CN102774497A - Driving device of double-helical panel saucer-shaped aircraft - Google Patents
Driving device of double-helical panel saucer-shaped aircraft Download PDFInfo
- Publication number
- CN102774497A CN102774497A CN2012102917389A CN201210291738A CN102774497A CN 102774497 A CN102774497 A CN 102774497A CN 2012102917389 A CN2012102917389 A CN 2012102917389A CN 201210291738 A CN201210291738 A CN 201210291738A CN 102774497 A CN102774497 A CN 102774497A
- Authority
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- China
- Prior art keywords
- flight
- fan blade
- center shaft
- wind hole
- turn
- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/06—Aircraft not otherwise provided for having disc- or ring-shaped wings
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0421—Initiating means actuated personally operated by hand control sticks for primary flight controls
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
- B64C13/02—Initiating means
- B64C13/04—Initiating means actuated personally
- B64C13/042—Initiating means actuated personally operated by hand
- B64C13/0423—Initiating means actuated personally operated by hand yokes or steering wheels for primary flight controls
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Automation & Control Theory (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Toys (AREA)
Abstract
The invention relates to a driving device of a double-helical panel saucer-shaped aircraft, is used for driving the double-helical panel saucer-shaped aircraft to fly and veer. The driving device consists of a veering operation system arranged in the aircraft cockpit, a flying operation system and a driving mechanism arranged below the double-helical panel. The driving device is simple in structure, stable in performance, convenient and fast in maintenance and low in cost, and the operating personnel can be familiar with related operations fast.
Description
Technical field
The present invention relates to a kind of aircraft actuating device, particularly relate to a kind of actuating device of double helix dish shape aircraft.
Background technology
Double helix dish shape aircraft; Actually rare, because double helix dish shape aircraft is different from common aircraft,, it differs from common aircraft so turning to, fly to drive; Need constantly adjustment aircraft all directions balance could guarantee the normal operation of disc-shaped flying craft; Careless slightlyly just aircraft accident possibly occur, so provide a kind of stable, simple double helix disc-shaped flying craft actuating device is very important.
Summary of the invention
The present invention provides a kind of double helix dish shape aircraft actuating device, and this actuating device is simple in structure, and stable performance is used simple.
For addressing the above problem; Technical scheme of the present invention is: a kind of double helix dish shape aircraft actuating device; Be used to drive the flight of double helix dish butterfly aircraft and turn to; Driver train by being located at turning operation system, the flight operation system in the aircraft cockpit and being located at double helix dish below is formed, and it is characterized in that:
Described driver train comprises a criss-cross limit frame that is arranged on the below of helical disk under the fuselage, respectively is symmetrically installed with one group of flight fan blade before and after on the frame of said criss-cross limit, respectively is symmetrically installed with one group about on the frame of criss-cross limit to turn to fan blade;
Saidly turn to fan blade to comprise to turn to main blade and Duo Gen to turn to secondary fan blade; Turn to the cross limit at fan blade and place to be configured to the variable wind hole; Turn to main blade to be connected with variable wind hole center shaft; Turn to main blade to be connected through connection lead is rotatable, be equipped with on the center shaft of variable wind hole and turn to the fan blade wheel flutter with the two ends up and down that turn to secondary fan blade;
The cross limit at said flight fan blade and place is configured to flight wind hole; On the center shaft of flight wind hole the center shaft driving wheel is installed; On the flight blade shaft of flight center shaft both sides, wind hole the flight fan blade flower wheel that cooperatively interacts is installed, the flight blade shaft driving wheel that cooperates with the center shaft driving wheel wherein is installed on the flight blade shaft on right side; On the flight blade shaft of flight center shaft both sides, wind hole the flight fan blade is installed, the center shaft fan blade that will fly in flight wind hole is told left and right sides two parts, and the fan blade in every part two ends up and down passes through the rotatable connection of connection lead;
Described turning operation system comprises steering direction dish, direction bevel gear, wire-drawing wheel, steering wheel; Described bearing circle is connected with a pipe link; The pipe link end is equipped with steering wheel; Steering wheel drives the wire-drawing wheel motion through the direction bevel gear that cooperates with it, and wire-drawing wheel is connected with turning to the backguy of fan blade wheel flutter;
Described flight operation system comprises flight balance control lever, operation bridge, backguy, flight fan blade wheel flutter; Described operation bridge lower end is fixed with an equicrural triangle framework; Described equicrural triangle framework two base angles are two spheroids; Described spheroid is provided with the groove that is used to place pull wire head; Described operation bridge is a Baltimore groove, and the Baltimore groove two ends are provided with the groove that is used to hold two spheroids on the fixing equicrural triangle framework, and described equicrural triangle framework is installed on the operation bridge through a control lever pull back spring; Described backguy one end is fixed on the spheroid groove through pull wire head; The other end is taken turns a side with dogled and is connected, and described flight fan blade wheel flutter opposite side is connected with retracing spring, and flight fan blade wheel flutter is installed in and drives the center shaft driving wheel motion that is installed on the center shaft of flight wind hole on the center shaft of flight wind hole.
