CN105810041B - It is a kind of for simulating the device of airplane throttle control system - Google Patents
It is a kind of for simulating the device of airplane throttle control system Download PDFInfo
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- CN105810041B CN105810041B CN201610363492.XA CN201610363492A CN105810041B CN 105810041 B CN105810041 B CN 105810041B CN 201610363492 A CN201610363492 A CN 201610363492A CN 105810041 B CN105810041 B CN 105810041B
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- sensor
- throttle lever
- pedestal
- throttle
- transmission mechanism
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- 230000005540 biological transmission Effects 0.000 claims abstract description 31
- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 claims abstract description 26
- 238000004088 simulation Methods 0.000 claims abstract description 8
- 238000001514 detection method Methods 0.000 claims abstract description 6
- 230000033001 locomotion Effects 0.000 claims description 14
- 238000006073 displacement reaction Methods 0.000 claims description 13
- 238000005452 bending Methods 0.000 claims description 3
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 claims 1
- 238000004364 calculation method Methods 0.000 abstract description 3
- 230000000694 effects Effects 0.000 description 5
- 238000012423 maintenance Methods 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 229910000831 Steel Inorganic materials 0.000 description 1
- 230000005611 electricity Effects 0.000 description 1
- 239000010721 machine oil Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000008450 motivation Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000010959 steel Substances 0.000 description 1
Classifications
-
- 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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- 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)
- Toys (AREA)
Abstract
The present invention relates to a kind of for simulating the device of airplane throttle control system comprising: pedestal；The throttle lever being rotatably arranged on pedestal；Driving mechanism that is on pedestal and being connected by transmission mechanism with throttle lever；And the first sensor being connected with transmission mechanism, the manipulation force that throttle lever is applied for detecting user；The controller being connected with driving mechanism and first sensor.Wherein, controller is configured to the detection signal based on first sensor come calculation of throttle control-rod to rotary speed, and controls driving mechanism driving throttle lever, promotes throttle lever to be rotated to rotary speed.The device for simulating airplane throttle control system of the invention can truer simulation airplane throttle control system, and performance easy to use is preferable.
Description
Technical field
The present invention relates to a kind of for simulating the device of airplane throttle control system.
Background technique
Airplane throttle control system is very important part in aircraft manipulation, is that pilot is directly docked with aircraft and connect
Mouthful.Device for simulating airplane throttle control system is used to simulate the operation resistance of the throttle lever of airplane throttle control system
Power and actual motion, for training new driver.
The existing device for simulating airplane throttle control system drives slip clutch using direct current generator, then
Linkage gear, chain and steel wire pull throttle lever to be moved forward and backward automatically to embody the automatic Pilot of aircraft.Work as automatic cruising
When turning to switch cruise manually, which can apply the resistance of motion to throttle lever using the coefficient of friction of slip clutch,
Relatively to feel that him is allowed to experience actual airplane throttle lever to aircraft pilot one, at this moment clutch is detached from direct current generator,
Reach the true effect of simulation actual airplane accelerator control.
Friction clutch relies primarily on friction plate to apply the above-mentioned resistance of motion, and friction plate is during operation often in mill
Damage state will lead to actual motion resistance and be lower than the setting resistance of motion gradually as the degree of wear of friction plate gradually increases, from
And reduce the simulated effect of the device for being used to simulate airplane throttle control system.Simultaneously as friction plate is in friction clutch
It is a component easy to wear in as soon as, therefore needs to readjust friction clutch at regular intervals, restores setting friction resistance
Power, and since adjustment process is completely felt to determine the resistance by adjustor, cause the adjusted result of device inaccurate.Letter
For it, the simulated effect of the device is poor, and performance easy to use is poor.
Summary of the invention
Based on the above issues, the object of the present invention is to provide a kind of for simulating the device of airplane throttle control system,
Can truer simulation airplane throttle control system, and performance easy to use is preferable.
