CN109911180A - A kind of light aerocraft flap runners - Google Patents
A kind of light aerocraft flap runners Download PDFInfo
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- CN109911180A CN109911180A CN201910297589.9A CN201910297589A CN109911180A CN 109911180 A CN109911180 A CN 109911180A CN 201910297589 A CN201910297589 A CN 201910297589A CN 109911180 A CN109911180 A CN 109911180A
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- rocker arm
- flap
- wing flap
- shaped rocker
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- 230000007246 mechanism Effects 0.000 claims abstract description 26
- 230000033001 locomotion Effects 0.000 claims description 14
- 230000008713 feedback mechanism Effects 0.000 claims description 10
- 230000005611 electricity Effects 0.000 claims description 3
- 239000007787 solid Substances 0.000 claims description 2
- 238000009434 installation Methods 0.000 claims 1
- 238000012423 maintenance Methods 0.000 abstract description 6
- 230000001360 synchronised effect Effects 0.000 abstract description 4
- 229910000831 Steel Inorganic materials 0.000 description 6
- 239000010959 steel Substances 0.000 description 6
- 238000010586 diagram Methods 0.000 description 4
- 238000000034 method Methods 0.000 description 3
- 230000000630 rising effect Effects 0.000 description 2
- FGRBYDKOBBBPOI-UHFFFAOYSA-N 10,10-dioxo-2-[4-(N-phenylanilino)phenyl]thioxanthen-9-one Chemical compound O=C1c2ccccc2S(=O)(=O)c2ccc(cc12)-c1ccc(cc1)N(c1ccccc1)c1ccccc1 FGRBYDKOBBBPOI-UHFFFAOYSA-N 0.000 description 1
- 235000006508 Nelumbo nucifera Nutrition 0.000 description 1
- 240000002853 Nelumbo nucifera Species 0.000 description 1
- 235000006510 Nelumbo pentapetala Nutrition 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
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- 230000007423 decrease Effects 0.000 description 1
- 230000009347 mechanical transmission Effects 0.000 description 1
- 230000000116 mitigating effect Effects 0.000 description 1
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- Power-Operated Mechanisms For Wings (AREA)
Abstract
The invention discloses a kind of light aerocraft flap runners, wing flap driving mechanism includes motor, and the output shaft of motor is fixedly connected with worm screw, is screwed on the outside of worm screw and is combined with worm screw beam barrel, worm screw beam barrel end is hinged with triangle part, and triangle part one end is fixedly connected with first rotating shaft；The wing flap linkage mechanism includes the first pull rod and the second pull rod, first pull rod and the second pull rod are hingedly arranged with two wing flap rotational positions respectively, first pull rod upper end and triangle part one end are hinged, the first fan-shaped rocker arm is fixedly installed in the first rotating shaft, second pull rod upper end is hinged with link block, the link block lower end is fixedly mounted in the second shaft, it is fixedly installed with the second fan-shaped rocker arm in second shaft, is attached by two to guiding cable wire between the described first fan-shaped rocker arm and the second fan-shaped rocker arm.The present apparatus can preferably mitigate aircraft power supply load, realize the synchronous rotation of wing flap, while reduce its failure rate, facilitate maintenance.
Description
Technical field
The present invention relates to General Aviation technical fields, and in particular to a kind of light aerocraft flap runners.
Background technique
Electric control system in the existing system of flaps generally comprises two independent electric motors, this makes the negative of aircraft power supply
Lotus increases, and power driven system drives principle when mechanical transmission mechanism rotation excessively complicated, and above two aspect can make the flap
Wing system failure rate increases, and has not only been able to achieve its function but also energy to guarantee that aircraft safety need to invent a kind of easy flap runners
Reduce its failure rate.
Summary of the invention
In view of the above shortcomings of the prior art, the technical problems to be solved by the present invention are: how one kind is provided can be more
Good mitigation aircraft power supply load, realizes the synchronous rotation of wing flap, while reducing its failure rate, facilitates the light aerocraft flap of maintenance
Wing manipulation device.
