CN101962078B - Aircraft propeller vector engine - Google Patents
Aircraft propeller vector engine Download PDFInfo
- Publication number
- CN101962078B CN101962078B CN201010257973.5A CN201010257973A CN101962078B CN 101962078 B CN101962078 B CN 101962078B CN 201010257973 A CN201010257973 A CN 201010257973A CN 101962078 B CN101962078 B CN 101962078B
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- Prior art keywords
- universal arm
- turns
- connects
- gear
- connection
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Abstract
The invention relates to an aircraft propeller vector engine. All these times, the take-off and the landing of fixed-wing propeller-driven planes always require a certain taxiing distance, the maneuverability is poor, and the practicability is greatly limited. The aircraft propeller vector engine comprises a propeller (1) and an engine (2), wherein the engine is connected with a connecting base (3), the connecting base is connected with a universal power transmitter (4), the universal power transmitter is connected with a universal arm (5), the universal arm is connected with a propeller connecting shaft (6), and the propeller connecting shaft is connected with the propeller. The invention is applied to aircraft engines.
Description
Technical field:
The utility model relates to a kind of new work engine of aviation field, is specifically related to a kind of aircraft propeller vector engine.
Background technology:
All the time, the taking off of fixed-wing propeller aeroplane, landing needs certain ground run distance, and motor-driven dynamic poor performance, practicality is subject to a lot of restriction.
Although helicopter can take off vertically, land, there is the shortcomings such as flying speed is slow, voyage is short, flying height is low.
Summary of the invention:
The purpose of this utility model is to provide the driving engine of the heart one classification in a kind of propeller aeroplane system, it solves the vertical and landing takeoff of fixed-wing propeller aeroplane and the problem of maneuvering performance difference.
Above-mentioned object is realized by following technical scheme:
Aircraft propeller vector engine, its composition comprises: screw propeller, driving engine, described driving engine connects Connection Block, described Connection Block connects universal dynamical transmitter, described universal dynamical transmitter connects Universal arm, described Universal arm connects screw propeller adapter shaft, and described screw propeller adapter shaft connects screw propeller.
Described aircraft propeller vector engine, described universal dynamical transmitter comprises and turns to cylinder base, the described cylinder base cover connection that turns to turns to cylinder, described turns to cylinder built with steering shaft, described steering shaft connects universal dynamical transmitter gear, described universal dynamical transmitter gear connection for transmission gear, a described one end cover that turns to connects wheel flutter and tightening nut, described turn to a lower end to be equipped with to turn to a gland, seal ring is equipped with in described turning between cylinder and described steering shaft, described cylinder base one end connection that turns to turns to cylinder base gland, described turn to cylinder base and described turn to upper end between cylinder, lower end is equipped with respectively and is turned to a bearing and turn to a seal ring, described cylinder base one end connection that turns to turns to a lock sleeve, a described lock sleeve connection that turns to turns to a lock bolt and turns to cylinder to lock electromagnetic device.
Described aircraft propeller vector engine, described Universal arm comprises sector roller box, described sector roller box connection turns to cylinder, described sector roller box is built with sector wheels, described sector roller box side connection bracket, described sector wheels comprise lower transverse gear and lower vertical gear, described lower transverse gear connects steering shaft, described lower vertical gear connects lower drive shaft, described lower drive shaft connects lower gear, described lower gear connection cogs, moving axis is uploaded in the described connection that cogs, described moving axis of uploading connects upper vertical gear, described upper vertical gear connects upper transverse gear, described upper transverse gear connects screw propeller adapter shaft, described upper vertical gear and upper transverse gear are contained in Universal arm, described Universal arm side inner connection by bearing uploads moving axis, described outer end, Universal arm side connects gear case by bearing, described Universal arm opposite side connects Universal arm turbine, described Universal arm turbine connects universal arm axle, described universal arm axle one end external diameter connects Universal arm shaft locking cover, Universal arm lock bolt and Universal arm electromagnetic device, outside described Universal arm turbine, Universal arm turbine box is housed, bearing is equipped with in described Universal arm and between described screw propeller adapter shaft and upper end, gland is equipped with in lower end.
