CN203439260U - Composite powered wing aircraft - Google Patents
Composite powered wing aircraft Download PDFInfo
- Publication number
- CN203439260U CN203439260U CN201320479297.5U CN201320479297U CN203439260U CN 203439260 U CN203439260 U CN 203439260U CN 201320479297 U CN201320479297 U CN 201320479297U CN 203439260 U CN203439260 U CN 203439260U
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- wing
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- type power
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Abstract
The utility model relates to a composite powered wing aircraft. The composite powered wing aircraft is characterized by comprising composite powered wings, an aircraft body, a horizontal direction control rudder, a body movement engine, a wing movement engine, a control cabin and a wing fixing support, wherein the aircraft body has a structure of a jet aircraft; the horizontal direction control rudder, the body movement engine and the control cabin are arranged in the aircraft body; the composite powered wings are in a disc shape, and are fixed on the left side and the right side of the aircraft body through the wing fixing support extending out of the aircraft body; the wing movement engine is arranged below the composite powered wings. The composite powered wing aircraft provided by the utility model overcomes the aerodynamic contradictions such as the lifting power and resistance as well as disturbing force of fixed wing aircrafts and rotary wing aircrafts, has the advantages of large lifting force and small size in comparison with aircrafts with the same physical dimensions, no restrictions to take-off and land conditions, has a simple structure, is low in development and manufacture costs, can realize vertical take-off and landing as well as hovering, and can be developed to aircrafts and transport and rescue equipment of different kinds, different specifications and different purposes.
Description
Technical field
The utility model belongs to aeronautical technology field, relates to a kind of type aircraft, particularly a kind of compound type power wing aircraft.
Background technology
Wing is the key components of aircraft, is one of decisive factor of aircraft load-carrying capacity.Present generation aircraft is broadly divided into fixed wing aircraft and rotary wing aircraft two classes by wing classification.Although fixed wing aircraft has the advantages that flying height is high, speed is fast, load-carrying capacity is large, because of large heavy alerting ability and the load-carrying capacity that has limited aircraft of its volume, because it takes off, landing condition is also harsher, restricted its range of use.The maximum take-off weight that the current take-off weight the biggest in the world of tool data introduction is about fortune-20 transport plane of the current development of 600Dun， China is 220 tons, and large like this aircraft can only be in the landing of minority airport.Although rotary wing aircraft has good alerting ability, to taking off, landing, environmental requirement is loose, but exist: flying height, flying speed and maximum take-off weight be the problem such as smaller all, tool data introduction at present autogyro take-off weight the biggest in the world is no more than 30 tons, and flying height is no more than 5000m, flying speed is no more than 600 kilometers/hour.
Summary of the invention
The utility model has overcome the defect of above-mentioned existence, object is to provide and a kind ofly can has both the two advantage of fixed wing aircraft and rotary wing aircraft, make take-off weight surpass current fixed wing aircraft maximum take-off weight, flying speed realizes supersonic flight, there is vertical lift airworthiness flexibly, and volume compound type power wing aircraft little, lightweight, simple in structure.
The utility model compound type power wing aircraft content Description:
The utility model compound type power wing aircraft, it is characterized in that: by compound type power wing, body, horizontal direction, control rudder, body movement driving engine, wing motion motor, control storehouse and wing fixed support and form, body adopts the housing construction of jet plane, horizontal direction is controlled to rudder, body movement driving engine and controlled storehouse and be arranged in body, compound type power wing is disc-shape, by the wing fixed support with body extension, be fixed on the left and right sides of body, wing motion motor be arranged on compound type power wing below.
On compound type power wing, be provided with rotating circular disk, rotating circular disk is arranged on the top of casing, in casing, be provided with rotating circular disk control system, in the bottom of casing, be provided with wing motion motor, one end of transmission shaft is vertically mounted on wing motion motor, and the other end of transmission shaft passes casing and is fixedly connected with rotating circular disk.
The utility model has overcome the contradiction of the aerodynamics aspects such as fixed-wing, rotary wing aircraft lift and resistance, exciting force; Under same physical dimension, lift is large, small, and the landing condition of taking off is unrestricted; Simple in structure, exploitation and composition cost is low; Can vertical takeoff and landing, can hover; Independently lift platform and different body combinations be can make, multiple types, many specifications, multiduty aircraft and transportation, the equipment of speedily carrying out rescue work developed.
Accompanying drawing explanation
Fig. 1 is compound type power wing aircaft configuration schematic diagram;
Fig. 2 is compound type power wing aircraft lateral plan;
Fig. 3 is compound type power wing aircraft birds-eye view;
Fig. 4 is compound type power wing structural representation;
Fig. 5 is compound type power wing birds-eye view;
In figure: the 1st, compound type power wing, the 2nd, body, the 3rd, horizontal direction is controlled rudder, the 4th, body movement driving engine, the 5th, wing motion motor, the 6th, cabin, the 7th, wing fixed support, the 8th, rotating circular disk, the 9th, casing, the 10th, rotating circular disk control system, the 11st, transmission shaft.
The specific embodiment
The utility model compound type power wing aircraft is achieved in that below in conjunction with accompanying drawing and illustrates.