Further, comprise that also eight are tiltedly drawn locating rack, described locating rack one end that tiltedly draws is captiveed joint with fuselage, and the other end is captiveed joint with the frame of cross limit frame; Center shaft protection link span 8 in wind hole is installed on the center shaft of described wind hole; The number that turns to fan blade is an odd number.
The present invention, simple in structure, stable performance, operating personal can be very fast be familiar with associative operation and quick, cost easy to maintenance.
Description of drawings
Fig. 1 is a structural representation of the present invention.
Fig. 2 is a cross of the present invention limit shelf structure scheme drawing.
Fig. 3 is that the present invention turns to the fan blade birds-eye view.
Fig. 4 is that the present invention turns to the fan blade front view.
Fig. 5 is the present invention's fan blade birds-eye view that flies.
Fig. 6 is the present invention's fan blade front view that flies.
Fig. 7 is a turning operation system scheme drawing of the present invention.
Fig. 8 is the A-A cutaway view of turning operation system scheme drawing of the present invention.
Fig. 9 is a flight operation system schematic of the present invention.
Figure 10 is the A-A cutaway view of flight operation system schematic of the present invention.
Figure 11 is that the present invention turns to fan blade and turning operation system scheme of installation.
Figure 12 is the present invention's fan blade wheel flutter front view that flies.
Figure 13 is the present invention's fan blade wheel flutter birds-eye view that flies.
The specific embodiment
Shown in Fig. 1-13, a kind of double helix dish shape aircraft actuating device is made up of the driver train that is located at turning operation system, the flight operation system in the aircraft cockpit and is located at double helix dish below,
Driver train comprises a criss-cross limit frame 1 that is arranged on helical disk below under the fuselage, and front and back respectively are symmetrically installed with one group of flight fan blade 2 on the criss-cross limit frame 1; Respectively be symmetrically installed with one group about on the criss-cross limit frame 1 and turn to fan blade 3;
Turn to fan blade 3 to comprise and turn to main blade 31 and Duo Gen to turn to secondary fan blade 32; Turn to the fan blade 3 and the cross limit frame 1 at place to constitute the variable wind hole; Turn to main blade 31 to be connected with variable wind hole center shaft 39; Turn to main blade 31 to be connected through connection lead is rotatable, be equipped with on the variable wind hole center shaft 39 and turn to fan blade wheel flutter 38 with the two ends up and down that turn to secondary fan blade 32;
Also comprise a turning operation system; Turning operation system comprises steering direction dish 41, direction bevel gear 42, wire-drawing wheel 43, steering wheel 44; Bearing circle 41 is connected with a pipe link 46; Pipe link 46 ends are equipped with steering wheel 44, and steering wheel 44 drives wire-drawing wheel 43 motions through the direction bevel gear 42 that cooperates with it, and wire-drawing wheel 43 is connected with turning to 38 backguys of fan blade wheel flutter;
Described flight operation system comprises flight balance control lever 5, operation bridge 51, backguy 52, flight fan blade wheel flutter; Described operation bridge 51 lower ends are fixed with an equicrural triangle framework 511; Described equicrural triangle framework two base angles are two spheroids 512; Described spheroid 512 is provided with the groove that is used to place pull wire head; Described operation bridge 51 is a Baltimore groove, and the Baltimore groove two ends are provided with the groove that is used to hold two spheroids on the fixing equicrural triangle framework, and described equicrural triangle framework 511 is installed on the operation bridge 51 through a control lever pull back spring 53; Described backguy 52 1 ends are fixed on the spheroid groove through pull wire head; The other end is taken turns a side with dogled and is connected, and described flight fan blade wheel flutter 55 opposite sides are connected with retracing spring 54, and flight fan blade wheel flutter 55 is installed in and drives center shaft driving wheel 291 motions that are installed on the center shaft of flight wind hole on the flight wind hole center shaft 29.