The present invention provides a kind of for simulating the device of airplane throttle control system comprising: pedestal；Rotationally set
Throttle lever on the pedestal；Driving mechanism on the pedestal, the driving mechanism by transmission mechanism with
Throttle lever is connected；And the first sensor being connected with the transmission mechanism, throttle lever is applied for detecting user
The manipulation force added；The controller being connected with the driving mechanism and first sensor.Wherein, the controller is configured to base
In the detection signal of the first sensor come calculate the throttle lever to rotary speed, and control the driving mechanism and drive
The throttle lever is moved, the throttle lever is promoted to be rotated with described to rotary speed.
Further, which further includes the second sensor for detecting the moving displacement of the transmission mechanism, described
Second sensor is connected with controller.
Further, the second sensor is stay wire displacement sensor, and the stay wire displacement sensor is arranged described
On pedestal, and it is connected with the transmission mechanism.
Further, the driving mechanism includes direct current generator, and the transmission mechanism includes being set to the direct current generator
Sprocket wheel on output shaft, the shaft on the pedestal and the belt wheel in the shaft, and be used for the sprocket wheel
The chain belt component connected with belt wheel, the throttle lever are connected with belt wheel or shaft.
Further, the chain belt component is made of chain and band, the both ends of the chain respectively with the band group two
End is connected to form a closed loop.
Further, the transmission mechanism further includes the reverse wheel on the pedestal, the reverse wheel be set as by
Described one set angle of chain belt component bending between the sprocket wheel and belt wheel.
Further, the first sensor is the push-and-pull force snesor being connected in the chain belt component.
Further, the quantity of the throttle lever, driving mechanism, transmission mechanism and first sensor is all two,
So that the movement complementation interference of two throttle levers.
Further, the pedestal includes the horizontal being connected with each other and vertical shell, and the driving mechanism is equipped with institute
It states in horizontal, the throttle lever from top to bottom runs through the top of the vertical shell, and one of the transmission mechanism
It is arranged in the horizontal and another part is set in the vertical shell.
Further, the top of the vertical shell is the cylindrical surface of half.
Device for simulating airplane throttle control system of the invention relies primarily on first sensor, controller, driving
Mechanism and transmission mechanism realize digitized control, being capable of truer simulation airplane throttle control system.Simultaneously as
The device only needs manufacturer simply to be debugged, without using component easy to wear, therefore the device be used without through
Normal repair and maintenance, to be easy to improve the ease of use of the device.
Apparatus structure for simulating airplane throttle control system of the invention is simple, easily manufactured, safe and reliable,
Popularization and application convenient to carry out.
Detailed description of the invention
The invention will be described in more detail below based on embodiments and refering to the accompanying drawings.Wherein:
Fig. 1 shows the perspective view of the device for simulating airplane throttle control system of embodiment according to the present invention；
Fig. 2 shows the top view of the device for simulating airplane throttle control system of embodiment according to the present invention；
Fig. 3 is the cross-sectional view of the line A-A in Fig. 2.
Identical component uses identical appended drawing reference in the accompanying drawings.Attached drawing might not be drawn according to actual ratio.
Specific embodiment
The embodiment of the present invention is illustrated with reference to the accompanying drawing.
Fig. 1 shows the solid of the device 10 for simulating airplane throttle control system of embodiment according to the present invention
Figure, Fig. 2 show the top view of the device 10 for simulating airplane throttle control system of embodiment according to the present invention, Fig. 3
It is the cross-sectional view of the line A-A in Fig. 2.As shown in Fig. 1 to Fig. 3, which includes pedestal 1.The shape of pedestal 1 is not made especially
It limits, those skilled in the art, which can according to need, to be set.In the present embodiment, pedestal 1 includes the level being connected with each other
Shell 11 and vertical shell 12.Horizontal 11 and vertical shell 12 can all be set as closing shell or semi-closed casings.But it is
For the sake of convenient disassembly, horizontal 11 and vertical shell 12 are preferably semi-closed casings.
