CN2753674Y - Dish aircraft - Google Patents

Dish aircraft Download PDF

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Publication number
CN2753674Y
CN2753674Y CN 200420063681 CN200420063681U CN2753674Y CN 2753674 Y CN2753674 Y CN 2753674Y CN 200420063681 CN200420063681 CN 200420063681 CN 200420063681 U CN200420063681 U CN 200420063681U CN 2753674 Y CN2753674 Y CN 2753674Y
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CN
China
Prior art keywords
aircraft
umbrella
fixed
aircraft body
rotor
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
Application number
CN 200420063681
Other languages
Chinese (zh)
Inventor
王忠信
青泉
孙树生
吴世海
丛林枝
Original Assignee
王忠信
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by 王忠信 filed Critical 王忠信
Priority to CN 200420063681 priority Critical patent/CN2753674Y/en
Application granted granted Critical
Publication of CN2753674Y publication Critical patent/CN2753674Y/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Abstract

The utility model relates to a dish aircraft. The position of the upper end of the outer side wall of an aircraft body is provided with a shaft sleeve on which umbrella-shaped rotor wings are fixed, and the bottom edge of each umbrella-shaped rotor wing is provided with a support frame of a rotor wing. The position of the lower end of the aircraft body is provided with screw propellers, the position of the top end of the aircraft body is provided with a seat cabin cover in which a driver seat is arranged and three leg type landing frames are fixed at the bottom part of the aircraft body. The utility model has the main application in aerial photography, advertisement propaganda, communication relay, escaped criminal pursuit, traffic guidance, counter-terrorism warfare, military intelligence reconnaissance, etc.

Description

Disc-shaped flying craft
Technical field
The utility model relates to a kind of airflight vehicle, especially can vertical takeoff and landing, and the vehicle that can aloft fly.
Background technology
At present, known early stage vertically taking off and landing flyer subject matter is that Power train is undesirable, and sensor and automatic control technology are immature at that time.Modern ordinary fixed rotor aircraft takes off to land needs special-purpose airfield runway, needs higher speed and could produce enough lift, causes the generation when taking off landing of about 50% left and right sides aircraft accident, and park occupied ground on ground very big.Modern common rotor craft great majority adopt single rotor magnetic tape trailer paddle structure of helicopter.The rotor of high speed revolution is fatal threats to the personnel of disembarking.The blade of high speed revolution also is easy to run into object and produces aircraft accident; Air resistance and induced drag cause flying speed lower more greatly.
Summary of the invention
The technical problems to be solved in the utility model is: overcome that weak point provides a kind of disc-shaped flying craft that all can be used as the vehicle in land, sea and air in the above-mentioned technology.
The technical scheme that its technical matters that solves the utility model adopts is: the position, lateral wall upper end of a body is equipped with axle sleeve, be fixed with the umbrella rotor on it, umbrella rotor base is provided with the rotor bracing frame, the body lower end part is fixed with screw propeller, position, body top is provided with a storehouse cover, driver's seat is installed in it, and organism bottom is with three leg type alighting gears are housed.
The beneficial effects of the utility model are:
1, anywhere vertical takeoff and landing, hover, spiral, noise in flight is very low, disguised very good;
2, it has fast, the mobility strong of speed, can do various aerobatics;
3, flight efficiency height, and fuel saving, so easy maintenance is economical and practical;
4, comformability is strong; Adapt to the city, country, factory, seashore, naval vessels, grassland, high mountain, the vertical takeoff and landing flight that express highway etc. are local;
5, safe and reliable, the design of umbrella formula rotor, safety to aircraft flight and aviator benefits, if it is high aerial just in case break down, the rotation of umbrella formula rotor with aircraft and occupant safety send ground back to, during low-latitude flying, break down and can adopt zero catapult technique that aircraft is served certain altitude, by umbrella formula rotor with aircraft and occupant safety send ground back to;
6, be the vehicle that save time most and increase work efficiency, and take advantage of a commercial air flights to compare not to be subjected to the flight time limitation, do not have the time of waiting, transferring to the vehicle.
7, various disc-shaped flying crafts series aircraft will become the most attractive a kind of sports item, a kind of convenience that everybody likes and cheap aircraft;
8, wide application: can take photo in the sky on civilian, advertising, communication repeating, the oil pipeline supervision, the monitoring of fire flood situation pursues and captures an escaped prisoner guiding of traffic etc.; The advantage that has other vehicle to hardly match equally militarily, fight-terrorism warfare, military situation is scouted, antisubmarine clearance, the strike of all types of target, attacks armed helicopter and low-to-medium altitude cruise missile etc.The present invention is a kind of rational in infrastructure, design ingenious, function admirable, convenient and practical aircraft.
Description of drawings
Fig. 1 is the utility model structural representation;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 be Figure 1A-A cut open side figure;
The specific embodiment
Below in conjunction with drawings and Examples the utility model is further described.
By Fig. 1-Fig. 3 as can be known the utility model be: position, the lateral wall of a body 1 upper end is equipped with axle sleeve 8, be fixed with umbrella rotor 4 on it, umbrella rotor 4 bases are provided with rotor bracing frame 3, body 1 lower end part is fixed with screw propeller 6, position, body 1 top is provided with a storehouse cover 2, driver's seat 7 is installed in it, and body 1 bottom is fixed with three leg type alighting gears 5.
Umbrella rotor 4 described in the utility model plays the effect that main lift and coordinated flight of stabilized flight device and balance are provided; screw propeller 6 plays the effect that lift and controlling aircraft flight attitude are provided; seat storehouse cover 2 plays protection occupant's effect, and body 1 also plays the effect in occupant's seat storehouse, capacity weight storehouse, power system and energy storehouse except that the effect of the axle that plays umbrella rotor 4 and screw propeller 6.During aircraft flight, propeller 6 is the anticlockwise direction rotation, and umbrella rotor 4 is right-hand revolution, and three leg type alighting gears 3 are played a supporting role when aircraft lands.

