CN102774497B - Driving device of double-helical panel saucer-shaped aircraft - Google Patents
Driving device of double-helical panel saucer-shaped aircraft Download PDFInfo
- Publication number
- CN102774497B CN102774497B CN201210291738.9A CN201210291738A CN102774497B CN 102774497 B CN102774497 B CN 102774497B CN 201210291738 A CN201210291738 A CN 201210291738A CN 102774497 B CN102774497 B CN 102774497B
- Authority
- CN
- China
- Prior art keywords
- flight
- fan blade
- center shaft
- wheel
- wind hole
- 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.)
- Expired - Fee Related
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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 driving device, particularly relate to a kind of actuating device of double helix dish disc-shaped flying craft.
Background technology
Double helix dish disc-shaped flying craft, actually rare, because double helix dish disc-shaped flying craft is different from common aircraft, so turning to, fly to drive, it differs from common aircraft, need constantly to adjust the normal operation of aircraft all directions balance guarantee disc-shaped flying craft, careless slightlyly just may occur aircraft accident, so provide a kind of stable, simple double helix disc-shaped flying craft actuating device is very important.
Summary of the invention
The invention provides a kind of double helix dish shape aircraft driving device, this actuating device, simple in structure, 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 driving device, for driving the flight of double helix dish butterfly aircraft and turning to, by the driver train that is located at turning operation system, the flight operation system in aircraft cockpit and is located at double helix dish below, formed, it is characterized in that:
Described driver train comprises a criss-cross limit frame that is arranged on helical disk below under fuselage, and on the frame of described criss-cross limit, front and back are respectively symmetrically installed with one group of flight fan blade, and on the frame of criss-cross limit, left and right is respectively symmetrically installed with one group and turns to fan blade;
Describedly 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 variable wind hole, turn to main blade to be connected with variable wind hole center shaft, turn to main blade and turn to the two ends up and down of secondary fan blade to be rotatably connected by connection lead, on the center shaft of variable wind hole, being provided with and turning to fan blade wheel flutter;
The cross limit at described flight fan blade and place is configured to flight wind hole, on the center shaft of flight wind hole, 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 cooperatively interacting is installed, the flight blade shaft driving wheel coordinating with center shaft driving wheel is wherein installed on the flight blade shaft on right side; On the flight blade shaft of flight center shaft both sides, wind hole, flight fan blade is installed, flight wind hole center shaft separates left and right two parts by flight fan blade, and the upper and lower two ends of fan blade in every part are rotatably connected by 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, pipe link end is provided with steering wheel, steering wheel drives wire-drawing wheel to move by the direction bevel gear coordinating with it, and wire-drawing wheel is connected with turning to the bracing wire of fan blade wheel flutter;
Described flight operation system comprises flight balance control lever, operation bridge, bracing wire, 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 for placing the groove of pull wire head, described operation bridge is a Baltimore groove, Baltimore groove two ends are provided with for holding the groove of two spheroids on fixing equicrural triangle framework, described equicrural triangle framework is arranged on operation bridge by a control lever pull back spring, described bracing wire one end is fixed on spheroid groove by pull wire head, the other end is taken turns a side with dogled and is connected, described flight fan blade wheel flutter opposite side is connected with retracing spring, flight fan blade wheel flutter is arranged on the center shaft of flight wind hole and drives the center shaft driving wheel being arranged on the center shaft of flight wind hole to move.
Further, also comprise eight oblique pull locating racks, described oblique pull locating rack one end is fixedly connected with fuselage, and the other end is fixedly connected with the frame of cross limit frame; Center shaft protection link span 8 in wind hole is installed on described wind hole center shaft; The number that turns to fan blade is odd number.
The present invention, simple in structure, stable performance, operating personal can be very fast is familiar with associative operation, and easy to maintenance quick, expense is cheap.
Accompanying drawing explanation
Fig. 1 is structural representation of the present invention.
Fig. 2 is cross of the present invention limit shelf structure schematic diagram.
Fig. 3 is that the present invention turns to fan blade birds-eye view.
Fig. 4 is that the present invention turns to 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 turning operation system schematic diagram of the present invention.
Fig. 8 is the A-A cutaway view of turning operation system schematic diagram of the present invention.
Fig. 9 is 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
As shown in Fig. 1-13, a kind of double helix dish shape aircraft driving device, is comprised of the driver train that is located at turning operation system, the flight operation system in 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 fuselage, and on criss-cross limit frame 1, front and back are respectively symmetrically installed with one group of flight fan blade 2; On criss-cross limit frame 1, left and right is respectively symmetrically installed with one group and turns 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 fan blade 3 and the cross limit frame 1 at place to form variable wind hole, turn to main blade 31 to be connected with variable wind hole center shaft 39, turn to main blade 31 and turn to the two ends up and down of secondary fan blade 32 to be rotatably connected by connection lead, on variable wind hole center shaft 39, being provided with and turning to fan blade wheel flutter 38;
Flight fan blade 2 forms flight wind hole with the cross limit frame 1 at place, on the center shaft of flight wind hole, 29 are provided with center shaft driving wheel 291, on the flight blade shaft 28 of flight center shaft 29 both sides, wind hole, the flight fan blade flower wheel 281 cooperatively interacting is installed, the flight blade shaft driving wheel 282 coordinating with center shaft driving wheel 291 is wherein installed on the flight blade shaft 28 on right side; Flight fan blade 2 is installed on the flight blade shaft 28 of flight center shaft 29 both sides, wind hole, and flight wind hole center shaft 29 separates left and right two parts by flight fan blade 2, and the upper and lower two ends of fan blade in every part are rotatably connected by connection lead.
