CN103274044A - Aircraft rudder plate transmission mechanism - Google Patents
Aircraft rudder plate transmission mechanism Download PDFInfo
- Publication number
- CN103274044A CN103274044A CN2013102279823A CN201310227982A CN103274044A CN 103274044 A CN103274044 A CN 103274044A CN 2013102279823 A CN2013102279823 A CN 2013102279823A CN 201310227982 A CN201310227982 A CN 201310227982A CN 103274044 A CN103274044 A CN 103274044A
- Authority
- CN
- China
- Prior art keywords
- cross bar
- gear
- box frame
- connecting rod
- wing
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Granted
Links
Images
Landscapes
- Gear Transmission (AREA)
Abstract
The invention relates to an aircraft rudder plate transmission mechanism. The aircraft rudder plate transmission mechanism comprises a fuselage, vertical swing wings and transverse swing wings, a box-shaped frame is arranged at the bottom of the fuselage, a motor is arranged at the rear side of the box-shaped frame, a first transverse rod and a second transverse rod are arranged in the box-shaped frame, and the second transverse rod movably stretches to the first transverse rod. Two ends of the first transverse rod are connected with the vertical swing wings respectively. Two ends of the second transverse rod cooperate with the transverse swing wings respectively. A wheel axle, a first gear, a worm and a worm gear are arranged in the box-shaped frame, and the motor drives the vertical swing wings at two ends of the first transverse rod to rotate at a certain angle through the worm and the worm gear, so the transmission of the vertical swing wings is realized. Another motor drives swing blocks at two ends of a connecting rod to rotate at a certain angle through a rotating shaft, the first gear, a first gullet on the second transverse rod, a tooth bar connected with the two ends of the second transverse rod, a second gear and the connecting rod, so the transmission of the transverse swing wings is realized. The aircraft rudder plate transmission mechanism has a simple structure and a low production cost, and is suitable for small aircrafts.
Description
Technical field
The present invention relates to a kind of aircraft.Specifically, be only can carry a people, can be at the carry-on rudder plate transmission device of the narrow and small MODEL OVER COMPLEX TOPOGRAPHY landing in high mountain or valley and so on.
Background technology
Know all that in the aircraft field of making traditional small aircraft needs the flank formula aircraft of runway when mostly being provided with flank, landing in the fuselage both sides, for satisfying the enough buoyancy in the flight course, just require two flanks to want enough length.And flank one is long, and the transmission device of handling this flank is more complicated also, makes manufacturing cost higher.
Summary of the invention
The problem to be solved in the present invention provides a kind of aircraft rudder plate transmission device.This aircraft rudder plate transmission device, simple in structure, productive costs is low.
For addressing the above problem, take following technical scheme:
Aircraft rudder plate transmission device of the present invention comprise fuselage, vertically put the wing, laterally put the wing, be characterized in that fuselage bottom has box frame, first cross bar is arranged in the box frame, and the first cross bar two ends are all stretched out outside the two lateral walls of box frame and are linked to each other with described vertical pendulum wing respectively.Being on first cross bar in the box frame fixedly has worm gear, in the box frame of worm gear one side worm screw is arranged, and worm and wheel meshes together.Be rotatable shape between described worm screw lower end and box frame bottom and cooperate, link to each other with the output shaft of a motor after passing the box frame top on the worm screw.Second cross bar is arranged in the box frame, and described first cross bar is hollow tubular, and described second cross bar is moving type and stretches in first cross bar.First cross bar, one side that is in the box frame has wheel shaft, is rotatable shape between wheel shaft lower end and box frame bottom and cooperates, and links to each other with the output shaft of another motor after passing the box frame top on the wheel shaft.First gear is fixedly arranged on the wheel shaft, on first cross bar relative with this first gear He on second cross bar axial long hole and first teeth groove is arranged respectively, one side described first gear cross described axial long hole after mesh together with described first teeth groove.There is transverse holes the centre of described vertical pendulum wing, the line of centers of this transverse holes is vertical with described second cross bar, be installed with connecting rod in the transverse holes, the two ends of described connecting rod are stretched out respectively and are vertically being put outside the wing two sides, the two ends of described connecting rod all are connected with wing piece, thereby constitute the described horizontal pendulum wing by the wing piece at connecting rod and connecting rod two ends.Being on that section connecting rod in the described transverse holes has two bearings, on that section connecting rod between described two bearings second gear is arranged fixedly.Have on described vertical pendulum wing and the parallel vertical blind hole of one side, the two ends of first cross bar are stretched into and are fixed in vertical blind hole on corresponding vertical pendulum wing.Vertical with connecting rod, parallel with vertical blind hole bar hole is arranged on vertical pendulum wing of described second gear, one side, and bar has tooth bar in the hole, and described tooth bar and described second gear mesh together.All there is axial pass trough at the two ends of described first cross bar, and an end of described two tooth bars all links together by the two ends of screw and axial pass trough and second cross bar.
