CN110310543A - A kind of simulated flight device flap runners - Google Patents
A kind of simulated flight device flap runners Download PDFInfo
- Publication number
- CN110310543A CN110310543A CN201910462148.XA CN201910462148A CN110310543A CN 110310543 A CN110310543 A CN 110310543A CN 201910462148 A CN201910462148 A CN 201910462148A CN 110310543 A CN110310543 A CN 110310543A
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- Prior art keywords
- shaft
- outer shaft
- flight device
- simulated flight
- switch block
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- 238000013016 damping Methods 0.000 claims description 4
- 230000005611 electricity Effects 0.000 claims 1
- 238000012549 training Methods 0.000 abstract description 4
- 238000004088 simulation Methods 0.000 description 3
- NIXOWILDQLNWCW-UHFFFAOYSA-N acrylic acid group Chemical group C(C=C)(=O)O NIXOWILDQLNWCW-UHFFFAOYSA-N 0.000 description 2
- 238000013461 design Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 238000000034 method Methods 0.000 description 2
- 238000012986 modification Methods 0.000 description 2
- 230000004048 modification Effects 0.000 description 2
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000000354 decomposition reaction Methods 0.000 description 1
- 230000007812 deficiency Effects 0.000 description 1
- 238000005457 optimization Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 238000012360 testing method Methods 0.000 description 1
- 230000017105 transposition Effects 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)
- Toys (AREA)
Abstract
The invention discloses a kind of simulated flight device flap runners, including bracket, upper cover and lower cover, switch block and shaft, guide rod and resetting-mechanism, wherein, the lower cover drives the outer shaft in the inner shaft when upward sliding, the guide rod is detached from the limiting groove of the guide groove, the outer shaft drives the switch block and shaft to rotate that the potentiometer is driven to rotate when rotating, the rotational angle information of the potentiometer is sent to the background server of flight simulator.The present invention uses full mechanical movement, is used in various places, is hardly damaged；In its flap control for being used in simulated flight device, flight training cost is reduced.
Description
Technical field
The present invention relates to simulated flight device flap runners, more particularly to being used to control on a kind of synthetic flight training device
The device of aircraft flap processed.
Background technique
It is known that aircraft, which flies up into the sky, needs enough lift.It increases wing area or flying speed improves, it can
Increase lift.But aircraft is during take-off and landing, in order to shorten landing distance and guarantee landing safety, cannot generally improve speed, and
Increasing wing area then will increase aircraft weight, consume big energy.Therefore, in order to both increase aircraft in low-speed stages such as landings
Lift, and reach load-carrying, speed, resistance and oil consumption etc. comprehensive optimization, wing flap come into being.Can wing flap why
It can increase lift? wing flap can change camber, increase wing area, keep Laminar Flow, and according to theory, this is in speed
In the case where certain, the lift of low-speed stage can be greatly increased.Wing flap is generally used in modern aircraft, and different winged
Machine will select the combination of different wing flaps or several wing flaps according to oneself requirement.Small-sized warplane is more using trailing edge flap, large-scale
Aircraft then uses the combination of leading edge and trailing edge flap, and often more slats simultaneously.Being designed and arranged for wing flap is also very fastidious,
It just can determine that by a large amount of wind tunnel test.However, flying cadet is dynamic by simulation softward progress aircraft floor wing flap etc.
When the simulated training of work, due to there is no simulation operation apparatus, need to simulate the ground flap of aircraft by mouse or keyboard operation
The wing can not experience operating handle when actual airplane operation wing flap.Therefore, in order to improve the authenticity of flight simulation, one is needed
Kind can simulate the operating device of actual airplane wing flap.
Summary of the invention
It is an object of the invention to overcome the deficiency of the prior art, provides a kind of simulated flight device flap runners.