In order to solve the above-mentioned technical problem, present invention employs the following technical solutions:
A kind of light aerocraft flap runners, including flap control handle mechanism, wing flap driving mechanism, wing flap gear
Structure and feedback mechanism, the wing flap driving mechanism includes motor, and the output shaft of the motor is fixedly connected with worm screw, described
It is screwed on the outside of worm screw and is combined with worm screw beam barrel, worm screw beam barrel end is hinged with triangle part, and triangle part one end is fixedly connected with
First rotating shaft；The wing flap linkage mechanism includes the first pull rod and the second pull rod, first pull rod and the second pull rod respectively with
Two wing flap rotational positions are hingedly arranged, and first pull rod upper end and triangle part one end are hinged, solid in the first rotating shaft
Equipped with the first fan-shaped rocker arm, second pull rod upper end is hinged with link block for Dingan County, and the link block lower end is fixedly mounted on the
In two shafts, the second fan-shaped rocker arm, the described first fan-shaped rocker arm and the second fan-shaped rocker arm are fixedly installed in second shaft
Between by two to guiding cable wire be attached.
In the technical program, flap control handle mechanism is used to control the connecting and disconnecting of motor, when motor is connected,
Motor drives worm screw rotation, and worm screw drives worm screw beam barrel to move along worm axis direction, and worm screw beam barrel drives triangle part around the
The rotation of one shaft, triangle part drive the first pull rod to move up during rotation, and the drive wing flap rotation of the first pull rod is simultaneously upward
It is mobile；The first fan-shaped rocker arm rotation is driven when first rotating shaft rotates, the first fan-shaped rocker arm and the second fan-shaped rocker arm pass through guiding steel
Rope connection setting, the first fan-shaped rocker arm rotation of fan-shaped rocker arm drive second, the second fan-shaped rocker arm drive the second shaft to rotate, and second
Shaft drives link block rotation, and link block drives the rotation of the second pull rod, and the second pull rod drives wing flap to rotate and move up.Feedback
Mechanism is used to give the motion feedback of wing flap to flap control handle mechanism, disconnects for controlling motor, wing flap stopping movement.This
Device can preferably mitigate aircraft power supply load, realize the synchronous rotation of wing flap, while reduce its failure rate, facilitate maintenance.
Upper and lower put of the receipts of wing flap is realize the positive and negative rotation of motor by changing the current direction of motor to realize.
Further, the open end of the described first fan-shaped rocker arm and the second fan-shaped rocker arm is disposed opposite to each other, and described first is fan-shaped
The open end of rocker arm and the second fan-shaped rocker arm, which respectively corresponds, is provided with connecting hole and lower connecting hole, wherein a guiding cable wire two
End is fixedly connected with the lower connecting hole of the upper connecting hole of the described first fan-shaped rocker arm and the second fan-shaped rocker arm respectively, is in addition led for one
It is fixedly connected respectively with the upper connecting hole of the lower connecting hole of the described first fan-shaped rocker arm and the second fan-shaped rocker arm to the both ends of cable wire,
It links for realizing two wing flaps.
In this way, drive two guiding cable wires to move in the opposite direction respectively when the first fan-shaped rocker arm rotates clockwise, into
And drive the second fan-shaped rocker arm to rotate clockwise by guiding cable wire, it is arranged on the first fan-shaped rocker arm and the second fan-shaped rocker arm upper
Connecting hole and lower connecting hole are disposed opposite to each other, and the first fan-shaped rocker arm and the second fan-shaped rocker arm can be made in rotation, drive first
Pull rod and the second pull rod do rising or descending motion simultaneously, and then wing flap is driven to rotate synchronously.Structure is simple, facilitates maintenance.
Further, trunnion, fixed company between the rotation trunnion upper end are rotated there are two being fixedly mounted on the wing flap
It is connected to connecting rod, first pull rod and the second pull rod lower end are provided with lantern ring and are socketed on the connecting rod, turn described in two
The distance between dynamic trunnion is greater than the width of lantern ring.
In this way, the distance between two trunnions are greater than the width of lantern ring, the first pull rod and the second pull rod can be preferably given
A space moved horizontally in uphill process can preferably guarantee its motion credibility.
Further, the sector of the described first fan-shaped rocker arm and the second fan-shaped rocker arm is circumferential is recessed for guiding steel
The guide groove of Suo Jinhang guiding.
In this way, guide groove can preferably be oriented to guiding cable wire, structure is simple, can preferably improve guiding steel
The motion credibility of rope.
Further, it is additionally provided between the described first fan-shaped rocker arm and the second fan-shaped rocker arm for being carried out to guiding cable wire
The directive wheel of guiding.
In this way, can preferably be oriented to guiding cable wire, structure is simple, can preferably improve the fortune of guiding cable wire
Dynamic reliability.
Further, the wing flap driving mechanism include wing flap Handleset, be fixedly connected with wing flap Handleset it is convex
The micro-switch of the cam side is taken turns and is arranged in, the micro-switch is fixedly mounted on wing flap micro-switch bracket,
The micro-switch connect setting by wing flap control circuit with the motor.
In this way, band moving cam rotates when wing flap Handleset rotates, the fine motion electricity on cam and wing flap micro-switch bracket
Door release, so that wing flap control circuit is connected, motor action.Micro-switch can preferably detect the rotation of cam, make
With convenient, high reliablity.
Further, the feedback mechanism includes the feedback wire rope being fixedly connected with wing flap micro-switch bracket, described anti-
It presents the cable wire other end and connect setting with wing flap linkage mechanism.
In this way, feedback mechanism drives wing flap micro-switch carriage turns, wing flap micro-switch bracket drives micro-switch to turn
Dynamic, so that cam is contacted with micro-switch, wing flap control circuit is disconnected, and electric motor circuit breaking, wing flap stops rotating.
Further, the wing flap Handleset includes handle and handle mount, is provided on the handle mount
Sliding slot, the handle outer end are located on the outside of the handle mount, and the handle inner end passes through the sliding slot and the cam one
End is fixedly connected, and the wing flap micro-switch carriage turns are mounted in the handle mount.
In this way, being provided with handle mount, preferably handle, cam and wing flap micro-switch bracket can be pacified
Dress is easy to use.
Further, stop block is provided on the handle mount, be provided on the handle mount indicator light and
Dial.
In this way, being provided with indicator light, wing flap current location can be preferably shown.It is provided with dial, it can also be more preferable
Display wing flap current location, meanwhile, preferably handle can be revolved to giving intuitively to observe in rotational handle
Turn, to adjust the position of wing flap.It is provided with stop block, preferably can carry out locking in the position to handle.Feedback wire rope, instruction
Lamp and micro-switch collectively form wing flap instruction system, can preferably learn the current location of wing flap, wing flap is being received
When above and putting down, indicator light and wing flap synchronization action are easy to use.
Further, the stop block is in steps setting.
In this way, locking preferably can be carried out to the wing flap in different location, it is easy to use.
Detailed description of the invention
Fig. 1 is the overall structure diagram of light aerocraft flap runners described in the specific embodiment of the invention.
Fig. 2 is the partial enlargement diagram in Fig. 1 at A.
Fig. 3 is the schematic perspective view of Fig. 2.
Fig. 4 is the partial enlargement diagram in Fig. 1 at B.
Fig. 5 is the schematic perspective view of Fig. 4.
Fig. 6 is the partial enlargement diagram in Fig. 1 at C.
Fig. 7 is the schematic perspective view of Fig. 6.
In attached drawing, 1, motor, 11, worm screw, 12, worm screw beam barrel, 13, first rotating shaft, 14, triangle part, the 2, first pull rod,
3, the second pull rod, 31, link block, the 32, second shaft, 4, wing flap, the 5, first fan-shaped rocker arm, 51, upper connecting hole, 52, lower connection
Hole, 53, directive wheel, the 6, second fan-shaped rocker arm, 7, guiding cable wire, 8, trunnion, 81, connecting rod, 9, cam, 91, micro-switch, 92,
Wing flap micro-switch bracket, 93, feedback wire rope, 94, handle, 95, handle mount, 96, stop block, 97, indicator light.