Comprise that also eight are tiltedly drawn locating rack 6, tiltedly draw locating rack 6 one ends to captive joint with fuselage 7, the other end with captive joint with the frame of cross limit frame.Center shaft protection link span in wind hole is installed on the center shaft of described wind hole; It is odd number that variable wind hole in-to-in turns to fan blade.
During use, promptly the clockwise direction steering wheel rotation 41, because bearing circle 41 belongs to coaxial with steering wheel 44 and is connected, steering wheel 44 can rotate with bearing circle 41 simultaneously, and engagement drive direction bevel gear 42 is done the clockwise direction rotation simultaneously.Again because direction bevel gear 42 also belongs to coaxial the connection with wire-drawing wheel 43; Direction bevel gear 42 also drives wire-drawing wheel 43 and does the clockwise direction rotation simultaneously; Wire-drawing wheel 43 is connected with turning to fan blade wheel flutter 38 through backguy, turns to fan blade wheel flutter 38 also to do right-hand revolution so drive, and turns to fan blade wheel flutter 38 and turns to 31 coaxial connections of main blade; Turn to main blade 31 to lodge to clockwise direction; Turn to main blade 31 to be connected with turning to secondary fan blade two ends are rotatable about in the of 32, turn to secondary fan blade 32 also in company with turning to main blade 31 to the clockwise direction lodging, the wind-force of helical disk is blown away to anticlockwise direction through turning to fan blade; Its antagonistic force promote fuselage to the right right-hand revolution be right-hand revolution, otherwise anti-clockwise rotation then; The fan blade that turns in 41 liang of variable wind holes of pushing direction dish lodges forward simultaneously forward, and the wind-force of helical disk is blown away through fan blade backward, and its antagonistic force promotes aircraft and moves horizontally forward.
Promote flight balance joystick 5 forward, because 511 spheroid 512 is connected with 55 backguys of flight fan blade wheel flutter on the equicrural triangle framework of flight balance joystick 5 ends, so flight fan blade wheel flutter 55 also moves; Flight fan blade wheel flutter 55 drives coaxial bonded assembly center shaft driving wheel 291 motions; Center shaft driving wheel 291 drives the flight blade shaft driving wheel that cooperates 282 motions with the right side, and flight blade shaft driving wheel 282 drives its coaxial mounted flight fan blade flower wheel 281 motions, and flight fan blade flower wheel 281 drives flight fan blade flower wheel 281 motions of the opposite side that cooperates with it; So the flight fan blade of axle 29 both sides will lodge in opposite directions in-flight; When the lodging angle of fan blade reaches 90 °, the flight wind hole in the place ahead will be fully closed, and lose lift; The flight so this aircraft will turn forward; If want to stop to fly forward, only need pulled backwards joystick 5, this aircraft just can restore balance rapidly.
What here pay particular attention to is in specific operation process, can only suitably close flight wind hole, makes the angle of inclination of aircraft reach desirable state of flight and gets final product.At this moment must unclamp joystick 5 at once, joystick 5 meetings rapid homing under the effect of joystick pull back spring 53.The fan blade that flies simultaneously also can set back rapidly under the effect of flight fan blade pull back spring 54.Operation only so, aircraft could be under desirable angle of inclination state, and long-time stable flies according to perfect condition, otherwise this aircraft will constantly turn forward until upset forward.
