CN2767323Y - Float bowl type loop umbrella one-seater aerobat - Google Patents
Float bowl type loop umbrella one-seater aerobat Download PDFInfo
- Publication number
- CN2767323Y CN2767323Y CN 200420054078 CN200420054078U CN2767323Y CN 2767323 Y CN2767323 Y CN 2767323Y CN 200420054078 CN200420054078 CN 200420054078 CN 200420054078 U CN200420054078 U CN 200420054078U CN 2767323 Y CN2767323 Y CN 2767323Y
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- aircraft
- umbrella
- fuselage
- aircraft fuselage
- utility
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Abstract
The utility model relates to a one-man aircraft of a float drum type loop umbrella. A dynamic force mechanism of the aircraft is arranged in an aircraft fuselage, and a drive shaft which is arranged at the top part of the aircraft fuselage is connected to an umbrella hub. Wing propeller blades are uniformly distributed and fixed on the umbrella hub in the shape of a circumferential array, and the lower end of the wing propeller blades is connected with a loop. Both sides of the middle part of the aircraft fuselage are provided with symmetrical floating drums which are parallel to each other, a propelling duct is fixed at the top part of the tail end of each floating drum and a motor with a screw propeller is arranged in each propelling duct. Both sides of the bottom end of the aircraft fuselage are provided with a landing gear of the aircraft fuselage. 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
Technical field
The utility model relates to a kind of single airflight vehicle, especially can vertical takeoff and landing, and the vehicle that can aloft fly.
Background technology
At present, known early stage individual lift device subject matter is under power, and Power train is undesirable, and sensor and automatic control technology are immature at that time.Modern ordinary fixed wing individual lift device takes off to land and 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 individual lift device 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 pontoon type circuit umbrella individual lift device 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 actuating unit of aircraft is installed in fuselage interior, the fuselage top is equipped with transmission shaft, transmission shaft is connected with the umbrella hub, wing blade is circumference array shape and is evenly distributed and is packed on the umbrella hub, the wing blade lower end is connected with circuit, and the waist both sides are equipped with the floating drum of parallel symmetry, and floating drum tail end top is fixed with the propelling duct, the electrical motor that has screw propeller is installed in it, and fuselage bottom bilateral symmetry is equipped with aircraft landing gear.
The beneficial effects of the utility model are:
1, anywhere vertical takeoff and landing, hover, noise is very low during orbit, and is 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 duct umbrella benefits to aircraft flight and aviator's safety, if high aerial just in case break down, the rotation of duct umbrella 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, 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 utility model is a kind of rational in infrastructure, design ingenious, function admirable, convenient and practical individual lift device.
Description of drawings:
Fig. 1 is a structural representation of the present utility model;
Fig. 2 is a three-dimensional view of the present utility model.
The specific embodiment
Below in conjunction with accompanying drawing and example the utility model is described in further details.
By Fig. 1-Fig. 2 as can be known the utility model be: the actuating unit 13 that aircraft is installed in fuselage 1 inside, fuselage 1 top is equipped with transmission shaft 12, transmission shaft 12 is connected with umbrella hub 4, wing blade 3 is circumference array shape and is evenly distributed and is packed on the umbrella hub 4, wing blade 3 lower ends are connected with circuit 2, both sides, fuselage 1 middle part are equipped with the floating drum 6 of parallel symmetry, floating drum 6 tail end tops are fixed with and advance duct 7, the electrical motor 10 that has screw propeller 9 is installed in it, and fuselage 1 bottom bilateral symmetry is equipped with aircraft landing gear 8.
The utility model fuselage 1 inside is equipped with aircraft actuating unit 13, the top install by circuit 2, wing blade 3, umbrella hub 4, the flight that the circuit lifting parachute that screw propeller 5 constitutes is mainly aircraft provides enough lift, power fuel and pertinent instruments equipment can be deposited in floating drum 6 inside that install fuselage 1 both sides, floating drum 6 tail end tops are equipped with and advance duct 7, its inside is made of electrical motor 10 and thrust screw propeller 9, in the aircraft traveling process, provide preceding action edge for aircraft, alighting gear 8 is positioned at fuselage 1 bottom, provides a supporting role when the aircraft grounding and landing.
Claims (1)
1, a kind of pontoon type circuit umbrella individual lift device, comprise body, the aircraft actuating unit, it is characterized in that: the actuating unit (13) that aircraft is installed in fuselage (1) inside, fuselage (1) top is equipped with transmission shaft (12), transmission shaft (12) is connected with umbrella hub (4), wing blade (3) is circumference array shape and is evenly distributed and is packed on the umbrella hub (4), wing blade (3) lower end is connected with circuit (2), both sides, fuselage (1) middle part are equipped with the floating drum (6) of parallel symmetry, floating drum (6) tail end top is fixed with and advances duct (7), the electrical motor (10) that has screw propeller (9) is installed in it, and fuselage (1) bottom bilateral symmetry is equipped with aircraft landing gear (8).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420054078 CN2767323Y (en) | 2004-12-28 | 2004-12-28 | Float bowl type loop umbrella one-seater aerobat |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420054078 CN2767323Y (en) | 2004-12-28 | 2004-12-28 | Float bowl type loop umbrella one-seater aerobat |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2767323Y true CN2767323Y (en) | 2006-03-29 |
Family
ID=36681183
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420054078 Expired - Fee Related CN2767323Y (en) | 2004-12-28 | 2004-12-28 | Float bowl type loop umbrella one-seater aerobat |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2767323Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102030106A (en) * | 2010-11-30 | 2011-04-27 | 杨茂亮 | Omnidirectional traction type rotor reconnaissance aircraft and system thereof |
| CN105814414A (en) * | 2013-12-17 | 2016-07-27 | 罗伯特·博世有限公司 | Pressure sensor device, air-mass-flow measurement device, air-mass-flow measurement system, and pressure measurement method |
-
2004
- 2004-12-28 CN CN 200420054078 patent/CN2767323Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102030106A (en) * | 2010-11-30 | 2011-04-27 | 杨茂亮 | Omnidirectional traction type rotor reconnaissance aircraft and system thereof |
| CN105814414A (en) * | 2013-12-17 | 2016-07-27 | 罗伯特·博世有限公司 | Pressure sensor device, air-mass-flow measurement device, air-mass-flow measurement system, and pressure measurement method |
| CN105814414B (en) * | 2013-12-17 | 2020-01-14 | 罗伯特·博世有限公司 | Pressure sensor device, air quality measuring system and pressure measuring method |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| C19 | Lapse of patent right due to non-payment of the annual fee | ||
| CF01 | Termination of patent right due to non-payment of annual fee |