CN204791639U - Aircraft is driven power of manipulation and is felt analogue means - Google Patents
Aircraft is driven power of manipulation and is felt analogue means Download PDFInfo
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- CN204791639U CN204791639U CN201520426052.5U CN201520426052U CN204791639U CN 204791639 U CN204791639 U CN 204791639U CN 201520426052 U CN201520426052 U CN 201520426052U CN 204791639 U CN204791639 U CN 204791639U
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- pedal
- load
- aircraft
- jociey stick
- analogue means
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Abstract
The utility model provides an aircraft is driven power of manipulation and is felt analogue means, the device comprises control stick mechanism, pedal mechanism, drive mechanism, controller and two sets of load devices, control stick mechanism, pedal mechanism, drive mechanism install on the base, one of them cover load device via drive mechanism hookup control stick mechanism, and another hookup pedal mechanism of cover load mechanism, control stick mechanism, pedal mechanism and two sets of load devices pass through sensor connection director. The device is applicable to the aircraft driver and trains in earlier stage.
Description
Technical field
The utility model relates to pilot control power sense analogue means, particularly relates to a kind of advaced trainer ground service and safeguards riding manipulation power sense analogue means in analog training device.
Background technology
Advaced trainer structure is very complicated, each professional height intersection, and aircraft maintenance, testing mode and maintenance means etc. are all different from conventional types, add that advaced trainer is expensive, is equipped with negligible amounts.If adopt the teaching means of actual load, owing to requiring restriction by place, personnel, equipment guarantee and airplane equipment security etc., add a lot of subject and do not allow repetition training on actual load aircraft, even some subjects do not allow to carry out aboard yet, cause training usefulness very low, simulated training then avoids the generation of various unsafe factor.Steering force sense analogue means is one of ground service key subsystem safeguarding simulator, the basis that the steering force induction device that development has a high fidelity is development high fidelity, simulator is safeguarded in high level ground service.
Summary of the invention
The purpose of this utility model is to provide a kind of high fidelity, high level aircraft handling steering force sense analogue means, for aviator's training in early stage.
The utility model adopts following technical proposals to realize, a kind of aircraft handling steering force sense analogue means, and this device is made up of jociey stick mechanism, pedal mechanism, gear train, controller and two cover load devices; Jociey stick mechanism, pedal mechanism, gear train are arranged on pedestal, wherein a set of load device connects jociey stick mechanism via gear train, another set of load mechanism connects pedal mechanism, and jociey stick mechanism, pedal mechanism and two cover load devices are by sensor connection control device.
The built-in analogue simulation program of controller, and be provided with instrument and display screen to show every drive parameter.
Jociey stick mechanism refers generally to the direct operated mechanism of human pilot, comprises compositions such as driving club head, bearing seat, axle bed, upper connecting rod.
Pedal mechanism mainly comprises: the compositions such as left and right pedal, pedal shaft, main shaft, lower connecting rocker arm.
Gear train mainly comprises intermediate connecting rod, support bar, bracing frame, long connecting rod, short connecting rod etc.
Load device mainly comprises servomotor and servo-driver.Load device is to provide the mechanism of power sense, for operator provides reacting force in jociey stick and pedal operating process, and adjusts the size of reacting force in real time according to the motion state of operation, thus the power sense of Reality simulation aircraft handling.This load device adopts servo-controlled mode, and by driven by servomotor jociey stick mechanism and pedal mechanism, and the analogue simulation program in controller is combined, and realizes the power sense true to nature of riding manipulation mechanism.
Accompanying drawing explanation
Fig. 1 structural representation of the present utility model.
In the drawings: 1. jociey stick mechanism; 2. gear train; 3. pedestal; 4. servomotor; 5. pedal mechanism; 6. controller.
Embodiment
As shown in Figure 1, a kind of aircraft handling steering force sense analogue means, this device is made up of jociey stick mechanism 1, pedal mechanism 5, gear train 2, controller 6 and two cover load devices; Load device mainly comprises servomotor 4 and servo-driver, jociey stick mechanism 1, pedal mechanism 5, gear train 2 are arranged on pedestal, wherein a set of load device connects jociey stick mechanism 1 via gear train 2, another set of load mechanism connects pedal mechanism 5, and jociey stick mechanism 1, pedal mechanism 5 and two cover load devices are by sensor connection control device 6.The built-in analogue simulation program of controller 6, and be provided with instrument and display screen to show every drive parameter.
Jociey stick mechanism 1 refers to the direct operated mechanism of human pilot, comprises compositions such as driving club head, bearing seat, axle bed, upper connecting rod.
Pedal mechanism mainly comprises: the compositions such as left and right pedal, pedal shaft, main shaft, lower connecting rocker arm.
Gear train mainly comprises intermediate connecting rod, support bar, bracing frame, long connecting rod, short connecting rod etc.
After this device powers up, start the neutral position of locating jociey stick and pedal, jociey stick and pedal be all encounter mechanical stop spacing after return neutral point, can not there be any obstruction period.After having located, load device can send position and the power sense size of current jociey stick and pedal to host computer, meanwhile, host computer also can arrange power inductance value to load device, and this load device has trim function.
Claims (1)
1. an aircraft handling steering force sense analogue means, is characterized in that, this device is made up of jociey stick mechanism, pedal mechanism, gear train, controller and two cover load devices; Jociey stick mechanism, pedal mechanism, gear train are arranged on pedestal, wherein a set of load device connects jociey stick mechanism via gear train, another set of load mechanism connects pedal mechanism, and jociey stick mechanism, pedal mechanism and two cover load devices are by sensor connection control device.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520426052.5U CN204791639U (en) | 2015-06-19 | 2015-06-19 | Aircraft is driven power of manipulation and is felt analogue means |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201520426052.5U CN204791639U (en) | 2015-06-19 | 2015-06-19 | Aircraft is driven power of manipulation and is felt analogue means |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN204791639U true CN204791639U (en) | 2015-11-18 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201520426052.5U Active CN204791639U (en) | 2015-06-19 | 2015-06-19 | Aircraft is driven power of manipulation and is felt analogue means |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN204791639U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106768582A (en) * | 2016-11-30 | 2017-05-31 | 江西洪都航空工业集团有限责任公司 | A kind of tandem cockpit pilot manipulates force measuring 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 |
-
2015
- 2015-06-19 CN CN201520426052.5U patent/CN204791639U/en active Active
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106768582A (en) * | 2016-11-30 | 2017-05-31 | 江西洪都航空工业集团有限责任公司 | A kind of tandem cockpit pilot manipulates force measuring device |
| CN106768582B (en) * | 2016-11-30 | 2019-08-16 | 江西洪都航空工业集团有限责任公司 | A kind of tandem cockpit pilot manipulation force measuring 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 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant |