CN2748384Y - One-man flight vehicle with coaxial culvert and umbrella paddle - Google Patents
One-man flight vehicle with coaxial culvert and umbrella paddle Download PDFInfo
- Publication number
- CN2748384Y CN2748384Y CN 200420063547 CN200420063547U CN2748384Y CN 2748384 Y CN2748384 Y CN 2748384Y CN 200420063547 CN200420063547 CN 200420063547 CN 200420063547 U CN200420063547 U CN 200420063547U CN 2748384 Y CN2748384 Y CN 2748384Y
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- CN
- China
- Prior art keywords
- shrouded
- parachute
- culvert
- umbrella
- frame
- 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
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- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
Abstract
The utility model discloses a coaxial one-man flight vehicle with a culvert and an umbrella paddle. Both sides of a machine frame is provided with joy sticks which are symmetrical and are connected with an operating mechanism which is arranged in the machine frame, and the top end position of the machine frame is provided with a paddle shaft which is connected with the operating mechanism, and is provided with a culvert umbrella shaft. The culvert umbrella leaf is fixedly arranged at the top portion of the culvert umbrella shaft, and the lower end position of the culvert umbrella leaf is connected with the culvert. The paddle shaft below the culvert umbrella leaf is fixedly provided with a screw propeller. The coaxial one-man flight vehicle with a culvert and an umbrella paddle has main purposes of photography in the sky, advertisement propaganda, communication relay, pursuing and capturing escaped criminals, traffic guidance, antiterrorism battle, scouting enemy situations, etc.
Description
Affiliated 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 shrouded parachute-propeller coaxial type one-man aircraft 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: frame both sides be equipped be arranged on frame in the joystick of the symmetry that is connected of steering unit, there is the slurry axle that links to each other with steering unit at position, frame top, be equipped with shrouded parachute axis on it, shrouded parachute blade is packed in the shrouded parachute axis top, the shrouded parachute blade lower end part is connected with the letter road, is fixed with screw propeller on the slurry axle of shrouded parachute blade below.
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 duct umbrella, safety to aircraft flight and aviator benefits, if it is high aerial just in case break down, the rotation of duct umbrella 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 the 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, various vertical takeoff and landing duct umbrella oar close coupled types 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 individual lift device.
Description of drawings
Fig. 1 is the utility model structural representation;
Fig. 2 is the birds-eye view of Fig. 1;
Fig. 3 is the cutaway view of A-A among Fig. 1;
Fig. 4 is the lateral plan of Fig. 1
The specific embodiment
Below in conjunction with drawings and Examples the utility model is further described.
By Fig. 1-Fig. 4 as can be known the utility model be: frame 1 both sides be equipped be arranged on frame in the joystick 6 of the symmetry that is connected of steering unit, there is the slurry axle 5 that links to each other with steering unit at position, frame top, be equipped with shrouded parachute axis 4 on it, shrouded parachute blade 7 is packed in shrouded parachute axis 4 tops, shrouded parachute blade 7 lower end parts are connected with letter road 2, are fixed with screw propeller 3 on the slurry axle 5 of shrouded parachute blade 7 belows.
Both sides, described frame 1 top are equipped with the airborne illuminating lamp 9 of symmetry.
Be positioned at the airborne Fuel Tank 10 that airborne illuminating lamp 9 belows are packed in the frame both sides.
In Fig. 1, letter road 2 links to each other with shrouded parachute blade 7, letter road 2, slurry axle 5, shrouded parachute axis 4, shrouded parachute blade 7 is positioned at frame 1 top, slurry axle 5 is connected with frame 1 in-to-in transmission device and carries out anticlockwise motion, airborne illuminating lamp 10 is packed in frame 1 both sides, airborne Fuel Tank 11 is positioned at airborne illuminating lamp 10 belows, and be packed in frame 1 both sides, joystick 6 is connected with frame 1 and is packed in frame 1 both sides, joystick 6 is by letter road 2 and the shrouded parachute blade 7 of frame 1 in-to-in transmission device to frame 1 top, screw propeller in the A-A is controlled, frame support 8 is connected with frame 1 and is positioned at frame below, is assemblied in scroll wheel 11 on the frame support 8 has guaranteed aircraft in aircraft takeoff and landing stationarity.