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 provided with steering wheel 44, steering wheel 44 drives wire-drawing wheel 43 motions by the direction bevel gear 42 coordinating with it, and wire-drawing wheel 43 is connected with turning to 38 bracing wires of fan blade wheel flutter;
Described flight operation system comprises flight balance control lever 5, operation bridge 51, bracing wire 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 for placing the groove of pull wire head, described operation bridge 51 is a Baltimore groove, Baltimore groove two ends are provided with for holding the groove of two spheroids on fixing equicrural triangle framework, described equicrural triangle framework 511 is arranged on operation bridge 51 by a control lever pull back spring 53, described bracing wire 52 one end are fixed on spheroid groove by pull wire head, the other end is taken turns a side with dogled and is connected, described flight fan blade wheel flutter 55 opposite sides are connected with retracing spring 54, flight fan blade wheel flutter 55 is arranged on flight wind hole center shaft 29 and drives the center shaft driving wheel 291 being arranged on the center shaft of flight wind hole to move.
Also comprise eight oblique pull locating racks 6, oblique pull locating rack 6 one end are fixedly connected with fuselage 7, the other end be fixedly connected with the frame of cross limit frame.Center shaft protection link span in wind hole is installed on described wind hole center shaft; The fan blade that turns to of inside, variable wind hole is odd number.
During use, clockwise direction steering wheel rotation 41, because bearing circle 41 belongs to coaxial with steering wheel 44, are connected, and steering wheel 44 can rotate with bearing circle 41 simultaneously, and engagement drives direction bevel gear 42 to do clockwise direction rotation simultaneously.Again because direction bevel gear 42 also belongs to coaxial connection with wire-drawing wheel 43, direction bevel gear 42 also drives wire-drawing wheel 43 to do clockwise direction simultaneously and rotates, wire-drawing wheel 43 is connected with turning to fan blade wheel flutter 38 by bracing wire, so drive, turn to fan blade wheel flutter 38 also to do clockwise direction rotation, turn to fan blade wheel flutter 38 to be coaxially connected with turning to main blade 31, turn to main blade 31 to lodge to clockwise direction, turn to main blade 31 and turn to secondary fan blade to be rotatably connected at two ends Shang Xia 32, turn to secondary fan blade 32 also in company with turning to main blade 31 to lodge to clockwise direction, the wind-force of helical disk is by turning to fan blade to blow away to anticlockwise direction, its antagonistic force promotes fuselage clockwise direction rotation to the right to right rotation, otherwise to anticlockwise, 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 backward by fan blade, and its antagonistic force promotes aircraft and moves horizontally forward.
Promote forward flight balance joystick 5, because 511 spheroid 512 on the equicrural triangle framework of flight balance joystick 5 ends is connected with 55 bracing wires of flight fan blade wheel flutter, so flight fan blade wheel flutter 55 also moves, flight fan blade wheel flutter 55 drives the coaxial center shaft driving wheel connecting 291 motions, center shaft driving wheel 291 drives the flight blade shaft driving wheel coordinating 282 motions with right side, flight blade shaft driving wheel 282 drives its coaxial mounted flight fan blade flower wheel 281 motions, flight fan blade flower wheel 281 drives flight fan blade flower wheel 281 motions of the opposite side coordinating 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, lose lift, the flight so this aircraft will turn forward, if wanted, stop flying forward, only need pull back 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.At this moment must unclamp at once joystick 5, joystick 5 meetings rapid homing under the effect of joystick pull back spring 53.The fan blade that simultaneously flies 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, the upset forward otherwise this aircraft will constantly turn forward.
