CN206210171U - A kind of new flight control system manipulates load device - Google Patents
A kind of new flight control system manipulates load device Download PDFInfo
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- CN206210171U CN206210171U CN201621115003.0U CN201621115003U CN206210171U CN 206210171 U CN206210171 U CN 206210171U CN 201621115003 U CN201621115003 U CN 201621115003U CN 206210171 U CN206210171 U CN 206210171U
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Abstract
The utility model belongs to aircraft control system equipment technical field, more particularly to a kind of new flight control system manipulates load device, and the new flight control system manipulates load device, including：Main driving device, control wheel, control stick, case lid, longitudinal transmission mechanism, pedal transmission mechanism, service brake mechanism of car, transverse transmission mechanism, copilot device, pedal, simulator master computer, Ethernet interface, trimmer is switched, system protector, indicator lamp, servo-control system, oil sources, the present apparatus is respectively arranged with the main driving device and the copilot device, the utility model is rational in infrastructure, it is with strong points, vertical load system can simulate the control wheel/bar of aircraft, the force characteristic of pedal, and can be according to the rudder face aerodynamic loading of different flight state, real-time adjustment force characteristic, and realize automatic pilot lag function, in real time, realistically reproduction aircraft under different flying conditions and different operating pattern lower-pilot systems static and dynamic c haracteristics.
Description
Technical field
The utility model belongs to aircraft control system equipment technical field, more particularly to a kind of new flight control system is manipulated and born
Lotus device.
Background technology
Flight control system has reversible and irreversible two type, and analog machine steerable system is all reversible.
The control mode of analog machine steerable system can be divided into:Semi physical steerable system, analog steerable system, numeral
Formula steerable system.
The power that semi physical control system simulation load is produced by rubber band spring etc. due to physical deformation, control run is led to
Analog machine computer is directly inputted after crossing displacement transducer and A/D converter.Feature:Simply, low cost.Shortcoming:Steering force is not
Energy change at random, only strong sense, but it is untrue.
The steering force of analog steerable system trainee resolves part and resolves by simulation, and the calculation result of gained is one
Individual analog signal, then removes drive load analog machine again, trainee is had a real-time change, there is steering force sense true to nature
Feel.But, simulation resolves part and is made up of various Function generators, not only debugs difficult, and system drifting is big.
The steering force of digital steerable system trainee is compared with theoretical power, and part is resolved by the numeral such as CPU
Resolving draws a data signal, then by after conversion, by D/A conversions, then removing drive load analog machine, makes trainee
The manipulation force feeling that the steering force of member has a real-time change, is really true to life, wherein it is also steering force control that numeral resolves part
A link in loop.
The content of the invention
In view of the shortcomings of the prior art, the purpose of this utility model is to provide a kind of rational in infrastructure, with strong points,
Vertical load system can simulate the control wheel/bar of aircraft, the force characteristic of pedal, and can be according to the rudder face of different flight state
Aerodynamic loading, real-time adjustment force characteristic, and automatic pilot lag function is realized, in real time, realistically reappear aircraft in difference
With the static and dynamic c haracteristics of different operating pattern lower-pilot systems under flying condition.
To achieve these goals, the technical solution adopted in the utility model is as follows：
The new flight control system manipulates load device, including：Main driving device, control wheel, control stick, case lid, longitudinal direction transmission
Mechanism, pedal transmission mechanism, service brake mechanism of car, transverse transmission mechanism, copilot device, pedal, simulator master computer, Ethernet
Mouthful, trimmer switch, system protector, indicator lamp, servo-control system, oil sources, the present apparatus is respectively arranged with the main driving
Device and the copilot device, the control wheel are connected with the control stick, and the control stick is connected with the case lid, the pedal
It is arranged on the both sides of the case lid, the case lid bottom is provided with the pedal transmission mechanism, the transverse transmission mechanism is by institute
Main driving device and copilot device connection are stated, the pedal transmission mechanism is provided with the service brake mechanism of car, and the longitudinal direction passes
Motivation structure is connected with people's electrification machine rocking arm, and the simulator master computer is connected by Ethernet with the Ethernet interface, system
It is provided with the trimmer switch, the system protector and the indicator lamp, the system protector and the SERVO CONTROL
System is connected, and the mechanical mechanism of device is connected with the oil sources.