The device 10 further includes the throttle lever 2 being rotatably arranged on pedestal 1.In the present embodiment, Throttle Opening Control
Bar 2 from top to bottom runs through the top of vertical shell 12, and is connected with the shaft 52 being arranged in vertical shell 12, so as to throttle control
Bar 2 processed is able to carry out S1 forward or the backward movement of S2.For the movement of smooth throttle lever 2, the top of vertical shell 12
For the cylindrical surface (i.e. central angle be 180 ° cylindrical surface) of half.The structure of throttle lever 2 on throttle lever 2 and aircraft
It is identical, to improve the simulated effect of the device 10.
The device 10 further includes transmission mechanism 5 and the driving mechanism 4 on pedestal 1.Driving mechanism 4 passes through transmission mechanism
5 are connected with throttle lever 2, to drive throttle lever 2 to be rotated.Meanwhile the device 10 further includes and 5 phase of transmission mechanism
First sensor 3 even, and the controller being connected with driving mechanism 4 and first sensor 3.First sensor 3 is for detecting
The manipulation force that user applies throttle lever 2.Wherein, controller can be calculated based on the detection signal of first sensor 3
Throttle lever 2 to rotary speed, and control driving mechanism 4 drive throttle lever 2, promote it to be turned to rotary speed
It is dynamic.In detail, driving mechanism 4 be arranged in horizontal 21, transmission mechanism 5 a part be arranged in horizontal 21 and
Another part is set in vertical shell 22.Wherein, the controller mainly includes logic controller (PLC or CPU) and auxiliary electricity
Subcomponent (such as resistance, transformer and amplifier), belongs to well known to those skilled in the art, and details are not described herein.
When user using the embodiment of the present invention for simulating the device 10 of airplane throttle control system when, user first
Need to apply to throttle lever 2 S1 forward or the backward manipulation force of S2, when first sensor 3 detects manipulation force, control
Device according to the manipulation force come calculation of throttle control-rod 2 under the manipulation force needed for rotary speed, then controller is based on calculating
As a result driving mechanism 4 is accordingly controlled, so that driving mechanism 4 drives throttle lever 2 by transmission mechanism 5, makes throttle
Control-rod 2 to rotary speed to be rotated.Wherein, controller can based on resistance that the throttle lever of actual airplane is born with
Relationship between manipulation force come calculation of throttle control-rod 2 under the manipulation force needed for rotary speed and journey to be changed one's profession, the relationship
It can be from the existing device for simulating airplane throttle control system and the detection for treating simulation airplane throttle control system.
The device 10 for simulating airplane throttle control system of the embodiment of the present invention rely primarily on first sensor 3,
Controller, driving mechanism 4 and transmission mechanism 5 realize digitized control, being capable of truer simulation airplane throttle control
System.Simultaneously as the device 10 only needs manufacturer simply to be debugged, without using component easy to wear, therefore the dress
It sets 10 and is used without frequent repair and maintenance, to be easy to improve the ease of use of the device 10.
In a preferred embodiment, the device 10 for simulating airplane throttle control system further includes passing for detecting
The second sensor 6 of the moving displacement of motivation structure 5, the second sensor 6 are connected with controller.Second sensor 6 is chosen as red
The displacement sensors such as outer linear movement pick-up or stay wire displacement sensor.Controller can be based on the detection signal of second sensor 6
Appropriate adjustment is carried out to the movement of throttle lever 2, to improve the simulated effect of the device 10.Preferably, the second sensor 6
It is selected as the stay wire displacement sensor being arranged on pedestal 1, the bracing wire of the stay wire displacement sensor is connected with transmission mechanism 5, so that
Bracing wire can follow transmission mechanism 5 to be moved, and stay wire displacement sensor is enable accurately and unhinderedly to detect transmission mechanism 5
Moving displacement.