The technical solution adopted by the present invention to solve the technical problems is:
A kind of simulated flight device flap runners, it is characterised in that: comprising:
Bracket, the bracket are equipped with guide groove, and the upper wall of the guide groove is arc, and it is recessed that lower wall is equipped with multiple limits
Slot,
Upper cover and lower cover, the upper cover connect inner shaft, and the lower cover connects outer shaft, and the outer shaft and lower cover are slidably socketed
Outside the inner shaft；
Switch block and shaft, the switch block are slidably socketed in outside the outer shaft, run through slot of the outer shaft equipped with radial direction, and described turn
Axis passes through being rotatably connected on the bracket after slot by damping bearing for the switch block and outer shaft, the shaft
One end is drivingly connected potentiometer；
Guide rod, the centre of the guide rod are connected on the outer shaft, and the guide rod is threaded through leading for the bracket
Into slot；And
Resetting-mechanism, the resetting-mechanism are mounted between the outer shaft and the switch block；
Wherein, the lower cover drives the outer shaft in the inner shaft when upward sliding, leads described in the guide rod disengaging
To the limiting groove of slot, the outer shaft drives the switch block and shaft to rotate that the potentiometer is driven to rotate when rotating, institute
The rotational angle information for stating potentiometer is sent to the background server of flight simulator.
In a further preferred embodiment, the inner shaft runs through slot equipped with radial, and slide bar is covered under described, described
Litter can slide in slot described.
In a further preferred embodiment, the resetting-mechanism is tension spring, is respectively equipped with confession on the outer shaft and the switch block
The screw of the both ends mounting of the tension spring.
In a further preferred embodiment, the both ends of the shaft pass through bearing respectively and are rotatably connected to the bracket
On.
In a further preferred embodiment, the bracket includes that left fixed plate, right fixed plate and the left fixed plate of connection and the right side are solid
The securing plate of fixed board, there are two the guide grooves, and two guide grooves are symmetrically arranged at the left fixed plate and right fixed plate
On.
In a further preferred embodiment, the shaft drive connection first gear, first gear engagement second gear, second
Gear is fixedly and coaxially connected the potentiometer.
It in a further preferred embodiment, further include indicator board, the indicator board is equipped with rotation recessing groove and mark.
The beneficial effects of the present invention are:
Simulated flight device flap runners of the present invention by being pulled upwardly wing flap lower cover then power forward or backward,
Band moving gear rotation is converted to signal by potentiometer transposition and simulated flight device wing flap is made to do rise and descending motion, passes through drawing
The active force of spring makes wing flap operating device return to design position in the effect for not having stress.The present invention uses full mechanical movement,
Various places are used in, are hardly damaged；In its flap control for being used in simulated flight device, flight training cost is reduced.
Invention is further described in detail with reference to the accompanying drawings and embodiments；But a kind of simulated flight device of the invention
Flap runners are not limited to the embodiment.
Detailed description of the invention
Fig. 1 is the decomposition texture schematic diagram of a preferred embodiment of the invention.
Fig. 2 is the mounting structure side schematic view of a preferred embodiment of the invention.
Fig. 3 is the mounting structure schematic diagram of a preferred embodiment of the invention.
Specific embodiment
Embodiment, referring to shown in Fig. 1 to Fig. 3, a kind of simulated flight device flap runners of the invention include upper cover 1,
Inner shaft 2, lower cover 3, outer shaft 4, acrylic laser carving version 5, nut 6, screw 7, right fixed plate 8, first gear 9, potentiometer 10, current potential
Device bracket 11, guide rod 12, second gear 13, damping bearing 14, shaft 15, securing plate 16, switch block 17, soket head cap screw 18,
Tension spring 19 and right fixed plate 20.