Claims (4)
1. double helix dish shape aircraft actuating device; Be used to drive the flight of double helix dish butterfly aircraft and turn to; Driver train by being located at turning operation system, the flight operation system in the aircraft cockpit and being located at double helix dish below is formed, and it is characterized in that:
Described driver train comprises a criss-cross limit frame that is arranged on the below of helical disk under the fuselage, respectively is symmetrically installed with one group of flight fan blade before and after on the frame of said criss-cross limit, respectively is symmetrically installed with one group about on the frame of criss-cross limit to turn to fan blade;
Saidly turn to fan blade to comprise to turn to main blade and Duo Gen to turn to secondary fan blade; Turn to the cross limit at fan blade and place to be configured to the variable wind hole; Turn to main blade to be connected with variable wind hole center shaft; Turn to main blade to be connected through connection lead is rotatable, be equipped with on the center shaft of variable wind hole and turn to the fan blade wheel flutter with the two ends up and down that turn to secondary fan blade;
The cross limit at said flight fan blade and place is configured to flight wind hole; On the center shaft of flight wind hole the center shaft driving wheel is installed; On the flight blade shaft of flight center shaft both sides, wind hole the flight fan blade flower wheel that cooperatively interacts is installed, the flight blade shaft driving wheel that cooperates with the center shaft driving wheel wherein is installed on the flight blade shaft on right side; On the flight blade shaft of flight center shaft both sides, wind hole the flight fan blade is installed, the center shaft fan blade that will fly in flight wind hole is told left and right sides two parts, and the fan blade in every part two ends up and down passes through the rotatable connection of connection lead;
Described turning operation system comprises steering direction dish, direction bevel gear, wire-drawing wheel, steering wheel; Described bearing circle is connected with a pipe link; The pipe link end is equipped with steering wheel; Steering wheel drives the wire-drawing wheel motion through the direction bevel gear that cooperates with it, and wire-drawing wheel is connected with turning to the backguy of fan blade wheel flutter;
Described flight operation system comprises flight balance control lever, operation bridge, backguy, flight fan blade wheel flutter; Described operation bridge lower end is fixed with an equicrural triangle framework; Described equicrural triangle framework two base angles are two spheroids; Described spheroid is provided with the groove that is used to place pull wire head; Described operation bridge is a Baltimore groove, and the Baltimore groove two ends are provided with the groove that is used to hold two spheroids on the fixing equicrural triangle framework, and described equicrural triangle framework is installed on the operation bridge through a control lever pull back spring; Described backguy one end is fixed on the spheroid groove through pull wire head; The other end is taken turns a side with dogled and is connected, and described flight fan blade wheel flutter opposite side is connected with retracing spring, and flight fan blade wheel flutter is installed in and drives the center shaft driving wheel motion that is installed on the center shaft of flight wind hole on the center shaft of flight wind hole.
2. double helix dish shape aircraft actuating device according to claim 1 is characterized in that: comprise that also eight are tiltedly drawn locating rack, described locating rack one end that tiltedly draws is captiveed joint with fuselage, and the other end is captiveed joint with the frame of cross limit frame.
3. double helix dish shape aircraft actuating device according to claim 1, it is characterized in that: the number that turns to fan blade is an odd number.