Take such scheme, have the following advantages:
By such scheme as can be seen, because fuselage bottom has box frame, first cross bar is arranged in the box frame, the first cross bar two ends are all stretched out outside the two lateral walls of box frame and are linked to each other with described vertical pendulum wing respectively.Being on first cross bar in the box frame fixedly has worm gear, in the box frame of worm gear one side worm screw is arranged, and worm and wheel meshes together.Be rotatable shape between described worm screw lower end and box frame bottom and cooperate, link to each other with the output shaft of a motor after passing the box frame top on the worm screw.Second cross bar is arranged in the box frame, and described first cross bar is hollow tubular, and described second cross bar is moving type and stretches in first cross bar.First cross bar, one side that is in the box frame has wheel shaft, is rotatable shape between wheel shaft lower end and box frame bottom and cooperates, and links to each other with the output shaft of another motor after passing the box frame top on the wheel shaft.First gear is fixedly arranged on the wheel shaft, on first cross bar relative with this first gear He on second cross bar axial long hole and first teeth groove is arranged respectively, one side described first gear cross described axial long hole after mesh together with described first teeth groove.There is transverse holes the centre of described vertical pendulum wing, the line of centers of this transverse holes is vertical with described second cross bar, be installed with connecting rod in the transverse holes, the two ends of described connecting rod are stretched out respectively and are vertically being put outside the wing two sides, the two ends of described connecting rod all are connected with wing piece, thereby constitute the described horizontal pendulum wing by the wing piece at connecting rod and connecting rod two ends.Being on that section connecting rod in the described transverse holes has two bearings, on that section connecting rod between described two bearings second gear is arranged fixedly.Have on described vertical pendulum wing and the parallel vertical blind hole of one side, the two ends of first cross bar are stretched into and are fixed in vertical blind hole on corresponding vertical pendulum wing.Vertical with connecting rod, parallel with vertical blind hole bar hole is arranged on vertical pendulum wing of described second gear, one side, and bar has tooth bar in the hole, and described tooth bar and described second gear mesh together.All there is axial pass trough at the two ends of described first cross bar, and an end of described two tooth bars all links together by the two ends of screw and axial pass trough and second cross bar.Just realize the transmission that two covers are vertically put the wing and laterally put the wing by worm gear, worm screw, gear, tooth bar and motor, thereby simplified the structure greatly, reduced productive costs.
Description of drawings
Fig. 1 is aircraft rudder plate transmission device structural representation of the present invention;
Fig. 2 is the A-A cross-sectional schematic of Fig. 1;
Fig. 3 is the B-B cross-sectional schematic of Fig. 1;
Fig. 4 is the C-C cross-sectional schematic of Fig. 1;
Fig. 5 is the D-D cross-sectional schematic of Fig. 2;
Fig. 6 is the F-F cross-sectional schematic of Fig. 2.