Claims (1)

1, a kind of disc-shaped flying craft, comprise: body, umbrella rotor, screw propeller, it is characterized in that: the position, lateral wall upper end of body (1) is equipped with axle sleeve (8), be fixed with umbrella rotor (4) on it, umbrella rotor (4) base is provided with rotor bracing frame (3), and body (1) lower end part is fixed with screw propeller (6), and body (1) position, top is provided with a storehouse cover (2), driver's seat (7) is installed in it, and body (1) bottom is fixed with three leg type alighting gears (5).
CN 200420063681 2004-11-01 2004-11-01 Dish aircraft Expired - Fee Related CN2753674Y (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN 200420063681 CN2753674Y (en) 2004-11-01 2004-11-01 Dish aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN 200420063681 CN2753674Y (en) 2004-11-01 2004-11-01 Dish aircraft

Publications (1)

Publication Number Publication Date
CN2753674Y true CN2753674Y (en) 2006-01-25

Family

ID=35925781

Family Applications (1)

Application Number Title Priority Date Filing Date
CN 200420063681 Expired - Fee Related CN2753674Y (en) 2004-11-01 2004-11-01 Dish aircraft

Country Status (1)

Country Link
CN (1) CN2753674Y (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101927826A (en) * 2010-05-10 2010-12-29 李文奇 Rotor wing disk-shaped aviation aircraft
CN107685856A (en) * 2017-05-27 2018-02-13 北京深远世宁科技有限公司 Dish-shaped flying machine

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN101927826A (en) * 2010-05-10 2010-12-29 李文奇 Rotor wing disk-shaped aviation aircraft
CN107685856A (en) * 2017-05-27 2018-02-13 北京深远世宁科技有限公司 Dish-shaped flying machine

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Legal Events

Date Code Title Description
C14 Grant of patent or utility model
GR01 Patent grant
C17 Cessation of patent right
CF01 Termination of patent right due to non-payment of annual fee

Granted publication date: 20060125

Termination date: 20101101