CN105314089A - Wing - Google Patents
Wing Download PDFInfo
- Publication number
- CN105314089A CN105314089A CN201410381589.4A CN201410381589A CN105314089A CN 105314089 A CN105314089 A CN 105314089A CN 201410381589 A CN201410381589 A CN 201410381589A CN 105314089 A CN105314089 A CN 105314089A
- Authority
- CN
- China
- Prior art keywords
- wing
- air intake
- hollow
- blower fan
- radial air
- 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.)
- Pending
Links
Landscapes
- Wind Motors (AREA)
Abstract
The invention provides a wing and belongs to aircraft parts. Flexible skin of the wing is movable, meanwhile, the wing is provided with a wing blowing mechanism, the lift is enhanced in the take-off and landing process of an aircraft, the running distance is reduced, and the wing can be widely applied to small fixed wing aircrafts such as small fixed wing airplanes, sport planes and delta-winged aircrafts, aerocars, airships and other amphibians and triphibians.
Description
Technical field:
A kind of wing, belongs to aircraft components field, particularly relates to a kind of covering movable, has again the wing blowing wing mechanism.
Background technology:
Some small-sized aerial crafts are as small-sized fixed wing aircraft, sport plane, delta wing etc., low-altitude low-speed, if have complete machine parachute, safety can be better, but it is long also to there is the landing run that takes off, and needs the shortcoming in certain place, we will blow wing mechanism and flexible covering follow mechanism is added on wing for this reason, reach the object of lift-rising for this reason, make it not need large place or airport, be also suitable for short take-off and landing (STOL) waterborne.
Summary of the invention:
Goal of the invention:
A kind of wing, will blow wing mechanism and flexible covering follow mechanism is installed on it, and to reach the lift-rising in landing process, realize the object of short take-off and landing (STOL).This wing configuration is simple, can improve the performance of the low-altitude low-speed aircraft such as small-sized fixed-wing, sport plane, delta wing, make it no longer need airport or larger take-off venue.
The present invention is achieved in that the wing-body of a kind of wing by hollow, belt flexible covering, motorized pulleys, tension wheel, wing backplate, radial air intake blower fan, wing flap, electro-thermal deicing device, secondary battery, electricity adjusts device, receiver forms, and it is characterized in that: tension wheel is arranged on the rear portion of hollow wing-body, electric roller is arranged on the front portion of hollow wing-body, and belt flexible covering is enclosed within tension wheel, hollow wing-body, the outside of motorized pulleys three combination, wing protection plate cover is in the front portion of belt flexible covering and bottom, whole wing profile is aerofoil profile shape, wing backplate front lower portion has horizontal stripe shape induction opening, there is radial air intake blower fan wing backplate inside, its induction opening is corresponding with the horizontal stripe shape induction opening that wing backplate front lower portion has, and the air gate of radial air intake blower fan corresponds to the gap between wing backplate and belt flexible covering, electro-thermal deicing device, secondary battery, electricity adjusts device, receiver is arranged on the inside of hollow wing-body, radial air intake blower fan drive motor, electro-thermal deicing device, motorized pulleys, secondary battery, electricity adjusts device, receiver electrically connects, wing flap is connected with tension wheel, and the radial air intake blower fan be contained in wing backplate can be cross flow fan also can be common centrifugal blower, but the most applicable with radial air intake blower fan, motorized pulleys are that drums inside is satisfied with by motor, through the motorized pulleys that gear cluster drives.
The advantage of this programme is: the gap between wing backplate and covering can be opened and also can be driveed at rear portion at the middle part of wing, take off, radial air intake blower fan action when landing, blow the upper surface of wing, flexible covering is servo-actuated with air-flow backward, it is very important for can realizing lift-rising, short take-off and landing (STOL), fixed wing aircraft, sport plane, fixed-wing unmanned plane and delta-winged aircraft for small-sized single seat, two-seater and the short take-off and landing (STOL) such as hovercar, ship, starts to dissolve ice and snow and use when electro-thermal deicing device is freezed in winter.