Driving mechanism 4 is chosen as the motor that direct current generator or servo motor etc. are easy to be precisely controlled revolving speed.In order to improve essence
For the sake of also reducing cost as far as possible while spending, driving mechanism 4 is selected as direct current generator.As shown in figure 3, transmission mechanism 5 includes setting
In the sprocket wheel 51 on the output shaft of direct current generator, the shaft 52 on pedestal 1 and the belt wheel 53, Yi Jiyong in shaft 52
In the chain belt component for connecting sprocket wheel 51 and belt wheel 53, throttle lever 2 is connected with belt wheel 53 or shaft 52.Work as driving machine
When structure 4 is run, the sprocket wheel 51 that driven-mechanism 4 drives is rotated by chain belt component band movable belt pulley 53, so that with band
The throttle lever 2 that wheel 53 or shaft 52 are connected is forced to be correspondingly rotated.Wherein, chain belt component is by chain 541 and band 542
Composition, the both ends of chain 541 are connected to form a closed loop with the both ends of band 542 respectively.Sprocket wheel 51 and belt wheel 53 are respectively positioned on chain
In inner ring with component.Wherein, band 542 is chosen as conventional drive belt, cordage or wirerope etc..
In the present embodiment, transmission mechanism 5 further includes the reverse wheel 55 on pedestal 1, is detailed in Fig. 3.Reverse wheel 55 is set
It is set to one set angle of chain belt component bending between sprocket wheel 51 and belt wheel 53.The set angle is only particularly limited to, excellent
It is selected as 90 °.Reverse wheel 55 can not only compress chain belt component, and avoid the design height of pedestal 1 excessively high.
In the present embodiment, first sensor 3 is selected as the push-and-pull force snesor being connected in chain belt component preferably, push-and-pull
Force snesor is located in the junction of sprocket wheel 51 and belt wheel 53.In this way, first sensor 3 can be detected accurately
The manipulation force that user applies throttle lever.In addition to the present embodiment, first sensor 3 is also selected as other type force-measuring sensings
Device.
In the present embodiment, the quantity of throttle lever 2, driving mechanism 4, transmission mechanism 5 and first sensor 3 is all two
It is a, so that the movement complementation interference of two throttle levers 2.Since the movement of each throttle lever 2 is by a driving machine
Structure 4 is driven, and the movement complementation interference of two throttle levers 2, the trim campaign of throttle is than conventional apparatus smooth flow
It is many.
The embodiment of the present invention for simulate airplane throttle control system device 10 can truer simulation fly
Machine oil accelerator control system, and performance easy to use is preferable.
Although by reference to preferred embodiment, invention has been described, the case where not departing from the scope of the present invention
Under, various improvement can be carried out to it and can replace component therein with equivalent.Especially, as long as there is no structures to rush
Prominent, items technical characteristic mentioned in the various embodiments can be combined in any way.The invention is not limited to
Specific embodiment disclosed herein, but include all technical solutions falling within the scope of the claims.
Claims (10)
1. a kind of for simulating the device of airplane throttle control system characterized by comprising
Pedestal；
The throttle lever being rotatably arranged on the pedestal；
Driving mechanism on the pedestal, the driving mechanism are connected by transmission mechanism with throttle lever；And
The first sensor being connected with the transmission mechanism, the manipulation force that throttle lever is applied for detecting user；
The controller being connected with the driving mechanism and first sensor, wherein the controller is configured to based on first
The manipulation force detected by sensor come calculate the throttle lever to rotary speed, and control the driving mechanism and drive
The throttle lever is moved, the throttle lever is promoted to be rotated with described to rotary speed；
Wherein, the relationship between resistance and manipulation force that the controller is born based on the throttle lever of actual airplane, meter
Needed for throttle lever is calculated under the manipulation force to rotary speed and journey to be changed one's profession, the relationship is from existing for simulating
The device of airplane throttle control system and the detection for treating simulation airplane throttle control system.
2. the apparatus according to claim 1, which is characterized in that further include the moving displacement for detecting the transmission mechanism
Second sensor, the second sensor is connected with controller.