Described aircraft propeller vector engine, described Universal arm turbine box comprises Universal arm turbine, described Universal arm turbine connects Universal arm worm screw and to wheel, described connects Universal arm motor to wheel, between described Universal arm turbine and Universal arm turbine box, bearing and bearing seat are housed, described Universal arm turbine box connects Universal arm turbine case lid.
Described aircraft propeller vector engine, described Connection Block connects flap, described Connection Block be connected flap and all there is connecting bore, described Connection Block comprises and turns to a turbine, a described turbine connection that turns to turns to a worm screw and turns to cylinder to wheel, a described worm screw connection that turns to turns to a worm seat, and the described cylinder that turns to turns to a motor to wheel connection, and bearing and bearing seat are equipped with in described turning to a turbine and turn between a worm seat.
Beneficial effect:
1. the utility model solves the vertical and landing takeoff of fixed-wing propeller aeroplane and the problem of maneuvering performance difference.
2. the utility model is relative to the airscrew driving engine of other classification, adds " universal dynamical transmitter " and makes it have vector functions, can accomplish the vertical lift of screw propeller fixed wing aircraft, have higher maneuvering performance.
3. gear of the present utility model, turbine and quadrant gear all adopt box typed structure, make that the structure of this product is safer, good airproof performance, and between part, transmission performance is good, long service life.
4. the utility model structure is simple, technology implementation condition is ripe, does not need special material, transforms existing Processes and apparatus and easily accomplish, can realize normalisation, integrated and producing in serial form.
5. the directed power of driving engine is passed to different azimuth, different angles by the utility model, makes pulling force or the thrust of screw propeller generation upper and lower, left and right different azimuth, different angles, has controlled taking off vertically, land and flying of airframe.
Accompanying drawing illustrates:
The structural representation of accompanying drawing 1 product.
Accompanying drawing 2 is that the A-A of accompanying drawing 1 is to attempting.
Accompanying drawing 3 is that the B--B of accompanying drawing 1 is to attempting.
Detailed description of the invention:
Embodiment 1:
Aircraft propeller vector engine, its composition comprises: screw propeller 1, driving engine 2, described driving engine 2 connects Connection Block 3, described Connection Block 3 connects universal dynamical transmitter 4, described universal dynamical transmitter 4 connects Universal arm 5, described Universal arm 5 connects screw propeller adapter shaft 6, and described screw propeller adapter shaft 6 connects screw propeller.
Embodiment 2:
Aircraft propeller vector engine described in embodiment 1, described universal dynamical transmitter 4 comprises and turns to cylinder base 8, described turn to cylinder base 8 to overlap connection to turn to cylinder 9, described turns to cylinder 9 built with steering shaft 10, described steering shaft 10 connects universal dynamical transmitter gear 11, described universal dynamical transmitter gear 11 connection for transmission gear 12, connection wheel flutter 13 and tightening nut 14 are overlapped in described cylinder 9 one end that turns to, described turn to cylinder 9 lower end to be equipped with to turn to a gland 15, seal ring 16 is equipped with in described turning between cylinder 9 and described steering shaft 10, described cylinder base 8 one end connection that turns to turns to cylinder base gland 17, described turn to cylinder base 8 and described turn to upper end between cylinder 9, lower end is equipped with respectively and is turned to a bearing 18 and turn to a seal ring 19, described cylinder base 8 one end connection that turns to turns to a lock sleeve 20, described turns to a lock sleeve 20 connection to turn to a lock bolt 21 and turns to cylinder to lock electromagnetic device 22.
Described aircraft propeller vector engine, described Connection Block 3 connects flap 23, described Connection Block 3 be connected flap 23 all there is connecting bore 24, described Connection Block 3 comprises and turns to a turbine 25, a described turbine 25 connection that turns to turns to a worm screw 26 and turns to cylinder to wheel 27, the described cylinder that turns to turns to a motor 28 to wheel 27 connection, a described worm screw 26 connection that turns to turns to a worm seat 29, and bearing 30 and bearing seat 31 are equipped with in described turning to a turbine 25 and turn between a worm seat 29.