See Fig. 1～Fig. 3, compound type power wing aircraft is by compound type power wing 1, body 2, horizontal direction is controlled rudder 3, body movement driving engine 4, wing motion motor 5, control storehouse 6 and wing fixed support 7 compositions, body 2 adopts the housing construction of jet plane, horizontal direction is controlled to rudder 3, body movement driving engine 4 and control storehouse 6 are arranged in body 2, compound type power wing 1 is disc-shape, by the wing fixed support 7 with body 2 extensions, be fixed on the left and right sides of body 2, wing motion motor 5 be arranged on compound type power wing 1 below.
The size of controlling wing motion motor 5 revolutions, controlling movement in vertical direction state and lift by being arranged on the wing control system of controlling in storehouse 6; By horizontal direction, control rudder 3 and control aircraft horizontal motion direction; By body movement driving engine 4, control aircraft horizontal movement state.
See Fig. 4～Fig. 5, on compound type power wing 1, be provided with rotating circular disk 8, rotating circular disk 8 is arranged on the top of casing 9, and casing 9 is erecting stages of each parts on compound type power wing 1, is also lift bearing surface.In casing 9, be provided with rotating circular disk control system 10, in the bottom of casing 9, be provided with wing motion motor 5, one end of transmission shaft 11 is vertically mounted on wing motion motor 5, and the other end of transmission shaft 11 passes casing 9 and is fixedly connected with rotating circular disk 8.
The utility model compound type power wing aircraft is according to Selections from The Principle of Relativity and Bernoulli's theorem, compound type power wing adopts disc-shape structure, there are two disk effects, its mode of motion that is different from the relative wing of aircraft wing upper and lower surface air-flow of the prior art is all identical, fixed wing aircraft is rectilinearity, rotary wing aircraft is circumference type, its upper and lower aerofoil flow speed creates a difference because of wing shapes, the lift and the aerofoil contour shape that produce, body movement speed is relevant, wing motion-promotion force derives from body, the shape of wing is complicated polygon geometry.
The utility model compound type power wing aircraft, the mode of motion of the relative wing of the upper and lower aerofoil flow of wing is different, air-flow above when wing body is static is in the horizontal direction circumference type, and that air-flow below wing body is lift and the wing body section shape of static (ignoring nature wind speed) its generation is irrelevant, irrelevant with wing body horizontal motion speed.Wing body carries independent power system, and its profile is regular disc.
There is compared with prior art following feature:
1, overcome the contradiction of the aerodynamics aspects such as fixed-wing, rotary wing aircraft lift and resistance, exciting force;
2, large, the small feature of lift under same physical dimension, take and transport 1 as example, and its oad is 50 * 50 * 15M, and take-off weight is 220 tons, and the compound type power wing aircraft that oad is 20 * 50 * 15M, take-off weight can reach 450 tons; Its landing condition of taking off is unrestricted, owing to having realized lift power and horizontal motion power sets up separately, therefore can realize high speed flight at high altitude, high-altitude low-speed operations, also can realize low altitude high speed flight, low-altitude low-speed flight, have both the advantage of autogyro and jet plane;
3, simple in structure, exploitation and composition cost is low;
4, can vertical takeoff and landing, can hover;
5, independently lift platform and different body combinations be can make, multiple types, many specifications, multiduty aircraft and transportation, the equipment of speedily carrying out rescue work developed.
Claims (2)
1. a compound type power wing aircraft, it is characterized in that: be by compound type power wing (1), body (2), horizontal direction is controlled rudder (3), body movement driving engine (4), wing motion motor (5), controlling storehouse (6) and wing fixed support (7) forms, body (2) adopts the housing construction of jet plane, horizontal direction is controlled to rudder (3), body movement driving engine (4) and control storehouse (6) are arranged in body (2), compound type power wing (1) is disc-shape, by the wing fixed support (7) with body (2) extension, be fixed on the left and right sides of body (2), wing motion motor (5) be arranged on compound type power wing (1) below.
2. compound type power wing aircraft according to claim 1, it is characterized in that: on compound type power wing (1), be provided with rotating circular disk (8), rotating circular disk (8) is arranged on the top of casing (9), in casing (9), be provided with rotating circular disk control system (10), in the bottom of casing (9), be provided with wing motion motor (5), it is upper that one end of transmission shaft (11) is vertically mounted on wing motion motor (5), and the other end of transmission shaft (11) passes casing (9) and is fixedly connected with rotating circular disk (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320479297.5U CN203439260U (en) | 2013-08-07 | 2013-08-07 | Composite powered wing aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201320479297.5U CN203439260U (en) | 2013-08-07 | 2013-08-07 | Composite powered wing aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN203439260U true CN203439260U (en) | 2014-02-19 |
Family
ID=50090328
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201320479297.5U Expired - Lifetime CN203439260U (en) | 2013-08-07 | 2013-08-07 | Composite powered wing aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN203439260U (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103381887A (en) * | 2013-08-07 | 2013-11-06 | 陈海生 | Airplane with composite power wings |
-
2013
- 2013-08-07 CN CN201320479297.5U patent/CN203439260U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103381887A (en) * | 2013-08-07 | 2013-11-06 | 陈海生 | Airplane with composite power wings |
| CN103381887B (en) * | 2013-08-07 | 2015-10-28 | 陈海生 | Compound type power wing aircraft |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| AV01 | Patent right actively abandoned |
Granted publication date: 20140219 Effective date of abandoning: 20151028 |
|
| C25 | Abandonment of patent right or utility model to avoid double patenting |