The specific embodiment
As Fig. 1, Fig. 2, Fig. 3, Fig. 4, Fig. 5, shown in Figure 6, aircraft rudder plate transmission device of the present invention comprises fuselage 7, as vertical pendulum wing 10 of rudder plate with laterally put the wing, fuselage 7 bottoms are connected with box frame 5, having first cross bar of installation, 11, the first cross bars, 11 two ends all to stretch out outside the two lateral walls of box frame 5 in the box frame 5 also links to each other with described vertical pendulum wing 10 respectively.
Being on first cross bar 11 in the box frame 5 fixedly has worm gear 2, is provided with worm screw 1 in the box frame 5 of worm gear 2 one sides, and worm screw 1 meshes together with worm gear 2.Being rotatable shape by bearing between described worm screw 1 lower end and box frame 5 bottoms cooperates.Worm screw 1 upper end links to each other with the output shaft of a motor 6 after passing box frame 5 tops.Box frame 5 is provided with second cross bar 12, and described first cross bar 11 is hollow tubular, and described second cross bar 12 is moving type and stretches in first cross bar 11, makes second cross bar 12 can move axially in first cross bar 11.First cross bar, 11 1 sides that are in the box frame 5 are provided with wheel shaft 8, are rotatable shape by bearing between wheel shaft 8 lower ends and box frame 5 bottoms and cooperate, and wheel shaft 8 upper ends link to each other with the output shaft of another motor 6 after passing box frame 5 tops.First gear 16 is fixedly arranged on the wheel shaft 8, on first cross bar 11 relative with first gear 16 and be processed with axial long hole 18 and first teeth groove 9 respectively on second cross bar 12, one side described axial long hole 18 backs of crossing of described first gear 16 mesh together with described first teeth groove 9.The centre of described vertical pendulum wing 10 is processed with transverse holes, the line of centers of this transverse holes is vertical with described second cross bar 12, be installed with connecting rod 3 in the transverse holes, the two ends of described connecting rod 3 are stretched out respectively and are vertically being put outside the wing 10 two sides, the two ends of described connecting rod 3 all are equipped with wing piece 4, thereby constitute the described horizontal pendulum wing by the wing piece 4 at connecting rod 3 and connecting rod 3 two ends.Be on that section connecting rod 3 in the described transverse holes two bearings are installed, second gear 13 is fixedly arranged on that section connecting rod 3 between described two bearings.There are the two ends of vertical blind hole 17, the first cross bars 11 parallel with aerofoil to stretch into and be fixed in vertical blind hole 17 on corresponding vertical pendulum wing 10 on described vertical pendulum wing 10.Be processed with 3 vertical with connecting rod, parallel with vertical blind hole 17 bar hole 19 on vertical pendulum wing 10 of described second gear, 13 1 sides, tooth bar 14 fixedly is arranged in the bar hole 19, described tooth bar 14 and described second gear 13 mesh together.The two ends of described first cross bar 11 all are processed with axial pass trough 20, and an end of described two tooth bars 14 all links together by the two ends of screw 15 and axial pass trough 20 and second cross bar 12.
When the angle of the wing 10 is vertically put in the need adjustment, start a motor 6 earlier, rotated to an angle by vertical pendulum wing 10 that worm screw 1, worm gear 2 drive first cross bar, 11 two ends successively by this motor, thereby realize the vertically transmission of the pendulum wing 10.When the need adjustment is laterally put the wing, start another motor 6 earlier, the tooth bar 14, second gear 13 and the connecting rod 3 that are connected together by first teeth groove 9 on rotating shaft 8, first gear 16, axial long hole 18, second cross bar 12, with second cross bar, 12 two ends successively by this motor, come the wing piece 4 at drivening rod 3 two ends to rotate to an angle, thereby realize the laterally transmission of the pendulum wing.