Embodiment 3:
Aircraft propeller vector engine described in embodiment 1 or 2, described Universal arm 5 comprises sector roller box 32, described sector roller box 32 connection turns to cylinder 9, described sector roller box 32 is built with sector wheels, described sector roller box 32 side connection bracket 33, described sector wheels comprise lower transverse gear 34 and lower vertical gear 35, described lower transverse gear 34 connects steering shaft 10, described lower vertical gear 34 connects lower drive shaft 37, described lower drive shaft 37 connects lower gear 38, described lower gear 38 connection cogs 39, moving axis 40 is uploaded in described 39 connections that cog, described moving axis 40 of uploading connects upper vertical gear 41, described upper vertical gear 41 connects upper transverse gear 42, described upper transverse gear 42 connects screw propeller adapter shaft 6, described upper vertical gear and upper transverse gear are contained in Universal arm, described Universal arm 5 side inner connection by bearing uploads moving axis 43, described outer end, Universal arm side connects gear case 44 by bearing, described Universal arm opposite side connects Universal arm turbine 45, described Universal arm turbine 45 connects universal arm axle 46, described universal arm axle 46 one end external diameter connects Universal arm shaft locking cover 47, Universal arm lock bolt 48 and Universal arm electromagnetic device 49, outside described Universal arm turbine, Universal arm turbine box 50 is housed, bearing is equipped with in described Universal arm and between described screw propeller adapter shaft and upper end, gland 51 is equipped with in lower end, described cog 39 and lower gear 38 to be all contained in gear case 36.
Described aircraft propeller vector engine, described Universal arm turbine box 50 comprises Universal arm turbine 52, described Universal arm turbine 52 connects Universal arm worm screw 53 and to wheel 54, described connects Universal arm motor 55 to wheel 54, between described Universal arm turbine and Universal arm turbine box, bearing and bearing seat are housed, described Universal arm turbine box connects Universal arm turbine case lid 56.
Claims (5)
1. an aircraft propeller vector engine, its composition comprises: screw propeller, driving engine, it is characterized in that: described driving engine connects Connection Block, described Connection Block connects universal dynamical transmitter, described universal dynamical transmitter connects Universal arm, described Universal arm connects screw propeller adapter shaft, described screw propeller adapter shaft connects screw propeller, described universal dynamical transmitter comprise turn to cylinder base overlap connection turn to cylinder, a described worm gear connection that turns to turns to a worm screw, a described worm screw connection that turns to turns to a motor, described Universal arm comprises sector roller box, described sector roller box connection turns to cylinder, described Universal arm worm case comprises Universal arm worm gear, described Universal arm worm gear connects Universal arm worm screw, described Universal arm worm screw connects Universal arm motor.
2. the aircraft propeller vector engine according to claim l, it is characterized in that: described turns to cylinder built with steering shaft, described steering shaft connects universal dynamical transmitter gear, described universal dynamical transmitter gear connection for transmission gear, a described one end cover that turns to connects wheel flutter and tightening nut, described turn to a lower end to be equipped with to turn to a gland, described turn to cylinder and asking of described steering shaft are equipped with seal ring, described cylinder base one end connection that turns to turns to cylinder base gland, described turn to cylinder base and described turn to upper end between cylinder, lower end is equipped with respectively and is turned to a bearing and turn to a seal ring, described cylinder base one end connection that turns to turns to a lock sleeve, a described lock sleeve connection that turns to turns to a lock bolt and turns to cylinder to lock electromagnetic device.