The upper cover 1 connects the inner shaft 2, and the lower cover 3 connects the outer shaft 4, and the lower cover 3 and outer shaft 4 are socketed in
Outside the inner shaft 2.The acrylic laser carving version 5 is equipped with rotation recessing groove 51 and sign, and the outer shaft passes through described turn
Dynamic recessing groove 51, the switch block 17 are slidably socketed on the outer shaft 4, and the outer shaft 4 runs through sliding slot 41 equipped with radial,
Shaft 15 passes through the switch block 17 and described its both ends after the sliding slot 41 pass through damping bearing 14 respectively and are rotatably connected to
In the left fixed plate 8 and right fixed plate 20.One end of the shaft drives first gear 9, the engagement of first gear 9 second
Gear 13, the second gear 13 are fixedly and coaxially connected the potentiometer 10, and the potentiometer 10 is mounted on potentiometer support 11
On.
The centre of the guide rod 12 is fixedly connected with the end of the outer shaft 4, in the left fixed plate 8 and right fixed plate 20
It is respectively equipped with symmetrical guide groove 81 and 201, the upper wall of the guide groove 81 (201) is arc, and it is recessed that lower wall is equipped with multiple limits
Slot, the both ends of the guide rod 12 can be slided in the guide groove respectively.
The both sides of the switch block 17 are respectively equipped with soket head cap screw 18, and the top of the outer shaft is respectively equipped with screw 7 and spiral shell
Mother 6, the tension spring is articulated between the soket head cap screw 18 and the screw 7.
The operating process of the present embodiment is as follows: wing flap lower cover 3 being pulled upwardly, guide rod 12 is detached from the limitation of limiting groove
And can be slided in guide groove, intermediate switch block 17 rotates, and shaft 15 drives first gear 9 to rotate, and first gear 9 drives the second tooth
13 rotation of wheel, so that potentiometer 10 be driven to rotate, rotational angle information is sent to background server by potentiometer 10, platform after listening
Server converts a signal into simulated flight device wing flap, so that simulated flight device be made to realize that wing flap does the function of rise and descending motion
Energy.Wing flap operating device is made to return to design position in the effect for not having stress by the active force of tension spring.
Above-described embodiment is only used to further illustrate a kind of simulated flight device flap runners of the invention, but the present invention
It is not limited to embodiment, according to the technical essence of the invention any simple modification to the above embodiments, equivalent
Variation and modification, fall within the scope of protection of technical solution of the present invention.
Claims (7)
1. a kind of simulated flight device flap runners, it is characterised in that: comprising:
Bracket, the bracket are equipped with guide groove, and the upper wall of the guide groove is arc, and lower wall is equipped with multiple limiting grooves,
Upper cover and lower cover, the upper cover connect inner shaft, and the lower cover connects outer shaft, and the outer shaft and lower cover are slidably socketed in institute
It states outside inner shaft；
Switch block and shaft, the switch block are slidably socketed in outside the outer shaft, and outer shaft runs through slot equipped with radial, and the shaft is worn
Cross being rotatably connected on the bracket after slot by damping bearing for the switch block and outer shaft, one end of the shaft
It is drivingly connected potentiometer；
Guide rod, the centre of the guide rod are connected on the outer shaft, and the guide rod is threaded through the guide groove of the bracket
It is interior；And
Resetting-mechanism, the resetting-mechanism are mounted between the outer shaft and the switch block；
Wherein, the lower cover drives the outer shaft in the inner shaft when upward sliding, and the guide rod is detached from the guide groove
Limiting groove, the outer shaft drives the switch block and shaft to rotate that the potentiometer is driven to rotate when rotating, the electricity
The rotational angle information of position device is sent to the background server of flight simulator.
2. a kind of simulated flight device flap runners according to claim 1, it is characterised in that: the inner shaft is equipped with
Radial runs through slot, and slide bar is covered under described, and the litter can slide in slot described.
3. a kind of simulated flight device flap runners according to claim 1, it is characterised in that: the resetting-mechanism is
The screw mounted for the both ends of the tension spring is respectively equipped on tension spring, the outer shaft and the switch block.
4. a kind of simulated flight device flap runners according to claim 1, it is characterised in that: the both ends of the shaft
It is rotatably connected on the bracket by bearing respectively.
