CN104843184A - Personal air vehicle - Google Patents
Personal air vehicle Download PDFInfo
- Publication number
- CN104843184A CN104843184A CN201510179345.2A CN201510179345A CN104843184A CN 104843184 A CN104843184 A CN 104843184A CN 201510179345 A CN201510179345 A CN 201510179345A CN 104843184 A CN104843184 A CN 104843184A
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- main wing
- bone
- air vehicle
- wing bone
- main
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Abstract
The invention discloses a personal air vehicle, discloses a sport device challenging limit sports, and particularly relates to the personal air vehicle. Both sides of a main wing bone are each provided with a gasoline engine, and each engine is provided with a propeller; the main wing bone is provided with a main wing bone cloth cape; a tail wing bone is provided with a tail wing cloth cape; during use, a passenger body is tied firmly by a tying belt and a passenger soft seat, a passenger holds a joystick by hand, the gasoline engines are started to drive the propellers to rotate, when a certain speed is reached, air is pushed to flow downward, an overall upward pushing force is generated, and the air vehicle gets off the ground to complete taking-off. The personal air vehicle is used as the athletic sports device challenging the limit, is novel in style and strong in challenge, can bring enjoyment of flying pleasure to a sporter, has the characteristics of small volume and light weight, and does not need special specifications and large-area places. With the joystick, a vehicle body is flexible to steer. The passenger is allowed to fly with various postures, the air retention time is long, the fuel consumption is low, and the problems existing in a conventional air vehicle are solved.
Description
Technical field
What the present invention announced is the sports equipment that a kind of Challenging the Limits moves, specifically a kind of personal aircraft.
Background technology
At present in the world for personal aircraft material dynamic delta wing formula, two duct turbo types, single rocket Backpack type, the coaxial anti-paddle of overhead and the coaxial anti-paddle of lower shaft of Challenging the Limits motion.All there is many problems in these aircraft.As dynamic-delta-wing formula aircraft need the landing place of large-scale, specification.The power that two the too large needs of duct turbo type weight are powerful, and people need remain the posture of standing when carrying out motion exercise, be easy to people is felt fatigue, controlling party is to also not easily.The consumption of fuel excessive flight time of single rocket Backpack type is short.There is the difficulty in steer direction in coaxial anti-paddle, easily safety misadventure occurs.
Summary of the invention
For above-mentioned situation, the object of this invention is to provide a kind of volume little, use easy to operate personal aircraft, solve existing various aircraft Problems existing.
The present invention for the taked technical scheme that solves the problem as follows; At the middle part of body with main framing, have a main wing bone on the top of main framing, main framing and main wing bone are hinged connection.With joystick on main wing bone.With power control button on joystick.Main wing bone both sides respectively there is an engine petrol.With screw propeller on engine petrol output shaft.At the rear portion of main wing bone with tubular fuel tank.Fluffy with main wing cloth on main wing bone.Occupant's soft seat is had in main framing bottom.At main framing pars intermedia with occupant's bondage belt.In the bottom of main wing bone with empennage bone, empennage bone and main wing bone are hinged connection.With empennage cloth paulin on empennage bone.Using method of the present invention is; With bondage belt and occupant's soft seat by firm for occupant's bondage, occupant holds joystick, start engine petrol carrying screws to rotate, air flows down is promoted when reaching certain rotating speed, produce overall thrust upwards, make aircraft leave ground upwards to run, progressively open the throttle wide makes propeller speed reach faster speed, produces larger thrust and completes and take off.Wait rise to need after certain altitude to turn time, manually can adjust joystick and drive main wing bone to rotate, change engine thrust direction and complete turning action.During landing, manual motivation of adjustment control button, slowly shrinks throttle, adjusts joystick simultaneously, makes occupant be erectility, slowly lands in ground.The present invention uses as a kind of athletic sports appliance of Challenging the Limits, and novel form, challenge is strong.Can be sporter bring enjoy circle in the air happy.Its feature is that volume is little, lightweight, and its main wing skeleton is aluminum alloy manufacture.Do not need special specification and large area place.Main wing cloth paulin and empennage cloth paulin are high strength chemical fiber cloth.Make body turn to flexibly with joystick.Can realize vector propelling by changing engine thrust direction, occupant can be made to fly by multiple posture, and airborne period is long, and oil consumption is low, and safety factor is high.Two driving engines work respectively, even if one breaks down, another still can ensure that occupant safety lands.Solve existing aircraft Problems existing.