3. the apparatus of claim 2, which is characterized in that the second sensor is stay wire displacement sensor, described
Stay wire displacement sensor setting is connected on the pedestal, and with the transmission mechanism.
4. according to claim 1 to device described in any one of 3, which is characterized in that the driving mechanism includes direct current generator,
The transmission mechanism include set on the direct current generator output shaft on sprocket wheel, the shaft on the pedestal and be set to institute
The belt wheel in shaft is stated, and the chain belt component for connecting the sprocket wheel and belt wheel, the throttle lever and band
Wheel or shaft are connected.
5. device according to claim 4, which is characterized in that the chain belt component is made of chain and band, the chain
Both ends be connected to form a closed loop with the both ends of the band group respectively.
6. device according to claim 4, which is characterized in that the transmission mechanism further includes changing on the pedestal
To wheel, the reverse wheel is set as described one set angle of chain belt component bending between the sprocket wheel and belt wheel.
7. device according to claim 4, which is characterized in that the first sensor is to be connected in the chain belt component
Push-and-pull force snesor.
8. according to claim 1 to device described in any one of 3, which is characterized in that the throttle lever, driving mechanism,
The quantity of transmission mechanism and first sensor is all two, so that the movement complementation interference of two throttle levers.
9. according to claim 1 to device described in any one of 3, which is characterized in that the pedestal includes the water being connected with each other
Flat shell and vertical shell, the driving mechanism are equipped in the horizontal, and the throttle lever from top to bottom runs through institute
State the top of vertical shell, a part of the transmission mechanism be equipped in the horizontal and another part be set to it is described vertical
In shell.
10. device according to claim 9, which is characterized in that the top of the vertical shell is the cylindrical surface of half.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610363492.XA CN105810041B (en) | 2016-05-27 | 2016-05-27 | It is a kind of for simulating the device of airplane throttle control system |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201610363492.XA CN105810041B (en) | 2016-05-27 | 2016-05-27 | It is a kind of for simulating the device of airplane throttle control system |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN105810041A CN105810041A (en) | 2016-07-27 |
| CN105810041B true CN105810041B (en) | 2019-06-25 |
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| CN201610363492.XA Expired - Fee Related CN105810041B (en) | 2016-05-27 | 2016-05-27 | It is a kind of for simulating the device of airplane throttle control system |
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Families Citing this family (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106898186B (en) * | 2017-03-28 | 2019-06-07 | 天津中天翔翼航空科技有限公司 | Aircraft Simulator accelerator control device |
| CN112951029B (en) * | 2021-01-22 | 2023-05-05 | 武汉木仓科技股份有限公司 | Pedal operation detection device of driving training robot and vehicle |
| CN115057002B (en) * | 2022-08-11 | 2022-11-01 | 北京天创凯睿科技有限公司 | Automatic following measuring device for automatic accelerator of airplane |
Family Cites Families (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US7107196B2 (en) * | 2002-03-21 | 2006-09-12 | International Business Machines Corporation | Model controller computer interface |
| CN102452481A (en) * | 2010-10-29 | 2012-05-16 | 贵州华阳电工有限公司 | Automatic throttle table operating device |
| CN103794104A (en) * | 2012-12-03 | 2014-05-14 | 天津工业大学 | Flight simulator autothrottle system |
| CN103092190B (en) * | 2013-01-04 | 2015-06-24 | 中国商用飞机有限责任公司 | Control force automatic checkout system for side lever controller |
| CN104658370B (en) * | 2014-11-19 | 2018-12-11 | 中国航空工业集团公司沈阳飞机设计研究所 | A kind of integrated form manual operation device in pilot individual's auxiliary system |
-
2016
- 2016-05-27 CN CN201610363492.XA patent/CN105810041B/en not_active Expired - Fee Related
Non-Patent Citations (1)
| Title |
|---|
| 《飞行模拟机电动式辅助操纵负荷***的仿真》;廖峰;《科学技术与工程》;20120731;全文 |
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Granted publication date: 20190625 |