5. a kind of simulated flight device flap runners according to claim 1, it is characterised in that: the bracket includes a left side
The securing plate of fixed plate, right fixed plate and connection left fixed plate and right fixed plate, there are two the guide grooves, two guide grooves point
It is not symmetricly set in the left fixed plate and right fixed plate.
6. a kind of simulated flight device flap runners according to claim 1, it is characterised in that: the shaft driving connects
First gear is connect, first gear engages second gear, and second gear is fixedly and coaxially connected the potentiometer.
7. a kind of simulated flight device flap runners according to claim 1, it is characterised in that: it further include indicator board,
The indicator board is equipped with rotation recessing groove and mark.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910462148.XA CN110310543A (en) | 2019-05-30 | 2019-05-30 | A kind of simulated flight device flap runners |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910462148.XA CN110310543A (en) | 2019-05-30 | 2019-05-30 | A kind of simulated flight device flap runners |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN110310543A true CN110310543A (en) | 2019-10-08 |
Family
ID=68074947
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201910462148.XA Pending CN110310543A (en) | 2019-05-30 | 2019-05-30 | A kind of simulated flight device flap runners |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN110310543A (en) |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070164153A1 (en) * | 2006-01-18 | 2007-07-19 | Groomes Kim C | Flap simulators |
| CN102095577A (en) * | 2011-01-05 | 2011-06-15 | 哈尔滨飞机工业集团有限责任公司 | Load control method for aircraft flap experiment |
| CN102157089A (en) * | 2011-04-01 | 2011-08-17 | 天津中天翔翼航空科技有限公司 | Simulation device for steering wheel of airplane flight simulator |
| CN102262099A (en) * | 2011-04-15 | 2011-11-30 | 北京航空航天大学 | 1400-DEG C high-temperature thermal-mechanical coupling test device for aerofoil structure of hypersonic vehicle |
| CN102642624A (en) * | 2012-05-11 | 2012-08-22 | 中国航空工业集团公司西安飞机设计研究所 | Load simulator of plane booster dummy assembly |
| CN107993514A (en) * | 2018-01-16 | 2018-05-04 | 镇江爱维森仿真科技有限公司 | The dedicated emulated parking control mechanism of Aircraft Simulator |
| CN108053718A (en) * | 2018-02-02 | 2018-05-18 | 安徽英釜航空科技有限公司 | A kind of simulation aircraft wide-angle turning control device |
| CN210015559U (en) * | 2019-05-30 | 2020-02-04 | 福建科德电子科技有限公司 | Flap control device for simulated aircraft |
-
2019
- 2019-05-30 CN CN201910462148.XA patent/CN110310543A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US20070164153A1 (en) * | 2006-01-18 | 2007-07-19 | Groomes Kim C | Flap simulators |
| CN102095577A (en) * | 2011-01-05 | 2011-06-15 | 哈尔滨飞机工业集团有限责任公司 | Load control method for aircraft flap experiment |
| CN102157089A (en) * | 2011-04-01 | 2011-08-17 | 天津中天翔翼航空科技有限公司 | Simulation device for steering wheel of airplane flight simulator |
| CN102262099A (en) * | 2011-04-15 | 2011-11-30 | 北京航空航天大学 | 1400-DEG C high-temperature thermal-mechanical coupling test device for aerofoil structure of hypersonic vehicle |
| CN102642624A (en) * | 2012-05-11 | 2012-08-22 | 中国航空工业集团公司西安飞机设计研究所 | Load simulator of plane booster dummy assembly |
| CN107993514A (en) * | 2018-01-16 | 2018-05-04 | 镇江爱维森仿真科技有限公司 | The dedicated emulated parking control mechanism of Aircraft Simulator |
| CN108053718A (en) * | 2018-02-02 | 2018-05-18 | 安徽英釜航空科技有限公司 | A kind of simulation aircraft wide-angle turning control device |
| CN210015559U (en) * | 2019-05-30 | 2020-02-04 | 福建科德电子科技有限公司 | Flap control device for simulated aircraft |
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