By using above-mentioned technical proposal, the new flight control system manipulates load device, including：Main driving device, control wheel,
Control stick, case lid, longitudinal transmission mechanism, pedal transmission mechanism, service brake mechanism of car, transverse transmission mechanism, copilot device, pedal,
Simulator master computer, Ethernet interface, trimmer switch, system protector, indicator lamp, servo-control system, oil sources, the present apparatus
The main driving device and the copilot device are respectively arranged with, the control wheel is connected with the control stick, and the control wheel makes
Welding, polishing after being processed using digital control processing point two sides with aluminium, surface carry out sandblasting, plastic-spraying treatment, install inlet switch, energy
Enough extend the service life of the control wheel, the control stick is connected with the case lid, and the pedal is arranged on the case lid
Both sides, the case lid bottom is provided with the pedal transmission mechanism, and the transverse transmission mechanism is by the main driving device and described
Copilot device is connected, and the pedal transmission mechanism is provided with the service brake mechanism of car, and the service brake mechanism of car is changed by rocking arm,
Rocking arm drives left foot, right crus of diaphragm power transmission shaft, and the service brake for respectively being driven left and right with two axles is in parallel, and the service brake mechanism of car is designed as a left side
Right linkage, it is automatic return, the strength of service brake reduction torsion spring is adjustable, the pedal uses aluminium digital control processing, design and produce captain,
Copilot linkage operating mechanism, is connected with people's electrification machine rocking arm, and the pedal has the function from returning, the direction of driver and copilot
Pedal described in rudder can realize linkage.Pilot can adjust the pedal to suitable actuated position, and the pedal adjusts stroke
261.6mm, regulation handle is in lower section just, on copilot's central instrument panel, and 10 grades of regulation shelves are adjustable 4 grades forward, adjustable backward
6 grades, longitudinal transmission mechanism is connected with people's electrification machine rocking arm, and the simulator master computer passes through Ethernet and the ether
Network interface connection, system is provided with trimmer switch, the system protector and the indicator lamp, the system protector with
The servo-control system connection, the mechanical mechanism of device is connected with the oil sources, and the motor that the present apparatus is used is for without moment of torsion arteries and veins
Dynamic AC servo motor, small rotary inertia, ultra-low torque pulsation, small volume, output torque is big, by monopole planetary gear speed reducing mechanism
Directly with steerable system connection, high pulling torque is exported, realize direct drive, overcome using the firm of various traditional reducing gears generations
Property gap, it is ensured that system mechanics manipulate smooth, and the remote control of the simulator master computer passes through standard industry Ethernet
Bus marco control loads controller, realizes three real-time controls of passage, and the cycle of operation of control software is controlled in 2KHz/
More than s, makes power be reached with Bit andits control accurately identical with aircraft actual curve.
The utility model is further arranged to：The control wheel is welded after being processed using digital control processing point two sides using aluminium
Connect, polish, surface carries out sandblasting, plastic-spraying treatment, installs inlet switch.
By using above-mentioned technical proposal, the control wheel processed using digital control processing point two sides using aluminium after welding,
Polishing, surface carries out sandblasting, plastic-spraying treatment, installs inlet switch, can extend the service life of the control wheel.
The utility model is further arranged to：The pedal uses aluminium digital control processing, designs and produces captain, copilot connection
Dynamic operating mechanism, is connected with people's electrification machine rocking arm.
By using above-mentioned technical proposal, the pedal uses aluminium digital control processing, designs and produces captain, copilot linkage
Operating mechanism, is connected with people's electrification machine rocking arm, and the pedal has the function from returning, pedal described in the rudder of driver and copilot
Linkage can be realized.Pilot can adjust the pedal to suitable actuated position, and the pedal adjusts stroke 261.6mm, adjusts
Section handle is in lower section just, on copilot's central instrument panel, 10 grades of regulation shelves, adjustable 4 grades forward, backward adjustable 6 grades.
The utility model is further arranged to：The service brake mechanism of car is changed by rocking arm, and rocking arm drives left foot, right crus of diaphragm to pass
Moving axis, the service brake for respectively being driven left and right with two axles is in parallel.
By using above-mentioned technical proposal, the service brake mechanism of car is changed by rocking arm, and rocking arm drives left foot, right crus of diaphragm transmission
Axle, the service brake for respectively being driven left and right with two axles is in parallel, the service brake mechanism of car be designed as left and right linkage, it is automatic return, service brake
The strength of reduction torsion spring is adjustable.
The utility model is further arranged to：The motor that the present apparatus is used is for without torque ripple AC servo motor, small turn
Dynamic inertia, ultra-low torque pulsation, small volume, output torque are big, are directly connected with steerable system by monopole planetary gear speed reducing mechanism,
Output high pulling torque.
By using above-mentioned technical proposal, the motor that the present apparatus is used is for without torque ripple AC servo motor, small rotation
Inertia, ultra-low torque pulsation, small volume, output torque are big, are directly connected with steerable system by monopole planetary gear speed reducing mechanism, defeated
Go out high pulling torque, realize direct drive, overcome the rigid clearance produced using various traditional reducing gears, it is ensured that system mechanics
Manipulate smooth.
The utility model is further arranged to：The remote control of the simulator master computer passes through standard industry Ethernet
Bus marco control loads controller.
By using above-mentioned technical proposal, the remote control of the simulator master computer is total by standard industry Ethernet
Line traffic control control loads controller, realizes three real-time controls of passage, and the cycle of operation of control software is controlled in 2KHz/s
More than, power is reached with Bit andits control accurately identical with aircraft actual curve.
Compared with prior art, a kind of new flight control system of the utility model manipulates load device has following beneficial effect
Really：
（1）The utility model control wheel is welded after being processed using digital control processing point two sides using aluminium, polishing, and surface is carried out
Sandblasting, plastic-spraying treatment, install inlet switch, can extend the service life of control wheel.
（2）The pedals that the utility model pedal has the function from returning, driver and copilot can realize linkage.Fly
To suitable actuated position, pedal adjusts stroke 261.6mm to the adjustable pedal of office staff, regulation handle just, the main instrument of copilot
Lower section on dash board, 10 grades of regulation shelves, adjustable 4 grades forward, backward adjustable 6 grades.
（3）The utility model service brake mechanism of car is changed by rocking arm, and rocking arm drives left foot, right crus of diaphragm power transmission shaft, with two axles point
The service brake that left and right is not driven is in parallel, service brake mechanism of car be designed as left and right linkage, it is automatic return, the strength of service brake reduction torsion spring can
Adjust.
（4）The motor that the utility model present apparatus is used is small rotary inertia, ultralow for without torque ripple AC servo motor
Torque ripple, small volume, output torque is big, is directly connected with steerable system by monopole planetary gear speed reducing mechanism, exports high pulling torque,
Direct drive is realized, the rigid clearance produced using various traditional reducing gears is overcome, it is ensured that system mechanics manipulate smooth.
（5）The remote control of the utility model simulator master computer is controlled to manipulate and carried by standard industry industry ethernet
Lotus controller, realizes three real-time controls of passage, and the cycle of operation of control software is controlled in more than 2KHz/s, makes power and position
Shifting control reaches accurately identical with aircraft actual curve.
（6）The utility model simple structure, it is safe and reliable, with good market popularization value.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Fig. 2 is steerable system theory diagram of the present utility model.
Wherein, the corresponding parts title of reference is：
1-main driving device, 2-control wheel, 3-control stick, 4-case lid, 5-longitudinal transmission mechanism, 6-pedal driver
Structure, 7-service brake mechanism of car, 8-transverse transmission mechanism, 9-copilot device, 10-pedal, 11-simulator master computer, 12-
Ethernet interface, 13-trimmer switch, 14-system protector, 15-indicator lamp, 16-servo-control system, 17-oil sources.
Specific embodiment
The utility model is described in further detail with reference to the accompanying drawings and examples, and implementation method of the present utility model includes
But it is not limited to the following example.