Specific embodiment
The 1-7 present invention is described in further detail with reference to the accompanying drawing.
A kind of light aerocraft flap runners, including flap control handle mechanism, wing flap driving mechanism, wing flap gear
Structure and feedback mechanism, the wing flap driving mechanism include motor 1, and the output shaft of the motor 1 is fixedly connected with worm screw 11,
It is screwed on the outside of the worm screw 11 and is combined with worm screw beam barrel 12,12 end of worm screw beam barrel is hinged with triangle part 14, triangle part 14
One end is fixedly connected with first rotating shaft 13；The wing flap linkage mechanism includes the first pull rod 2 and the second pull rod 3, and described first draws
Bar 2 and the second pull rod 3 are hingedly arranged with two 4 rotational positions of wing flap respectively, 2 upper end of the first pull rod and triangle part 12 1
End is hinged, the first fan-shaped Rocker arm 5 is fixedly installed in the first rotating shaft 13,3 upper end of the second pull rod is hinged with link block
31,31 lower end of link block is fixedly mounted in the second shaft 32, and the second sector is fixedly installed in second shaft 32
Rocker arm 6 is attached by two to guiding cable wire 7 between described first fan-shaped Rocker arm 5 and the second fan-shaped rocker arm 6.
In the technical program, flap control handle mechanism is used to control the connecting and disconnecting of motor, when motor is connected,
Motor drives worm screw rotation, and worm screw drives worm screw beam barrel to move along worm axis direction, and worm screw beam barrel drives triangle part around the
The rotation of one shaft, triangle part drive the first pull rod to move up during rotation, and the drive wing flap rotation of the first pull rod is simultaneously upward
It is mobile；The first fan-shaped rocker arm rotation is driven when first rotating shaft rotates, the first fan-shaped rocker arm and the second fan-shaped rocker arm pass through guiding steel
Rope connection setting, the first fan-shaped rocker arm rotation of fan-shaped rocker arm drive second, the second fan-shaped rocker arm drive the second shaft to rotate, and second
Shaft drives link block rotation, and link block drives the rotation of the second pull rod, and the second pull rod drives wing flap to rotate and move up.Feedback
Mechanism is used to give the motion feedback of wing flap to flap control handle mechanism, disconnects for controlling motor, wing flap stopping movement.This
Device can preferably mitigate aircraft power supply load, realize the synchronous rotation of wing flap, while reduce its failure rate, facilitate maintenance.
Upper and lower put of the receipts of wing flap is realize the positive and negative rotation of motor by changing the current direction of motor to realize.
Further, the open end of the described first fan-shaped Rocker arm 5 and the second fan-shaped rocker arm 6 is disposed opposite to each other, first fan
The open end of shape Rocker arm 5 and the second fan-shaped rocker arm 6, which respectively corresponds, is provided with connecting hole 51 and lower connecting hole 52, wherein one is led
It fixes and connects with the lower connecting hole of the upper connecting hole of the described first fan-shaped Rocker arm 5 and the second fan-shaped rocker arm 6 respectively to 7 both ends of cable wire
Connect, in addition the both ends of a guiding cable wire 7 respectively with the lower connecting hole of the described first fan-shaped Rocker arm 5 and the second fan-shaped rocker arm 6
Upper connecting hole is fixedly connected, and is linked for realizing two wing flaps 4.
In this way, drive two guiding cable wires to move in the opposite direction respectively when the first fan-shaped rocker arm rotates clockwise, into
And drive the second fan-shaped rocker arm to rotate clockwise by guiding cable wire, it is arranged on the first fan-shaped rocker arm and the second fan-shaped rocker arm upper
Connecting hole and lower connecting hole are disposed opposite to each other, and the first fan-shaped rocker arm and the second fan-shaped rocker arm can be made in rotation, drive first
Pull rod and the second pull rod do rising or descending motion simultaneously, and then wing flap is driven to rotate synchronously.Structure is simple, facilitates maintenance.