Claims (1)
1. aircraft rudder plate transmission device, comprise fuselage (7), vertically put the wing (10), laterally put the wing, it is characterized in that fuselage bottom has box frame (5), first cross bar (11) is arranged in the box frame (5), and first cross bar (11) two ends are all stretched out outside the two lateral walls of box frame (5) and are linked to each other with described vertical pendulum wing (10) respectively; First cross bar (11) that is in the box frame (5) upward fixedly has worm gear (2), in the box frame (5) of worm gear (2) one sides worm screw (1) is arranged, and worm screw (1) meshes together with worm gear (2); Be rotatable shape between described worm screw (1) lower end and box frame (5) bottom and cooperate, link to each other with the output shaft of a motor (6) after passing box frame (5) top on the worm screw (1); Second cross bar (12) is arranged in the box frame (5), and described first cross bar (11) is hollow tubular, and described second cross bar (12) is moving type and stretches in first cross bar (11); First cross bar (11) one sides that are in the box frame (5) have wheel shaft (8), be rotatable shape between wheel shaft (8) lower end and box frame (5) bottom and cooperate, link to each other with the output shaft of another motor (6) after passing box frame (5) top on the wheel shaft (8); Wheel shaft (8) is gone up fixedly first gear (16), first cross bar (11) relative with this first gear go up and second cross bar (12) on axial long hole (18) and first teeth groove (9) are arranged respectively, described first gear (16) one side cross described axial long hole (18) back and described first teeth groove (9) meshes together; There is transverse holes the centre of described vertical pendulum wing (10), the line of centers of this transverse holes is vertical with described second cross bar (12), be installed with connecting rod (3) in the transverse holes, the two ends of described connecting rod (3) are stretched out respectively and are vertically being put outside the wing two sides, the two ends of described connecting rod (3) all are connected with wing piece (4), thereby constitute the described horizontal pendulum wing by the wing piece (4) at connecting rod (3) and connecting rod (3) two ends; Being on that section connecting rod (3) in the described transverse holes has two bearings, and that section connecting rod (3) between described two bearings is gone up fixedly second gear (13); Have on described vertical pendulum wing (10) and the parallel vertical blind hole (17) of one side, the two ends of first cross bar (11) are stretched into and are fixed in vertical blind hole (17) on corresponding vertical pendulum wing (10); Vertical with connecting rod (3), parallel with vertical blind hole (17) bar hole (19) is arranged on vertical pendulum wing (10) of described second gear (13) one sides, tooth bar (14) is arranged in the bar hole (19), and described tooth bar (14) meshes together with described second gear (13); All there is axial pass trough (20) at the two ends of described first cross bar (11), and an end of described two tooth bars (14) all links together by the two ends of screw (15) and axial pass trough (20) and second cross bar (12).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310227982.3A CN103274044B (en) | 2013-06-08 | 2013-06-08 | Aircraft rudder plate transmission mechanism |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201310227982.3A CN103274044B (en) | 2013-06-08 | 2013-06-08 | Aircraft rudder plate transmission mechanism |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN103274044A true CN103274044A (en) | 2013-09-04 |
| CN103274044B CN103274044B (en) | 2015-07-08 |
Family
ID=49056708
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201310227982.3A Active CN103274044B (en) | 2013-06-08 | 2013-06-08 | Aircraft rudder plate transmission mechanism |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103274044B (en) |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5513543A (en) * | 1993-03-26 | 1996-05-07 | Mpc Products | Adjustable control lever with variable pressure detent |