Embodiment
To achieve these goals, the technical solution adopted in the utility model is as follows：
The new flight control system manipulates load device, including：Main driving device 1, control wheel 2, control stick 3, case lid 4, longitudinal direction
Transmission mechanism 5, pedal transmission mechanism 6, service brake mechanism of car 7, transverse transmission mechanism 8, copilot device 9, pedal 10, simulator analytic accounting
Calculation machine 11, Ethernet interface 12, trimmer switch 13, system protector 14, indicator lamp 15, servo-control system 16, oil sources 17, this
Device is respectively arranged with main driving device 1 and copilot device 9, and control wheel 2 is connected with control stick 3, and control stick 3 is connected with case lid 4, pin
Pedal 10 both sides for being arranged on case lid 4, the bottom of case lid 4 is provided with pedal transmission mechanism 6, transverse transmission mechanism 8 is by the He of main driving device 1
Copilot device 9 is connected, and pedal transmission mechanism 6 is provided with service brake mechanism of car 7, and longitudinal transmission mechanism 5 is connected with people's electrification machine rocking arm,
Simulator master computer 11 is connected by Ethernet with Ethernet interface 12, and system is provided with trimmer switch 13, system protector
14 and indicator lamp 15, system protector 14 is connected with servo-control system 16, and the mechanical mechanism of device is connected with oil sources 17.
By using above-mentioned technical proposal, the new flight control system manipulates load device, including：Main driving device 1, control wheel
2, control stick 3, case lid 4, longitudinal transmission mechanism 5, pedal transmission mechanism 6, service brake mechanism of car 7, transverse transmission mechanism 8, copilot
Device 9, pedal 10, simulator master computer 11, Ethernet interface 12, trimmer switch 13, system protector 14, indicator lamp 15 is watched
Control system 16, oil sources 17 are taken, the present apparatus is respectively arranged with main driving device 1 and copilot device 9, and control wheel 2 connects with control stick 3
Connect, control wheel 2 is welded after being processed using digital control processing point two sides using aluminium, polishing, surface carries out sandblasting, plastic-spraying treatment, peace
Dress inlet switch, can extend the service life of control wheel 2, and control stick 3 is connected with case lid 4, and pedal 10 is arranged on the two of case lid 4
Side, the bottom of case lid 4 is provided with pedal transmission mechanism 6, and transverse transmission mechanism 8 connects main driving device 1 and copilot device 9, pedal
Transmission mechanism 6 is provided with service brake mechanism of car 7, and service brake mechanism of car 7 is changed by rocking arm, and rocking arm drives left foot, right crus of diaphragm power transmission shaft, is used
The service brake that two axles respectively drive left and right is in parallel, service brake mechanism of car 7 be designed as left and right linkage, it is automatic return, service brake reduction torsion spring
Strength it is adjustable, pedal 10 use aluminium digital control processing, captain, copilot linkage operating mechanism are designed and produced, with people's electrification machine
Rocking arm is connected, and the pedals 10 that pedal 10 has the function from returning, driver and copilot can realize linkage, and pilot is adjustable
Section pedal 10 to suitable actuated position, the regulation stroke 261.6mm of pedal 10, regulation handle just, copilot's central instrument panel
On lower section, 10 grades regulation shelves, adjustable 4 grades forward, adjustable 6 grades backward, longitudinal transmission mechanism 5 is connected with people's electrification machine rocking arm,
Simulator master computer 11 is connected by Ethernet with Ethernet interface 12, and system is provided with trimmer switch 13, system protector
14 and indicator lamp 15, system protector 14 is connected with servo-control system 16, and the mechanical mechanism of device is connected with oil sources 17, this dress
The motor for using is put for without torque ripple AC servo motor, small rotary inertia, ultra-low torque pulsation, small volume, output torque
Greatly, directly connected with steerable system by monopole planetary gear speed reducing mechanism, export high pulling torque, realize direct drive, overcome use
The rigid clearance that various traditional reducing gears are produced, it is ensured that system mechanics manipulate smooth, the distal end of simulator master computer 11
Control controls control loads controller by standard industry industry ethernet, realizes three real-time controls of passage, control software
The cycle of operation control in more than 2KHz/s, power is reached with Bit andits control accurately identical with aircraft actual curve.
The utility model is further arranged to：Control wheel 2 is welded after being processed using digital control processing point two sides using aluminium, beaten
Mill, surface carries out sandblasting, plastic-spraying treatment, installs inlet switch.
By using above-mentioned technical proposal, control wheel 2 divides two sides to be welded after processing, beaten using aluminium using digital control processing
Mill, surface carries out sandblasting, plastic-spraying treatment, installs inlet switch, can extend the service life of control wheel 2.