Accompanying drawing explanation
Accompanying drawing is structural representation of the present invention
Fluffy 9-tubular the fuel tank of 1-occupant soft seat, 2-main framing, 3-bondage belt, 4-joystick, 5-main wing bone 6-screw propeller, 7-engine petrol, 8-main wing cloth 10-empennage cloth paulin 11-empennage bone 12-power control button
Detailed description of the invention
Below in conjunction with accompanying drawing, the invention will be further described
Embodiment
At the middle part of body with main framing 2, have a main wing bone 5 on the top of main framing, main framing and main wing bone are hinged connection.With joystick 4 on main wing bone.With power control button 12 on joystick.Main wing bone both sides respectively have an engine petrol 7.With screw propeller 6 on engine petrol output shaft.At the rear portion of main wing bone with tubular fuel tank 9.With main wing cloth fluffy 8 on main wing bone.Occupant's soft seat 1 is had in main framing bottom.At main framing pars intermedia with occupant's bondage belt 3.In the bottom of main wing bone with empennage bone 11, empennage bone and main wing bone are hinged connection.With empennage tarpaulin 10 on empennage bone.Driving engine is 30 horsepowers of two-cycle gasoline engines.Main wing tarpaulin is that high strength chemistry fiber cloth is made, and the span is 5 meters.The span of empennage tarpaulin is 3 meters.Main wing bone and empennage bone are high strength aluminum alloy manufacture.
Claims (1)
1. a personal aircraft, is characterized in that, at the middle part of body with main framing (2), a main wing bone (5) is had on the top of main framing, with joystick (4) on main wing bone, with power control button (12) on joystick, main wing bone both sides respectively have an engine petrol (7), with screw propeller (6) on engine petrol output shaft, at the rear portion of main wing bone with tubular fuel tank (9), with main wing cloth fluffy (8) on main wing bone, occupant's soft seat (1) is had in main framing bottom, at main framing pars intermedia with occupant's bondage belt (3), in the bottom of main wing bone with empennage bone (11), with empennage tarpaulin (10) on empennage bone.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510179345.2A CN104843184A (en) | 2015-04-14 | 2015-04-14 | Personal air vehicle |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510179345.2A CN104843184A (en) | 2015-04-14 | 2015-04-14 | Personal air vehicle |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN104843184A true CN104843184A (en) | 2015-08-19 |
Family
ID=53843263
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510179345.2A Pending CN104843184A (en) | 2015-04-14 | 2015-04-14 | Personal air vehicle |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN104843184A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105835038A (en) * | 2016-05-19 | 2016-08-10 | 成都润惠科技有限公司 | Exoskeleton capable of flying |
Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2667568B1 (en) * | 1990-10-09 | 1994-05-13 | Eugen Vintila | INDIVIDUAL POWERED FLIGHT APPARATUS. |
| DE4302791A1 (en) * | 1993-02-02 | 1994-08-04 | Juergen Schuster | Portable helicopter attachment for lifting single person |
| CN1203167A (en) * | 1997-06-24 | 1998-12-30 | 宫晓明 | Manned aerobat capable of landing or taking-off vertically |
| US20020003188A1 (en) * | 1998-12-16 | 2002-01-10 | Michael Moshier | Single passenger aircraft |
| CN2573374Y (en) * | 2002-08-30 | 2003-09-17 | 张俊海 | One-man vertical takeoff and landing aircraft |
| CN101108654A (en) * | 2007-06-27 | 2008-01-23 | 东莞市龙行航空科技有限公司 | Double-culvert one-seater vertically taking off and landing flyer |
| CN102991673A (en) * | 2012-12-17 | 2013-03-27 | 刘斌 | New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings |
| CN204587306U (en) * | 2015-04-14 | 2015-08-26 | 王学礼 | A kind of personal aircraft |
-
2015
- 2015-04-14 CN CN201510179345.2A patent/CN104843184A/en active Pending
Patent Citations (8)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2667568B1 (en) * | 1990-10-09 | 1994-05-13 | Eugen Vintila | INDIVIDUAL POWERED FLIGHT APPARATUS. |
| DE4302791A1 (en) * | 1993-02-02 | 1994-08-04 | Juergen Schuster | Portable helicopter attachment for lifting single person |
| CN1203167A (en) * | 1997-06-24 | 1998-12-30 | 宫晓明 | Manned aerobat capable of landing or taking-off vertically |
| US20020003188A1 (en) * | 1998-12-16 | 2002-01-10 | Michael Moshier | Single passenger aircraft |
| CN2573374Y (en) * | 2002-08-30 | 2003-09-17 | 张俊海 | One-man vertical takeoff and landing aircraft |
| CN101108654A (en) * | 2007-06-27 | 2008-01-23 | 东莞市龙行航空科技有限公司 | Double-culvert one-seater vertically taking off and landing flyer |
| CN102991673A (en) * | 2012-12-17 | 2013-03-27 | 刘斌 | New type one-man flight vehicle capable of vertically taking off and landing and with fixed wings |
| CN204587306U (en) * | 2015-04-14 | 2015-08-26 | 王学礼 | A kind of personal aircraft |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105835038A (en) * | 2016-05-19 | 2016-08-10 | 成都润惠科技有限公司 | Exoskeleton capable of flying |
| CN105835038B (en) * | 2016-05-19 | 2017-10-27 | 成都润惠科技有限公司 | One kind can flight ectoskeleton |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| C06 | Publication | ||
| PB01 | Publication | ||
| EXSB | Decision made by sipo to initiate substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| RJ01 | Rejection of invention patent application after publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20150819 |