Further, it is fixedly mounted on the wing flap 4 there are two trunnion 8 is rotated, is fixed between 8 upper end of rotation trunnion
It is connected with connecting rod 81, first pull rod 2 and 3 lower end of the second pull rod are provided with lantern ring and are socketed on the connecting rod 81, two
The distance between a described rotation trunnion 8 is greater than the width of lantern ring.
In this way, the distance between two trunnions are greater than the width of lantern ring, the first pull rod and the second pull rod can be preferably given
A space moved horizontally in uphill process can preferably guarantee its motion credibility.
Further, the sector of the described first fan-shaped Rocker arm 5 and the second fan-shaped rocker arm 6 is circumferential is recessed for guiding
The guide groove that cable wire 7 is oriented to.
In this way, guide groove can preferably be oriented to guiding cable wire, structure is simple, can preferably improve guiding steel
The motion credibility of rope.
Further, be additionally provided between the described first fan-shaped rocker arm 6 and the second fan-shaped rocker arm 7 for guiding cable wire into
The directive wheel 53 of row guiding.
In this way, can preferably be oriented to guiding cable wire, structure is simple, can preferably improve the fortune of guiding cable wire
Dynamic reliability.
Further, the wing flap driving mechanism include wing flap Handleset, be fixedly connected with wing flap Handleset it is convex
Wheel 9 and the micro-switch 91 that 9 side of cam is arranged in, the micro-switch 91 are fixedly mounted on wing flap micro-switch support
On frame 92, the micro-switch 91 connect setting by wing flap control circuit with the motor 1.
In this way, band moving cam rotates when wing flap Handleset rotates, the fine motion electricity on cam and wing flap micro-switch bracket
Door release, so that wing flap control circuit is connected, motor action.Micro-switch can preferably detect the rotation of cam, make
With convenient, high reliablity.
Further, the feedback mechanism includes the feedback wire rope 93 being fixedly connected with wing flap micro-switch bracket 92, institute
It states 93 other end of feedback wire rope and connect setting with wing flap linkage mechanism.
In this way, feedback mechanism drives wing flap micro-switch carriage turns, wing flap micro-switch bracket drives micro-switch to turn
Dynamic, so that cam is contacted with micro-switch, wing flap control circuit is disconnected, and electric motor circuit breaking, wing flap stops rotating.
Further, the wing flap Handleset includes handle 94 and handle mount 95, on the handle mount 95
Be provided with sliding slot, 94 outer end of handle is located on the outside of the handle mount, 94 inner end of handle pass through the sliding slot with
Described 9 one end of cam is fixedly connected, and the wing flap micro-switch bracket 92 is rotatably installed in the handle mount 95.
In this way, being provided with handle mount, preferably handle, cam and wing flap micro-switch bracket can be pacified
Dress is easy to use.
Further, it is provided with stop block 96 on the handle mount 95, is provided with finger on the handle mount 95
Show lamp 97 and dial.
In this way, being provided with indicator light, wing flap current location can be preferably shown.It is provided with dial, it can also be more preferable
Display wing flap current location, meanwhile, preferably handle can be revolved to giving intuitively to observe in rotational handle
Turn, to adjust the position of wing flap.It is provided with stop block, preferably can carry out locking in the position to handle.Feedback wire rope, instruction
Lamp and micro-switch collectively form wing flap instruction system, can preferably learn the current location of wing flap, wing flap is being received
When above and putting down, indicator light and wing flap synchronization action are easy to use.
Further, the stop block 96 is in steps setting.
In this way, locking preferably can be carried out to the wing flap in different location, it is easy to use.
The working principle of the present apparatus are as follows: handle is grasped, handle is turned into desired location, cam is rotated with handle,
So that micro-switch is connected, motor action is made by wing flap control circuit, drives worm screw rotation, worm screw drives worm screw beam barrel
It is mobile, and then first rotating shaft rotation is driven, first rotating shaft drives the first fan-shaped rocker arm rotation, and the first fan-shaped rocker arm passes through guiding steel
The fan-shaped rocker arm rotation of strap dynamic second, the second fan-shaped rocker arm drive the second rotation rotation, and the second shaft drives link block rotation, leads to
It crosses link block and triangle part drives the first pull rod and the second pull rod to rise or decline, and then in the receipts of realization wing flap and put down.