The utility model is further arranged to：Pedal 10 uses aluminium digital control processing, designs and produces captain, copilot linkage
Operating mechanism, is connected with people's electrification machine rocking arm.
By using above-mentioned technical proposal, pedal 10 uses aluminium digital control processing, designs and produces captain, copilot linkage behaviour
Vertical mechanism, is connected with people's electrification machine rocking arm, and pedal 10 has the function from returning, and the pedals 10 of driver and copilot can be real
Now link, the adjustable pedal 10 of pilot to suitable actuated position, the regulation stroke 261.6mm of pedal 10, regulation handle just,
Lower section on copilot's central instrument panel, 10 grades of regulation shelves, adjustable 4 grades forward, backward adjustable 6 grades.
The utility model is further arranged to：Service brake mechanism of car 7 is changed by rocking arm, and rocking arm drives left foot, right crus of diaphragm transmission
Axle, the service brake for respectively being driven left and right with two axles is in parallel.
By using above-mentioned technical proposal, service brake mechanism of car 7 is changed by rocking arm, and rocking arm drives left foot, right crus of diaphragm power transmission shaft,
The service brake for respectively being driven left and right with two axles is in parallel, service brake mechanism of car 7 be designed as left and right linkage, it is automatic return, service brake resets and turns round
The strength of spring is adjustable.
The utility model is further arranged to：The motor that the present apparatus is used is for without torque ripple AC servo motor, small turn
Dynamic inertia, ultra-low torque pulsation, small volume, output torque are big, are directly connected with steerable system by monopole planetary gear speed reducing mechanism,
Output high pulling torque.
By using above-mentioned technical proposal, the motor that the present apparatus is used is for without torque ripple AC servo motor, small rotation
Inertia, ultra-low torque pulsation, small volume, output torque are big, are directly connected with steerable system by monopole planetary gear speed reducing mechanism, defeated
Go out high pulling torque, realize direct drive, overcome the rigid clearance produced using various traditional reducing gears, it is ensured that system mechanics
Manipulate smooth.
The utility model is further arranged to：The remote control of simulator master computer 11 is total by standard industry Ethernet
Line traffic control control loads controller.
Pass through standard industry industry ethernet by using the remote control of above-mentioned technical proposal, simulator master computer 11
Control control loads controller, realizes three real-time controls of passage, cycle of operation of control software control 2KHz/s with
On, power is reached with Bit andits control accurately identical with aircraft actual curve.
Using technical scheme described in the utility model, or those skilled in the art is in technical solutions of the utility model
Under inspiration, similar technical scheme is designed, and reach above-mentioned technique effect, be to fall into protection model of the present utility model
Enclose.
Claims (6)
1. a kind of new flight control system manipulates load device, it is characterised in that the new flight control system manipulates load device, bag
Include：Main driving device（1）, control wheel（2）, control stick（3）, case lid（4）, longitudinal transmission mechanism（5）, pedal transmission mechanism（6）, pin
Braking mechanism（7）, transverse transmission mechanism（8）, copilot device（9）, pedal（10）, simulator master computer（11）, Ethernet interface
（12）, trimmer switch（13）, system protector（14）, indicator lamp（15）, servo-control system（16）, oil sources（17）, this dress
Put and be respectively arranged with the main driving device（1）With the copilot device（9）, the control wheel（2）With the control stick（3）Even
Connect, the control stick（3）With the case lid（4）Connection, the pedal（10）It is arranged on the case lid（4）Both sides, the case
Lid（4）Bottom is provided with the pedal transmission mechanism（6）, the transverse transmission mechanism（8）By the main driving device（1）With it is described
Copilot device（9）Connection, the pedal transmission mechanism（6）It is provided with the service brake mechanism of car（7）, longitudinal transmission mechanism
（5）It is connected with people's electrification machine rocking arm, the simulator master computer（11）By Ethernet and the Ethernet interface（12）Connection,
System is provided with the trimmer switch（13）, the system protector（14）With the indicator lamp（15）, the system protection
Device（14）With the servo-control system（16）Connection, the mechanical mechanism of device is connected with the oil sources（17）.
