical surface, one side surface of the tooth groove (21) far away from the parking handle (3) is a slope surface, a clamping shaft (61) positioned in the tooth groove (21) can be clamped by the vertical surface, so that the main shaft (2) cannot move forwards, and the clamping shaft (61) can slide out of the tooth groove (21) from the slope surface, so that the main shaft (2) can move backwards smoothly; the two ends of the clamping shaft (61) are respectively fixed on two fixing lugs (63), the bracket (1) extends out of a bracket foot (64) at a position corresponding to the tension spring (62), one end of the tension spring (62) is fixedly connected with the fixing lugs (63), the other end of the tension spring is fixedly connected with the bracket foot (64), the tension spring (62) is perpendicular to the main shaft (2), and the tension spring (62) vertically pulls the clamping shaft (61) to the main shaft (2); the front end of the main shaft (2) is fixed with a front end fixing plate (22), and the front end of the pressure spring (5) is fixed on the front end fixing plate (22); the parking handle (3) is an L-shaped handle; the linear sensor (4) consists of a linear speed sensor and an angular speed sensor; the bracket (1), the main shaft (2) and the parking handle (3) are all made of stainless steel materials; the simulated parking control mechanism is divided into five gears from front to back and represents different parking forces, when the parking handle is positioned at the down position, the parking handle is pulled to the position of the corresponding gear when the parking handle is to be parked, then the handle is released after being rotated 90 degrees anticlockwise, or the handle is rotated 90 degrees anticlockwise and then is released after being pulled to the position of the corresponding gear, if the gear is insufficient, the handle is pulled to the higher gear and then is released continuously, when the parking handle is positioned at the up position, the parking handle is to be put down, only the handle is required to be rotated 90 degrees clockwise, then is released, if the parking handle is required to be rotated 90 degrees clockwise, and is rotated 90 degrees anticlockwise after being pushed to the position of the corresponding gear, and then hands are put away.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810037454.4A CN107993514B (en) | 2018-01-16 | 2018-01-16 | Special simulation parking control mechanism for aircraft simulator |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201810037454.4A CN107993514B (en) | 2018-01-16 | 2018-01-16 | Special simulation parking control mechanism for aircraft simulator |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN107993514A CN107993514A (en) | 2018-05-04 |
| CN107993514B true CN107993514B (en) | 2024-06-11 |
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| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201810037454.4A Active CN107993514B (en) | 2018-01-16 | 2018-01-16 | Special simulation parking control mechanism for aircraft simulator |
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| CN (1) | CN107993514B (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN110310543B (en) * | 2019-05-30 | 2025-01-28 | 福建科德电子科技有限公司 | A flap control device for simulating an aircraft |
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| CN201281902Y (en) * | 2008-09-26 | 2009-07-29 | 昆明理工大学 | Device for detecting and correcting feet brake of automobilism simulator |
| CN201745746U (en) * | 2010-07-16 | 2011-02-16 | 中国航空工业集团公司西安飞机设计研究所 | Electrical signal transmission steering braking system on airplane |
| CN102530247A (en) * | 2012-01-05 | 2012-07-04 | 西安航空制动科技有限公司 | Return mechanism for automatic braking selection switch |
| CN202633119U (en) * | 2012-06-18 | 2012-12-26 | 中国航空工业集团公司西安飞机设计研究所 | Automatic brake selection switch |
| CN103303462A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Vertical spindle foot control system |
| CN208655067U (en) * | 2018-01-16 | 2019-03-26 | 镇江爱维森仿真科技有限公司 | The dedicated emulated parking control mechanism of Aircraft Simulator |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP4516485B2 (en) * | 2005-06-14 | 2010-08-04 | 本田技研工業株式会社 | Motorcycle transmission, motorcycle and motorcycle simulation device |
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2018
- 2018-01-16 CN CN201810037454.4A patent/CN107993514B/en active Active
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN201281902Y (en) * | 2008-09-26 | 2009-07-29 | 昆明理工大学 | Device for detecting and correcting feet brake of automobilism simulator |
| CN201745746U (en) * | 2010-07-16 | 2011-02-16 | 中国航空工业集团公司西安飞机设计研究所 | Electrical signal transmission steering braking system on airplane |
| CN102530247A (en) * | 2012-01-05 | 2012-07-04 | 西安航空制动科技有限公司 | Return mechanism for automatic braking selection switch |
| CN103303462A (en) * | 2012-03-09 | 2013-09-18 | 陕西飞机工业（集团）有限公司 | Vertical spindle foot control system |
| CN202633119U (en) * | 2012-06-18 | 2012-12-26 | 中国航空工业集团公司西安飞机设计研究所 | Automatic brake selection switch |
| CN208655067U (en) * | 2018-01-16 | 2019-03-26 | 镇江爱维森仿真科技有限公司 | The dedicated emulated parking control mechanism of Aircraft Simulator |
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| CN107993514A (en) | 2018-05-04 |
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Effective date of registration: 20240515 Address after: 201620 Building 1, 1128 Wenhui Road, Songjiang District, Shanghai Applicant after: Shanghai Fengru Aviation Technology Co.,Ltd. Country or region after: China Address before: No.98, Dagang Peishan Road, New District, Zhenjiang City, Jiangsu Province Applicant before: ZHENJIANG AIWEISEN SIMULATION TECHNOLOGY Co.,Ltd. Country or region before: China |
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