| US5950774A (en) * | 1997-10-02 | 1999-09-14 | Sundstrand Corporation | Load limiter |
| CN102076561A (en) * | 2008-06-27 | 2011-05-25 | 马丁飞机有限公司 | Personal flight vehicle including control system |
| CN201951711U (en) * | 2010-10-18 | 2011-08-31 | 南京航空航天大学 | Tilting mechanism |
| CN203486134U (en) * | 2013-06-08 | 2014-03-19 | 无锡振华机械有限公司 | Aircraft rudder plate transmission mechanism |
-
2013
- 2013-06-08 CN CN201310227982.3A patent/CN103274044B/en active Active
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5513543A (en) * | 1993-03-26 | 1996-05-07 | Mpc Products | Adjustable control lever with variable pressure detent |
| US5950774A (en) * | 1997-10-02 | 1999-09-14 | Sundstrand Corporation | Load limiter |
| CN102076561A (en) * | 2008-06-27 | 2011-05-25 | 马丁飞机有限公司 | Personal flight vehicle including control system |
| CN201951711U (en) * | 2010-10-18 | 2011-08-31 | 南京航空航天大学 | Tilting mechanism |
| CN203486134U (en) * | 2013-06-08 | 2014-03-19 | 无锡振华机械有限公司 | Aircraft rudder plate transmission mechanism |
Also Published As
| Publication number | Publication date |
|---|---|
| CN103274044B (en) | 2015-07-08 |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| CN103693121B (en) | A kind of Transformable caterpillar | |
| CN202505628U (en) | Engaging and disengaging type electrically powered wheelchair driver | |
| EP3159262A1 (en) | Inter-propeller blade pitch control device of coaxial double-propeller helicopter | |
| CN103072689B (en) | Slow speed of revolution double-layer propeller helicopter | |
| CN203486134U (en) | Aircraft rudder plate transmission mechanism | |
| CN103603517A (en) | Cantilever type parking garage | |
| CN103287488A (en) | Front wheel steering mechanism | |
| CN203008873U (en) | Rack type twin-well oil pumping unit | |
| CN202029679U (en) | Power-driven lifting device of skylight of bus | |
| CN101873089B (en) | Double-spiral transmission sun-tracking large-area composite frame | |
| CN103274044A (en) | Aircraft rudder plate transmission mechanism | |
| CN203637971U (en) | Transformable crawler | |
| CN105235903A (en) | Bionic swing wing aircraft | |
| CN205838500U (en) | The scissors lift device of height can be adjusted flexibly | |
| CN103017112B (en) | Lifting support frame and comprise the lighting device of this lifting support frame | |
| CN203141009U (en) | Vertical type connecting-rod-type intersecting line cutting head | |
| CN209795809U (en) | Flap control mechanism of light sport aircraft | |
| CN103274048B (en) | Can at the aircraft of complex-terrain landing | |
| CN203585222U (en) | Coaxial reverse rotation planetary speed reducer | |
| CN203652108U (en) | Transmission mechanism for extension and retraction of ceiling propeller of vertical takeoff and landing low-altitude civil rotorcraft | |
| CN204473141U (en) | Bionic mechanical bird | |
| CN203127143U (en) | Low-rotating-speed double-layer propcopter | |
| CN206349072U (en) | A kind of polygon involute draws teaching aid | |
| CN202245628U (en) | Elevator car cordless lifting mechanism of vertical lift elevator | |
| CN201934590U (en) | Differential planetary power distribution reduction gear |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C41 | Transfer of patent application or patent right or utility model | ||
| TR01 | Transfer of patent right |
Effective date of registration: 20161208 Address after: Suzhou City, Jiangsu province 215155 Xiangcheng District Wang Ting Zhen Hua Yang Cun Hua Lu Qiang Patentee after: HELIPELLER GENERAL AIRCRAFT CO.,LTD. Address before: 214156 Jiangsu city of Wuxi province Yangshan Huishan Economic Development Zone, supporting the district on the day Patentee before: WUXI ZHENHUA MACHINERY CO.,LTD. |
|
| TR01 | Transfer of patent right |
Effective date of registration: 20230818 Address after: Room 202, No. 11 Dexing Lane, Chong'an District, Wuxi City, Jiangsu Province, 214000 Patentee after: Yang Haiyan Address before: 215155 Qianghua Road, Huayang Village, Wangting Town, Xiangcheng District, Suzhou City, Jiangsu Province Patentee before: HELIPELLER GENERAL AIRCRAFT CO.,LTD. |
|
| TR01 | Transfer of patent right |