In embodiment illustrated in fig. 2, screw propeller 3 is positioned at 2 inboards, letter road, and screw propeller 3 is positioned at shrouded parachute blade 7 belows, and screw propeller 3 is the anticlockwise direction rotation when rotating, and shrouded parachute blade 7 is connected with letter road 2.
In the embodiment shown in fig. 3, slurry axle 5 outsides at shrouded parachute axis 4, letter road 2 links to each other with shrouded parachute axis 4 by shrouded parachute blade 7, the rotation of shrouded parachute axis 4 drives letter road 2 and is attached thereto the shrouded parachute blade 7 that connects carries out the clockwise direction rotation, screw propeller 3 links to each other with slurry axle 5, slurry axle 5 drives screw propeller 3 and carries out the anticlockwise direction rotation by rotating, and shrouded parachute blade 7 is connected with letter road 2, and letter road 2 is connected with shrouded parachute blade 7 and is positioned at screw propeller 3 tops.
In the embodiment shown in fig. 4, duct 2 is connected with shrouded parachute axis 4 and is packed on the frame 1, slurry axle 5 is connected with shrouded parachute axis 4, shrouded parachute blade 7 is connected with letter road 2, shrouded parachute blade 7 is connected with shrouded parachute axis 4 simultaneously, joystick 6 is connected the rotation of rotation and shrouded parachute axis 4 of control slurry axle 5 to reach the purpose of controlling aircraft flight with driving device in the frame 1, frame support 8 is connected with frame 1, and frame is played support and stabilization.
Claims (4)
1, a kind of shrouded parachute-propeller coaxial type one-man aircraft, comprise frame (1), slurry axle (5), screw propeller (3), it is characterized in that a frame (1) both sides are equipped with the joystick (6) of the symmetry that is connected with the steering unit that is arranged in the frame, there is the slurry axle (5) that links to each other with steering unit at position, frame top, be equipped with shrouded parachute axis (4) on it, shrouded parachute blade (7) is packed in shrouded parachute axis (4) top, shrouded parachute blade (7) lower end part is connected with letter road (2), is fixed with screw propeller (3) on the slurry axle (5) of shrouded parachute blade (7) below.
2, want 1 described shrouded parachute-propeller coaxial type one-man aircraft it is characterized in that according to right: both sides, frame (1) top are equipped with the airborne illuminating lamp (9) of symmetry.
3, shrouded parachute-propeller coaxial type one-man aircraft according to claim 1 is characterized in that: be positioned at the airborne Fuel Tank (10) that airborne illuminating lamp (9) below is packed in the frame both sides
4, shrouded parachute-propeller coaxial type one-man aircraft according to claim 1 is characterized in that: frame (1) below is equipped with the fuselage support (8) that has scroll wheel (11).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420063547 CN2748384Y (en) | 2004-10-12 | 2004-10-12 | One-man flight vehicle with coaxial culvert and umbrella paddle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 200420063547 CN2748384Y (en) | 2004-10-12 | 2004-10-12 | One-man flight vehicle with coaxial culvert and umbrella paddle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN2748384Y true CN2748384Y (en) | 2005-12-28 |
Family
ID=35719876
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 200420063547 Expired - Fee Related CN2748384Y (en) | 2004-10-12 | 2004-10-12 | One-man flight vehicle with coaxial culvert and umbrella paddle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN2748384Y (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102806994A (en) * | 2011-05-31 | 2012-12-05 | 王略 | Ultra-light single-person deceleration tilting type coaxial helicopter |
| WO2016037543A1 (en) * | 2014-09-11 | 2016-03-17 | 周承岗 | Suction-cup-type aircraft |
-
2004
- 2004-10-12 CN CN 200420063547 patent/CN2748384Y/en not_active Expired - Fee Related
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN102806994A (en) * | 2011-05-31 | 2012-12-05 | 王略 | Ultra-light single-person deceleration tilting type coaxial helicopter |
| WO2016037543A1 (en) * | 2014-09-11 | 2016-03-17 | 周承岗 | Suction-cup-type aircraft |
| CN105460216A (en) * | 2014-09-11 | 2016-04-06 | 周承岗 | Sucker type aircraft |
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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 |