4. double helix dish shape aircraft actuating device according to claim 1 is characterized in that: center shaft protection link span in wind hole is installed on the center shaft of described wind hole.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210291738.9A CN102774497B (en) | 2012-08-16 | 2012-08-16 | Driving device of double-helical panel saucer-shaped aircraft |
| PCT/CN2013/081260 WO2014026574A1 (en) | 2012-08-16 | 2013-08-12 | Flight control device for double-spiral saucer-shaped aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201210291738.9A CN102774497B (en) | 2012-08-16 | 2012-08-16 | Driving device of double-helical panel saucer-shaped aircraft |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN102774497A true CN102774497A (en) | 2012-11-14 |
| CN102774497B CN102774497B (en) | 2014-11-19 |
Family
ID=47119656
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201210291738.9A Expired - Fee Related CN102774497B (en) | 2012-08-16 | 2012-08-16 | Driving device of double-helical panel saucer-shaped aircraft |
Country Status (2)
| Country | Link |
|---|---|
| CN (1) | CN102774497B (en) |
| WO (1) | WO2014026574A1 (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103057699A (en) * | 2012-12-26 | 2013-04-24 | 徐四旺 | Flying machine with new structure |
| CN103171388A (en) * | 2013-03-18 | 2013-06-26 | 中国人民解放军装甲兵工程学院 | Vertical lifting land-air dual-purpose vehicle |
| WO2014026574A1 (en) * | 2012-08-16 | 2014-02-20 | Chai Guijing | Flight control device for double-spiral saucer-shaped aircraft |
| CN108448478A (en) * | 2017-10-27 | 2018-08-24 | 广东电网有限责任公司揭阳供电局 | A kind of adjust automatically center of gravity circuit foreign body eliminating apparatus |
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| WO2001051354A1 (en) * | 2000-01-12 | 2001-07-19 | Eduardo Bittencourt Sampaio | A device for generating an aerodynamic force by inducing rotational movement on the air |
| CN1313226A (en) * | 2000-03-10 | 2001-09-19 | 史绵武 | Disk-shaped aircraft with wings |
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| CN202765292U (en) * | 2012-08-16 | 2013-03-06 | 柴贵景 | Driving device of double helix disc saucer-shaped air vehicle |
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| CN102602539B (en) * | 2012-04-06 | 2014-04-30 | 柴贵景 | Double spiral disc butterfly aircraft |
| CN102774497B (en) * | 2012-08-16 | 2014-11-19 | 柴贵景 | Driving device of double-helical panel saucer-shaped aircraft |
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2012
- 2012-08-16 CN CN201210291738.9A patent/CN102774497B/en not_active Expired - Fee Related
-
2013
- 2013-08-12 WO PCT/CN2013/081260 patent/WO2014026574A1/en active Application Filing
Patent Citations (7)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2001051354A1 (en) * | 2000-01-12 | 2001-07-19 | Eduardo Bittencourt Sampaio | A device for generating an aerodynamic force by inducing rotational movement on the air |
| CN1313226A (en) * | 2000-03-10 | 2001-09-19 | 史绵武 | Disk-shaped aircraft with wings |
| GB2378427A (en) * | 2001-08-08 | 2003-02-12 | Eric Ronald Walmsley | V.T.O.L. Aircraft |
| CN101368550A (en) * | 2007-08-16 | 2009-02-18 | 吴利明 | Vacuum type rotary disc |
| US20110049307A1 (en) * | 2008-06-03 | 2011-03-03 | Raphael Yoeli | Vtol vehicle with offset engine |
| CN101559702A (en) * | 2009-03-27 | 2009-10-21 | 谢雁洲 | Longitudinal-line-type dual-culvert vertical-lifting air-ground vehicle |
| CN202765292U (en) * | 2012-08-16 | 2013-03-06 | 柴贵景 | Driving device of double helix disc saucer-shaped air vehicle |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| WO2014026574A1 (en) * | 2012-08-16 | 2014-02-20 | Chai Guijing | Flight control device for double-spiral saucer-shaped aircraft |
| CN103057699A (en) * | 2012-12-26 | 2013-04-24 | 徐四旺 | Flying machine with new structure |
| CN103171388A (en) * | 2013-03-18 | 2013-06-26 | 中国人民解放军装甲兵工程学院 | Vertical lifting land-air dual-purpose vehicle |
| CN103171388B (en) * | 2013-03-18 | 2015-04-22 | 中国人民解放军装甲兵工程学院 | Vertical lifting land-air dual-purpose vehicle |
| CN108448478A (en) * | 2017-10-27 | 2018-08-24 | 广东电网有限责任公司揭阳供电局 | A kind of adjust automatically center of gravity circuit foreign body eliminating apparatus |
| CN108448478B (en) * | 2017-10-27 | 2024-01-05 | 广东电网有限责任公司揭阳供电局 | Automatic adjust focus circuit foreign matter clearing device |
Also Published As
| Publication number | Publication date |
|---|---|
| CN102774497B (en) | 2014-11-19 |
| WO2014026574A1 (en) | 2014-02-20 |
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