CN201357943Y - Rotary-wing vertical takeoff and landing jet aircraft - Google Patents
Rotary-wing vertical takeoff and landing jet aircraft Download PDFInfo
- Publication number
- CN201357943Y CN201357943Y CNU2008201351471U CN200820135147U CN201357943Y CN 201357943 Y CN201357943 Y CN 201357943Y CN U2008201351471 U CNU2008201351471 U CN U2008201351471U CN 200820135147 U CN200820135147 U CN 200820135147U CN 201357943 Y CN201357943 Y CN 201357943Y
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Abstract
The utility model relates to a rotary-wing vertical takeoff and landing jet aircraft, which comprises a rotary wing, an air inlet cabin, an air jet cabin, a main cabin, rotating shafts, rudder plates and the like, and also comprises a rotating cabin (1), wherein the air inlet cabin (4) and the air jet cabin (5) are collectively known as the rotating cabin (1), and the rudder plates (43,46,49) rotate by the rotating power of motors (41,44,47) transmitted by the rotating shafts (42,45,48); and air is jetted from air nozzles (6,7) below wings to drive the rotary wing to rotate, and meanwhile, air is sucked from air inlets (2,3) and air is jetted from the air nozzles, so that the low air pressure above the wings and the high air pressure below the wings are generated to generate lift force. In this way, the jet aircraft can take off and land vertically and suspend in the air, and when the aircraft turns, the rudder plates (43,46,49) can be used to enable the main cabin (21) to horizontally rotate to complete the turning of the aircraft. Through the design, the jet aircraft can take off and land vertically, suspend in the air and no longer needs larger maneuver when turning.
Description
Technical field
The utility model is rotatable wing aircraft, but specifically rotates wing vertical takeoff and landing jet plane.
Background technology
Need long runway when existing jet plane takes off, need bigger maneuver when turning to, can't aloft suspend in addition.
Summary of the invention
But the jet plane that the purpose of this utility model provides a vertical takeoff and landing, suspends and turn in the mode of rotation in the air.
The utility model above-mentioned purpose is to realize by such technical scheme, but be a kind of rotation wing vertical takeoff and landing jet plane, comprise the rotation wing, admission port, air inlet gas cabin, jet gas cabin, air nozzle, turbo-machine, bearing, main cabin, turbo-machine air inlet pipe, turbo-machine gas ejector pipe, jet valve, motor, S. A., rudder plate; It is characterized in that: inlet air compartment and thrust unit are collectively referred to as rotatable cabin; Main cabin only contacts at the bearing place with rotatable cabin; Rotatable cabin relies on bearing suspension to enclose main out of my cabin; Rudder plate is rotated by the rotary power by the motor of S. A. transmission.Rotatable cabin is connected with 4 groups of 8 bearings with main cabin, and rotatable cabin can enclose out of my cabin to do and horizontally rotate the master.Gas ejector pipe and turbo-machine join and are sprayed by air nozzle after gas with turbo-machine ejection imports thrust unit, the jet promotion rotatable cabin rotation of air nozzle, the admission port opening direction is opposite with air nozzle direction direction, the admission port opening direction forward when rotatable cabin rotates, air pours into and admission port bonded assembly inlet air compartment, and air enters turbo-machine by air inlet pipe.Admission port and air nozzle are all slightly to main cabin direction, the air that admission port will suck above the aircraft in a large number when rotatable cabin rotates makes infrabar center of formation above the aircraft, air nozzle makes the aircraft below form an anticyclonic pressure center to a large amount of air of aircraft below ejection simultaneously, can make aircraft take off vertically or hover aloft thereby produce lift.The air nozzle opening direction is slightly to main cabin direction, the rotation rudder plate makes rudder plate stop that the part of air nozzle ejection is jet, the jet rudder plate that can promote is to the opposite direction rotation of rotation wing hand of rotation, rudder plate passes to main cabin by S. A. with thrust makes main cabin keep static relatively when rotatable cabin rotates, otherwise can make main cabin along with the aircraft flight direction is adjusted in the rotatable cabin rotation.
By the vertical takeoff and landing of the utility model design-calculated jet plane, suspend in the air and the mode by rotation technical characterictic such as turns to the manoevreability of aircraft is had to the utmost to improve.
Description of drawings
But Fig. 1 is the birds-eye view above this rotation wing vertical takeoff and landing jet plane.
But Fig. 2 is the lateral plan of A-B direction among this rotation wing vertical takeoff and landing jet plane Fig. 1.
But Fig. 3 is the section drawing of C-D direction among this rotation wing vertical takeoff and landing jet plane Fig. 1
The specific embodiment
Comprise the rotation wing 1, admission port 2,3, air inlet gas cabin 4, jet gas cabin 5, air nozzle 6,7, turbo-machine 8,9, bearing 11,12,13,14,15,16,17,18, main cabin 21, turbo-machine air inlet pipe 22,23,24,25, turbo-machine gas ejector pipe 26,27,28,29, jet valve 31,32,33,34, motor 41,44,47, S. A. 42,45,48, rudder plate 43,46,49; Also comprise: inlet air compartment 4 and thrust unit 5 are collectively referred to as rotatable cabin 1; Main cabin 21 only contacts at bearing 11,12,13,14,15,16,17,18 places with rotatable cabin 1; Rotatable cabin 1 relies on bearing 11,12,13,14,15,16,17,18 to be suspended on 21 peripheries, main cabin; Rudder plate 43,46,49 is rotated by the rotary power of the motor 41,44,47 that transmitted by S. A. 42,45,48.