2. a kind of new flight control system according to claim 1 manipulates load device, it is characterised in that：The control wheel
（2）Welding, polishing after being processed using digital control processing point two sides using aluminium, surface carry out sandblasting, plastic-spraying treatment, install import and open
Close.
3. a kind of new flight control system according to claim 1 manipulates load device, it is characterised in that：The pedal（10）
Using aluminium digital control processing, captain, copilot linkage operating mechanism are designed and produced, be connected with people's electrification machine rocking arm.
4. a kind of new flight control system according to claim 1 manipulates load device, it is characterised in that：The foot brake machine
Structure（7）Changed by rocking arm, rocking arm drives left foot, right crus of diaphragm power transmission shaft, the service brake for respectively being driven left and right with two axles is in parallel.
5. a kind of new flight control system according to claim 1 manipulates load device, it is characterised in that：What the present apparatus was used
Motor is that, without torque ripple AC servo motor, small rotary inertia, ultra-low torque pulsation, small volume, output torque are big, by list
Pole planetary gear speed reducing mechanism is directly connected with steerable system, exports high pulling torque.
6. a kind of new flight control system according to claim 1 manipulates load device, it is characterised in that：The simulator master
Computer（11）Remote control by standard industry industry ethernet control control loads controller.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621115003.0U CN206210171U (en) | 2016-10-12 | 2016-10-12 | A kind of new flight control system manipulates load device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201621115003.0U CN206210171U (en) | 2016-10-12 | 2016-10-12 | A kind of new flight control system manipulates load device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN206210171U true CN206210171U (en) | 2017-05-31 |
Family
ID=58762165
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201621115003.0U Expired - Fee Related CN206210171U (en) | 2016-10-12 | 2016-10-12 | A kind of new flight control system manipulates load device |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN206210171U (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106652650A (en) * | 2017-02-17 | 2017-05-10 | 吉林大学 | Helicopter control loading simulator having touch guidance |
| 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 |
| CN108182861A (en) * | 2017-12-27 | 2018-06-19 | 天津津航神舟科技有限公司 | A kind of manipulation coupling device for Helicopter Simulator emulation cycle Adjustable length rod |
| CN109147467A (en) * | 2017-08-22 | 2019-01-04 | 南京乐飞航空技术有限公司 | Helicopter control load system and Simulation Methods based on actual load control linkage |
| CN110335518A (en) * | 2019-05-30 | 2019-10-15 | 福建科德电子科技有限公司 | A kind of simulated flight device decelerating manoeuvre device |
| CN114005327A (en) * | 2021-12-30 | 2022-02-01 | 江苏普旭科技股份有限公司 | Human sensing system for driving simulator |
-
2016
- 2016-10-12 CN CN201621115003.0U patent/CN206210171U/en not_active Expired - Fee Related
Cited By (10)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106652650A (en) * | 2017-02-17 | 2017-05-10 | 吉林大学 | Helicopter control loading simulator having touch guidance |
| CN106652650B (en) * | 2017-02-17 | 2018-05-15 | 吉林大学 | A kind of helicopter control load simulation device with tactile guiding |
| 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 |
| CN109147467A (en) * | 2017-08-22 | 2019-01-04 | 南京乐飞航空技术有限公司 | Helicopter control load system and Simulation Methods based on actual load control linkage |
| CN109147467B (en) * | 2017-08-22 | 2021-05-04 | 南京乐飞航空技术有限公司 | Helicopter control load system based on actual-mounted control lever system and simulation implementation method |
| CN108182861A (en) * | 2017-12-27 | 2018-06-19 | 天津津航神舟科技有限公司 | A kind of manipulation coupling device for Helicopter Simulator emulation cycle Adjustable length rod |
| CN108182861B (en) * | 2017-12-27 | 2023-10-31 | 天津华翼蓝天科技股份有限公司 | Control coupling device for simulation period variable-pitch rod of helicopter simulator |
| CN110335518A (en) * | 2019-05-30 | 2019-10-15 | 福建科德电子科技有限公司 | A kind of simulated flight device decelerating manoeuvre device |
| CN114005327A (en) * | 2021-12-30 | 2022-02-01 | 江苏普旭科技股份有限公司 | Human sensing system for driving simulator |
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| GR01 | Patent grant | ||
| 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: 20170531 Termination date: 20201012 |