Claims (4)
1. a double helix dish shape aircraft driving device, for driving the flight of double helix dish butterfly aircraft and turning to, by the driver train that is located at turning operation system, the flight operation system in aircraft cockpit and is located at double helix dish below, formed, it is characterized in that:
Described driver train comprises a criss-cross limit frame that is arranged on helical disk below under fuselage, and on the frame of described criss-cross limit, front and back are respectively symmetrically installed with one group of flight fan blade, and on the frame of criss-cross limit, left and right is respectively symmetrically installed with one group and turns to fan blade;
Describedly turn to fan blade to comprise to turn to main blade and Duo Gen to turn to secondary fan blade, turn to the criss-cross limit at fan blade and place to be configured to variable wind hole, turn to main blade to be connected with variable wind hole center shaft, turn to main blade and turn to the two ends up and down of secondary fan blade to be rotatably connected by connection lead, on the center shaft of variable wind hole, being provided with and turning to fan blade wheel flutter;
The criss-cross limit at described flight fan blade and place is configured to flight wind hole, on the center shaft of flight wind hole, 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 cooperatively interacting is installed, the flight blade shaft driving wheel coordinating with center shaft driving wheel is wherein installed on the flight blade shaft on right side; On the flight blade shaft of flight center shaft both sides, wind hole, flight fan blade is installed, flight wind hole center shaft separates left and right two parts by flight fan blade, and the upper and lower two ends of fan blade in every part are rotatably connected by connection lead;
Described turning operation system comprises steering direction dish, direction bevel gear, wire-drawing wheel, steering wheel, described steering direction dish is connected with a pipe link, pipe link end is provided with steering wheel, steering wheel drives wire-drawing wheel to move by the direction bevel gear coordinating with it, and wire-drawing wheel is connected with turning to the bracing wire of fan blade wheel flutter;
Described flight operation system comprises flight balance control lever, operation bridge, bracing wire, 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 for placing the groove of pull wire head, described operation bridge is a Baltimore groove, Baltimore groove two ends are provided with for holding the groove of two spheroids on fixing equicrural triangle framework, described equicrural triangle framework is arranged on operation bridge by a control lever pull back spring, described bracing wire one end is fixed on spheroid groove by pull wire head, the other end is connected with flight fan blade wheel flutter one side, described flight fan blade wheel flutter opposite side is connected with retracing spring, flight fan blade wheel flutter is arranged on the center shaft of flight wind hole and drives the center shaft driving wheel being arranged on the center shaft of flight wind hole to move.
2. double helix dish shape aircraft driving device according to claim 1, is characterized in that: also comprise eight oblique pull locating racks, described oblique pull locating rack one end is fixedly connected with fuselage, and the other end is fixedly connected with the frame of criss-cross limit frame.
3. double helix dish shape aircraft driving device according to claim 1, is characterized in that: the number that turns to fan blade is odd number.
4. double helix dish shape aircraft driving device according to claim 1, is characterized in that: center shaft protection link span in wind hole is installed on described wind hole center shaft.
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 CN102774497A (en) | 2012-11-14 |
| CN102774497B true 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) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102774497B (en) * | 2012-08-16 | 2014-11-19 | 柴贵景 | Driving device of double-helical panel saucer-shaped aircraft |
| CN103057699A (en) * | 2012-12-26 | 2013-04-24 | 徐四旺 | Flying machine with new structure |
| 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 |
| 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 |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN101559702A (en) * | 2009-03-27 | 2009-10-21 | 谢雁洲 | Tandem double-duct vertical take-off and landing land-air vehicle |
| CN202765292U (en) * | 2012-08-16 | 2013-03-06 | 柴贵景 | Driving device of double helix disc saucer-shaped air vehicle |
Family Cites Families (11)
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|---|---|---|---|---|
| ES2054133T3 (en) * | 1989-04-19 | 1994-08-01 | Sky Disc Holding Sa | AIRCRAFT WITH A PAIR OF ROTORS ROTATING IN THE OPPOSITE DIRECTION. |
| CN2143591Y (en) * | 1992-11-05 | 1993-10-13 | 钟守生 | Flying disc aeroplane |
| CN1172054A (en) * | 1997-05-30 | 1998-02-04 | 周伟 | Aerobat |
| BR0000053A (en) * | 2000-01-12 | 2001-10-02 | Eduardo Bittencourt Sampaio | Aerodynamic force generating device through the circulation of the fluid on a surface |
| CN1626407A (en) * | 2003-12-08 | 2005-06-15 | 陶杰杰 | Frisbee aircraft |
| CN1693139A (en) * | 2004-05-06 | 2005-11-09 | 李泽奇 | Dish type aircraft and its application |
| US20110049307A1 (en) * | 2008-06-03 | 2011-03-03 | Raphael Yoeli | Vtol vehicle with offset engine |
| CN101525052A (en) * | 2009-03-10 | 2009-09-09 | 陶玉兰 | Sucker aircraft |
| CN101857087A (en) * | 2009-04-09 | 2010-10-13 | 史智勇 | Dual-rotor dish-shaped aircraft |
| 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 |
-
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 (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| 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 |
| CN101559702A (en) * | 2009-03-27 | 2009-10-21 | 谢雁洲 | Tandem double-duct vertical take-off and landing land-air vehicle |
| CN202765292U (en) * | 2012-08-16 | 2013-03-06 | 柴贵景 | Driving device of double helix disc saucer-shaped air vehicle |
Also Published As
| Publication number | Publication date |
|---|---|
| WO2014026574A1 (en) | 2014-02-20 |
| CN102774497A (en) | 2012-11-14 |
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| 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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20141119 Termination date: 20210816 |