Rotatable cabin 1 is connected with 4 groups of 8 bearings 11,12,13,14,15,16,17,18 with main cabin, and rotatable cabin 1 can be done in 21 peripheries, main cabin and horizontally rotate. Gas ejector pipe 26,27,28 and turbo-machine 8,9 join the gas importing thrust unit 5 of turbo-machine 8,9 ejections is back by air nozzle 6,7 ejections, air nozzle 6,7 jet promotion rotatable cabin 1 rotations, admission port 2,3 opening directions are opposite with air nozzle 6,7 direction directions, admission port 2,3 opening directions forward when rotatable cabin 1 rotation, air pours into and admission port 2,3 bonded assembly inlet air compartments 5, and air enters turbo-machine 8,9 by air inlet pipe 22,23,24,25.The quantity of admission port 2,3 and air nozzle 6,7 should decide according to the jet ability and the needs amount of air of turbo-machine 8,9, but should note the symmetry that distributes. Admission port 2,3 and air nozzle 6,7 are all slightly to main cabin 21 directions, the air that admission port 2,3 will suck above the aircraft in a large number when rotatable cabin 1 rotation makes infrabar center of formation above the aircraft, air nozzle 6,7 makes the aircraft below form an anticyclonic pressure center to a large amount of air of aircraft below ejection simultaneously, can make aircraft take off vertically or hover aloft thereby produce lift.Air nozzle 6,7 opening directions are slightly to main cabin 21 directions, rudder plate 43,46,49 with S. A. 42,45,48 connect, S. A. 42,45,48 with motor 41,44,47 connect, motor 41,44,47 can drive rudder plate 43,46,49 rotations, rotation rudder plate 43,46,49 make rudder plate 43,46,49 stop air nozzle 6, the part of 7 ejections is jet, jet meeting promotes rudder plate 43,46,49 to the opposite direction rotation of the rotation wing 1 hand of rotation, rudder plate 43,46,49 by S. A. 42,45,48 pass to main cabin 21 with thrust makes main cabin 21 keep static relatively when rotatable cabin 1 rotates, otherwise can make main cabin 21 along with the aircraft flight direction is adjusted in rotatable cabin 1 rotation. Gas ejector pipe 26,27,28,29 by valve 31,32,33,34 controls, is opened when aircraft need take off vertically and is led to the valve 31,34 that rotates the wing, and open valve 32,33 when aircraft need fly forward respectively, for aircraft provides the power of flight forward.
Claims (1)
1. but a rotation wing vertical takeoff and landing jet plane comprises the rotation wing (1), admission port (2,3), air inlet gas cabin (4), jet gas cabin (5), air nozzle (6,7), turbo-machine (8,9), bearing (11,12,13,14,15,16,17,18), main cabin (21), turbo-machine air inlet pipe (22,23,24,25), turbo-machine gas ejector pipe (26,27,28,29), jet valve (31,32,33,34), motor (41,44,47), S. A. (42,45,48), rudder plate (43,46,49); It is characterized in that: inlet air compartment (4) and thrust unit (5) are collectively referred to as rotatable cabin (1); Main cabin (21) has only been located to contact at bearing (11,12,13,14,15,16,17,18) with rotatable cabin (1); Rotatable cabin (1) relies on bearing (11,12,13,14,15,16,17,18) to be suspended on periphery, main cabin (21); Rudder plate (43,46,49) is rotated by the rotary power of the motor (41,44,47) that transmitted by S. A. (42,45,48).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201351471U CN201357943Y (en) | 2008-09-01 | 2008-09-01 | Rotary-wing vertical takeoff and landing jet aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CNU2008201351471U CN201357943Y (en) | 2008-09-01 | 2008-09-01 | Rotary-wing vertical takeoff and landing jet aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201357943Y true CN201357943Y (en) | 2009-12-09 |
Family
ID=41423705
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CNU2008201351471U Expired - Fee Related CN201357943Y (en) | 2008-09-01 | 2008-09-01 | Rotary-wing vertical takeoff and landing jet aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN201357943Y (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102120490A (en) * | 2010-01-11 | 2011-07-13 | 刘跃东 | Wind tunnel type aircraft |
| CN108609183A (en) * | 2016-12-11 | 2018-10-02 | 梁韵琳 | Aerial spray |
| CN110254707A (en) * | 2019-07-03 | 2019-09-20 | 杨德安 | A kind of umbrella resistance VTOL jet airplane |
-
2008
- 2008-09-01 CN CNU2008201351471U patent/CN201357943Y/en not_active Expired - Fee Related
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102120490A (en) * | 2010-01-11 | 2011-07-13 | 刘跃东 | Wind tunnel type aircraft |
| CN108609183A (en) * | 2016-12-11 | 2018-10-02 | 梁韵琳 | Aerial spray |
| CN110254707A (en) * | 2019-07-03 | 2019-09-20 | 杨德安 | A kind of umbrella resistance VTOL jet airplane |
| CN110254707B (en) * | 2019-07-03 | 2024-05-31 | 杨德安 | Umbrella-resistance vertical take-off and landing jet aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| DD01 | Delivery of document by public notice |
Addressee: Ye Feng Document name: Notification to Pay the Fees |
|
| C17 | Cessation of patent right | ||
| CF01 | Termination of patent right due to non-payment of annual fee |
Granted publication date: 20091209 Termination date: 20120901 |