Flap configuration is fed back into wing flap micro-switch bracket by feedback wire rope, wing flap micro-switch carriage turns is driven, realizes convex
The compression of wheel and micro-switch, wing flap control circuit disconnect, electric motor circuit breaking, wing flap stopping movement.Using stop block to handle
Position carries out locking.Wing flap current location is indicated using indicator light.
Finally, it should be noted that the above embodiments are merely illustrative of the technical solutions of the present invention, rather than its limitations；Although
Present invention has been described in detail with reference to the aforementioned embodiments, those skilled in the art should understand that；It still may be used
To modify to technical solution documented by previous embodiment, or some or all of the technical features are equal
Replacement；And these are modified or replaceed, the model for technical solution of the embodiment of the present invention that it does not separate the essence of the corresponding technical solution
It encloses, should all cover within the scope of the claims and the description of the invention.
Claims (10)
1. a kind of light aerocraft flap runners, which is characterized in that including flap control handle mechanism, wing flap driving mechanism,
Wing flap linkage mechanism and feedback mechanism, the wing flap driving mechanism includes motor, and the output shaft of the motor is fixedly connected
There is worm screw, is screwed on the outside of the worm screw and is combined with worm screw beam barrel, worm screw beam barrel end is hinged with triangle part, triangle part one end
It is fixedly connected with first rotating shaft；The wing flap linkage mechanism includes the first pull rod and the second pull rod, first pull rod and second
Pull rod is hingedly arranged with two wing flap rotational positions respectively, and first pull rod upper end and triangle part one end are hinged, and described
The first fan-shaped rocker arm is fixedly installed in one shaft, second pull rod upper end is hinged with link block, and the link block lower end is solid
Dingan County is fixedly installed with the second fan-shaped rocker arm in the second shaft in second shaft, the described first fan-shaped rocker arm and the
It is attached by two to guiding cable wire between two fan-shaped rocker arms.
2. a kind of light aerocraft flap runners according to claim 1, it is characterised in that: the described first fan-shaped rocker arm
It is disposed opposite to each other with the open end of the second fan-shaped rocker arm, the open end of the described first fan-shaped rocker arm and the second fan-shaped rocker arm respectively corresponds
It is provided with connecting hole and lower connecting hole, wherein one is oriented to upper connecting hole of the cable wire both ends respectively with the described first fan-shaped rocker arm
Be fixedly connected with the lower connecting hole of the second fan-shaped rocker arm, in addition the both ends of a guiding cable wire respectively with the described first fan-shaped rocker arm
Lower connecting hole and the upper connecting hole of the second fan-shaped rocker arm be fixedly connected, link for realizing two wing flaps.
3. a kind of light aerocraft flap runners according to claim 2, it is characterised in that: fixed peace on the wing flap
Dress is fixedly connected with connecting rod between the rotation trunnion upper end there are two trunnion is rotated, under first pull rod and the second pull rod
End is provided with lantern ring and is socketed on the connecting rod, and the distance between two described rotation trunnions are greater than the width of lantern ring.
4. a kind of light aerocraft flap runners according to claim 3, it is characterised in that: the described first fan-shaped rocker arm
With the circumferential guide groove being recessed for being oriented to guiding cable wire of sector of the second fan-shaped rocker arm.
5. a kind of light aerocraft flap runners according to claim 4, it is characterised in that: the described first fan-shaped rocker arm
And second be additionally provided between fan-shaped rocker arm for the directive wheel for being oriented to cable wire and being oriented to.
6. a kind of light aerocraft flap runners according to claim 5, it is characterised in that: the wing flap driving mechanism
Including wing flap Handleset, the cam being fixedly connected with wing flap Handleset and the fine motion that the cam side is arranged in electricity
Door, the micro-switch are fixedly mounted on wing flap micro-switch bracket, and the micro-switch and the motor pass through wing flap
Control circuit connection setting.