3. the aircraft propeller vector engine according to claim l or 2, it is characterized in that: described sector roller box is built with sector wheels, described sector roller box side connection bracket, described sector wheels comprise lower transverse gear and lower vertical gear, described lower transverse gear connection turns coaxial, described lower vertical gear connects lower drive shaft, described lower drive shaft connects lower gear, described lower gear connection cogs, moving axis is uploaded in the described connection that cogs, described moving axis of uploading connects upper vertical gear, described upper vertical gear connects upper transverse gear, described upper transverse gear connects screw propeller adapter shaft, described upper vertical gear and upper transverse gear are contained in Universal arm, described Universal arm side inner connection by bearing uploads moving axis, described outer end, Universal arm side connects gear case by bearing, described Universal arm opposite side connects Universal arm worm gear, described Universal arm worm gear connects universal arm axle, through connecting Universal arm shaft locking cover outside described universal arm axle one end, Universal arm lock bolt and Universal arm electromagnetic device, outside described Universal arm worm gear, Universal arm worm case is housed, bearing is equipped with in described Universal arm and between described screw propeller adapter shaft and upper end, gland is equipped with in lower end.
4. aircraft propeller vector engine according to claim 1, is characterized in that: between described Universal arm worm gear and Universal arm worm case, bearing and bearing seat are housed, and described Universal arm worm case connects Universal arm worm gear case lid.
5. aircraft propeller vector engine according to claim 1, it is characterized in that: described Connection Block connects flap, described Connection Block be connected flap and all there is connecting bore, described Connection Block comprises and turns to a worm gear, and described turns to a worm gear and turn to asking of a worm seat that bearing and bearing seat are housed.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010257973.5A CN101962078B (en) | 2010-08-20 | 2010-08-20 | Aircraft propeller vector engine |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201010257973.5A CN101962078B (en) | 2010-08-20 | 2010-08-20 | Aircraft propeller vector engine |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| CN101962078A CN101962078A (en) | 2011-02-02 |
| CN101962078B true CN101962078B (en) | 2015-02-25 |
Family
ID=43515184
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201010257973.5A Expired - Fee Related CN101962078B (en) | 2010-08-20 | 2010-08-20 | Aircraft propeller vector engine |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN101962078B (en) |
Families Citing this family (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102390527B (en) * | 2011-09-06 | 2015-02-04 | 陈仁多 | Improved design of helicopter rotor wing moving system |
| CN103010469B (en) * | 2011-09-26 | 2016-05-04 | 王泽民 | Vector power |
| CN104554733A (en) * | 2013-10-14 | 2015-04-29 | 姜文睿 | Jet engine capable of flexibly changing angle of jet engine body relative to airframe |
| CN106275424B (en) * | 2015-05-18 | 2020-01-21 | 王泽民 | Rotor wing tilting mechanism and belt type sealing mechanism for rotor wing tilting mechanism |
Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1880169A (en) * | 2006-03-06 | 2006-12-20 | 孙旻哲 | Double screw propeller one-seater aerobat |
| CN1907806A (en) * | 2005-08-02 | 2007-02-07 | 韩培洲 | helicopter with tilted front rotary wing |
| CN101643116A (en) * | 2009-08-03 | 2010-02-10 | 北京航空航天大学 | Tiltrotor controlled by double-propeller vertical duct |
Family Cites Families (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| MX2008014774A (en) * | 2006-05-19 | 2009-02-06 | Textron Innovations Inc | Constant-velocity drive system for gimbaled rotor hubs. |
-
2010
- 2010-08-20 CN CN201010257973.5A patent/CN101962078B/en not_active Expired - Fee Related
Patent Citations (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1907806A (en) * | 2005-08-02 | 2007-02-07 | 韩培洲 | helicopter with tilted front rotary wing |
| CN1880169A (en) * | 2006-03-06 | 2006-12-20 | 孙旻哲 | Double screw propeller one-seater aerobat |
| CN101643116A (en) * | 2009-08-03 | 2010-02-10 | 北京航空航天大学 | Tiltrotor controlled by double-propeller vertical duct |
Also Published As
| Publication number | Publication date |
|---|---|
| CN101962078A (en) | 2011-02-02 |
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| 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 | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20150225 Termination date: 20180820 |
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| CF01 | Termination of patent right due to non-payment of annual fee |