Accompanying drawing illustrates:
The front elevation of a kind of wing of Fig. 1
The birds-eye view of a kind of wing of Fig. 2
The schematic diagram (three-view diagram) of Fig. 3 wing backplate
The schematic diagram (facing and birds-eye view) of the radial air intake blower fan of Fig. 4
In figure: the wing-body of 1 hollow, 2 belt flexible coverings, 3 motorized pulleys, 4 tension wheels, 5 radial air intake blower fans, 6 wing backplates, 7 wing flaps, 8 electro-thermal deicing devices, 9 secondary battery, 10 electricity adjust device, 11 receivers, 12 tightening devices, 13 Connection Cards, 14 gaps, 15 radial air intake blower fan drive motor, 16 bar shaped induction openings, 17 radial air intake blower fan induction openings, 18 radial air intake blower fan air gates, 19 radial air intake blower fan impellers, 20 radial air intake blower fan engine housings
Detailed description of the invention:
Embodiment 1:
The wing-body that 3 electric rollers are arranged on 1 hollow is anterior, 4 tension wheels are connected to the rear portion of the wing-body of 1 hollow through 12 tightening devices, 2 belt flexible coverings are enclosed within the wing-body of 1 hollow, 3 motorized pulleys, the outside of 4 tension wheel three combinations, the wing-body of 1 hollow, 3 motorized pulleys connect by 13 Connection Cards, the wing-body that 6 wing backplates are fixed on 1 hollow is anterior, 5 radial air intake blower fans, 15 radial air intake blower fan drive motor are installed together, it is inner that 5 radial air intake blower fans are arranged on 6 wing backplates, its induction opening is corresponding with the bar shaped induction opening that 6 wing backplates are opened, the air gate of the corresponding 5 radial air intake blower fans in 14 gaps between 6 wing backplates with 2 belt flexible coverings, 7 wing flaps and 4 tension wheels link together, 8 electro-thermal deicing devices, 9 secondary battery, 10 electricity adjust device, the wing-body that 11 receivers are arranged on 1 hollow is inner, 8 electro-thermal deicing devices, 9 secondary battery, 10 electricity adjust device, 11 receivers, 3 motorized pulleys, 15 radial air intake blower fan drive motor electrically connect, after 11 receivers receive signal, 3 motorized pulleys rotation drive 2 belt flexible coverings move backward, 5 radial air intake blower fans rotate and produce the upper surface generation lift that air-flow blows 2 belt flexible coverings simultaneously, make the wing lift-rising taken off in descent.
Claims (1)
1. a wing is by the wing-body of hollow, belt flexible covering, motorized pulleys, tension wheel, wing backplate, radial air intake blower fan, wing flap, electro-thermal deicing device, secondary battery, electricity adjusts device, receiver forms, and it is characterized in that: tension wheel is arranged on the rear portion of hollow wing-body, motorized pulleys are arranged on the front portion of hollow wing-body, and belt flexible covering is enclosed within tension wheel, hollow wing-body, the outside of motorized pulleys three combination, wing protection plate cover is in the front portion of belt flexible covering and bottom, whole wing profile is aerofoil profile shape, wing backplate front lower portion has horizontal stripe shape induction opening, radial air intake blower fan is had in wing backplate, its induction opening is corresponding with the horizontal stripe shape induction opening that wing backplate front lower portion has, and the air gate of radial air intake blower fan corresponds to the gap between wing backplate and belt flexible covering, electro-thermal deicing device, secondary battery, electricity adjusts device, receiver is arranged on the inside of hollow wing-body, radial air intake blower fan drive motor, electro-thermal deicing device, motorized pulleys, secondary battery, electricity adjusts device, receiver electrically connects, and wing flap is connected with tension wheel.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410381589.4A CN105314089A (en) | 2014-07-29 | 2014-07-29 | Wing |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201410381589.4A CN105314089A (en) | 2014-07-29 | 2014-07-29 | Wing |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105314089A true CN105314089A (en) | 2016-02-10 |
Family
ID=55242599
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201410381589.4A Pending CN105314089A (en) | 2014-07-29 | 2014-07-29 | Wing |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN105314089A (en) |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3837812A1 (en) * | 1988-11-08 | 1990-05-10 | Juergen Schoenell | Wing (mainplane) |
| US5590854A (en) * | 1994-11-02 | 1997-01-07 | Shatz; Solomon | Movable sheet for laminar flow and deicing |
| RU2072942C1 (en) * | 1993-02-02 | 1997-02-10 | Владимир Николаевич Желтко | Aircraft wing |
| CN102267559A (en) * | 2011-04-24 | 2011-12-07 | 王志成 | Moving-surface aerofoil |
| CN202071984U (en) * | 2011-05-02 | 2011-12-14 | 刘自拔 | Movable wing airplane with wind wheels at leading edges |
| CN204110354U (en) * | 2014-07-29 | 2015-01-21 | 陈志石 | A kind of wing |
-
2014
- 2014-07-29 CN CN201410381589.4A patent/CN105314089A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE3837812A1 (en) * | 1988-11-08 | 1990-05-10 | Juergen Schoenell | Wing (mainplane) |
| RU2072942C1 (en) * | 1993-02-02 | 1997-02-10 | Владимир Николаевич Желтко | Aircraft wing |
| US5590854A (en) * | 1994-11-02 | 1997-01-07 | Shatz; Solomon | Movable sheet for laminar flow and deicing |
| CN102267559A (en) * | 2011-04-24 | 2011-12-07 | 王志成 | Moving-surface aerofoil |
| CN202071984U (en) * | 2011-05-02 | 2011-12-14 | 刘自拔 | Movable wing airplane with wind wheels at leading edges |
| CN204110354U (en) * | 2014-07-29 | 2015-01-21 | 陈志石 | A kind of wing |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| WO2015012935A3 (en) | Vertical takeoff and landing (vtol) air vehicle | |
| CN110683045B (en) | Aircraft with a plurality of aircraft body | |
| CN111498109A (en) | Vertical take-off and landing aircraft | |
| CN106043689A (en) | Vertical take-off auxiliary system for top-mounted fixed-wing aircraft | |
| CN107963209B (en) | Tandem wing rotor unmanned aerial vehicle that verts | |
| CN103318411B (en) | Fixed-wing vertical take-off and landing aircraft (VTOL aircraft) | |
| CN204916182U (en) | High -speed vertical take -off and landing aircraft | |
| WO2014209198A4 (en) | Propulsion system for an aerial vehicle | |
| CN104401485A (en) | Four-wing unmanned aerial vehicle and control method thereof | |
| CN204210731U (en) | Autogyro | |
| CN204110354U (en) | A kind of wing | |
| CN105329056A (en) | Wheel type rotor wing vehicle | |
| CN106864744A (en) | A kind of co-axial rotor variant vertically taking off and landing flyer | |
| CN103264773A (en) | Seasonal icing test bench | |
| CN204021250U (en) | A kind of have the round wing unmanned plane blowing wing mechanism | |
| CN204548505U (en) | A kind of alternating expression four rotor flying motor | |
| CN105314089A (en) | Wing | |
| CN102233950A (en) | Vertical takeoff and landing miniature aircraft | |
| CN105270622B (en) | A kind of compound wing aircraft in the band upper counterangle | |
| CN104908942A (en) | Vertical take-off and landing light airplane | |
| CN104992586A (en) | Airplane system capable of realizing flight experience | |
| CN203075664U (en) | Flying machine | |
| RU179060U1 (en) | Unmanned aerial vehicle vertical takeoff and landing | |
| CN104548616B (en) | A kind of telecontrolled aircraft | |
| CN104787324A (en) | Lift force generator |
Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20160210 |
|
| RJ01 | Rejection of invention patent application after publication |