7. a kind of light aerocraft flap runners according to claim 6, it is characterised in that: the feedback mechanism includes
The feedback wire rope being fixedly connected with wing flap micro-switch bracket, the feedback wire rope other end is connect with wing flap linkage mechanism to be set
It sets.
8. a kind of light aerocraft flap runners according to claim 7, it is characterised in that: the wing flap Handleset
Including handle and handle mount, sliding slot is provided on the handle mount, the handle outer end is located at handle installation
Seat outside, the handle inner end pass through the sliding slot and are fixedly connected with described cam one end, and the wing flap micro-switch bracket turns
It is dynamic to be mounted in the handle mount.
9. a kind of light aerocraft flap runners according to claim 8, it is characterised in that: on the handle mount
It is provided with stop block, is provided with indicator light and dial on the handle mount.
10. a kind of light aerocraft flap runners according to claim 9, it is characterised in that: the stop block is in rank
Ladder setting.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910297589.9A CN109911180A (en) | 2019-04-15 | 2019-04-15 | A kind of light aerocraft flap runners |
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| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201910297589.9A CN109911180A (en) | 2019-04-15 | 2019-04-15 | A kind of light aerocraft flap runners |
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| CN109911180A true CN109911180A (en) | 2019-06-21 |
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| CN201910297589.9A Pending CN109911180A (en) | 2019-04-15 | 2019-04-15 | A kind of light aerocraft flap runners |
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Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN111017237A (en) * | 2019-12-19 | 2020-04-17 | 中国航空工业集团公司西安飞机设计研究所 | Mechanical operation alarm device conformal with airfoil |
| CN111762335A (en) * | 2020-07-06 | 2020-10-13 | 中国人民解放军空军军医大学 | Pilot control system mounting fixture |
| CN111874214A (en) * | 2020-07-31 | 2020-11-03 | 九成通用飞机设计制造(大连)有限公司 | Airplane flap mechanism based on linear execution control |
| CN113942631A (en) * | 2021-10-19 | 2022-01-18 | 贵州贵飞飞机设计研究院有限公司 | Aileron rotation locking structure |
| CN115123521A (en) * | 2022-07-11 | 2022-09-30 | 湖南翔龙飞机有限公司 | Flap control system of light airplane |
| CN111874214B (en) * | 2020-07-31 | 2024-07-09 | 九成通用飞机设计制造(大连)有限公司 | Linear execution control-based aircraft flap mechanism |
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| US4244541A (en) * | 1979-01-02 | 1981-01-13 | The Boeing Company | Dual cam control mechanism for coordinated deployment and retraction of an air-craft's leading and trailing edge wing flaps |
| RU2539018C1 (en) * | 2014-02-06 | 2015-01-10 | Федеральное государственное унитарное предприятие "Сибирский научно-исследовательский институт авиации им. С.А. Чаплыгина" | Aircraft wing fan-type flap drive |
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| CN104554710A (en) * | 2014-11-19 | 2015-04-29 | 中国航空工业集团公司沈阳飞机设计研究所 | Servo actuation system for leading edge flap of mechanical double-redundancy airplane |
| CN106428529A (en) * | 2016-09-23 | 2017-02-22 | 江西洪都航空工业集团有限责任公司 | Control mechanism for trailing edge flap of agriculture light airplane |
| CN108313268A (en) * | 2017-01-17 | 2018-07-24 | 湖南山河科技股份有限公司 | A kind of light aerocraft Aileron control system |
| CN208325609U (en) * | 2018-06-11 | 2019-01-04 | 通航国际（西安）飞机技术有限公司 | A kind of aircraft flap control device |
| CN209719900U (en) * | 2019-04-15 | 2019-12-03 | 重庆恩斯特龙通用航空技术研究院有限公司 | A kind of light aerocraft flap runners |
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| CN111874214A (en) * | 2020-07-31 | 2020-11-03 | 九成通用飞机设计制造(大连)有限公司 | Airplane flap mechanism based on linear execution control |
| CN111874214B (en) * | 2020-07-31 | 2024-07-09 | 九成通用飞机设计制造(大连)有限公司 | Linear execution control-based aircraft flap mechanism |
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