CN103192977A - High-speed floating aircraft - Google Patents
High-speed floating aircraft Download PDFInfo
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- CN103192977A CN103192977A CN2013101338294A CN201310133829A CN103192977A CN 103192977 A CN103192977 A CN 103192977A CN 2013101338294 A CN2013101338294 A CN 2013101338294A CN 201310133829 A CN201310133829 A CN 201310133829A CN 103192977 A CN103192977 A CN 103192977A
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- hollow inner
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- inner casing
- aircraft fuselage
- buoyance lift
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Abstract
The invention relates to a high-speed floating aircraft with floating air bags. According to the technical scheme, the high-speed floating aircraft comprises an aircraft body, the floating air bags, electric lift impellers, balance wings, a cabin, a cockpit, an equipment cabin, a landing gear and tires. The floating air bags are disposed between a housing and a hollow inner shell of the aircraft body. The cabin is located between the hollow inner shell and the housing of the aircraft body. The cockpit is located at the front end of the cockpit. A motor is disposed in the hollow inner shell, and a thrust propeller is mounted on the motor. The motor is fixedly mounted on the hollow inner shell through a motor support. The electric lift impellers are mounted on the balance wings. Various control buttons and a steering wheel are mounted on a console inside the cockpit. The high-speed floating aircraft is powered by electricity which is natural and clean, and the requirements for energy conservation, environment protection and low-carbon economy are met. The features of a conventional airship, such as high weight and high flying safety, are retained, and the high-speed floating aircraft flies fast, increased from 200KM/h of the common low-attitude aircraft to 400KM/h.
Description
Technical field
The present invention relates to fly the field of wafing, particularly relate to the high speed flight device that has the buoyance lift air bag, this flight device also can sail on the water except can aloft flying.
Background technology
Existing aircraft, roughly there are three kinds: aircraft, dirigible and fire balloon, most of aviation aircrafts all adopt fuel oil equal energy source power to start aircraft, and the aviation aircraft that adopts the energy to do power does not meet low-carbon economy and environmental protection requirement, and flight cost is also very high; Aircraft flight speed is very fast, but safety problem is not solved so far; Fire balloon is because self flight theory determines that it can not be as load transportation instrument professional purpose; Flying speed can not get significantly improving always though dirigible has utility function.Up to now, also do not find the existing flight device that has air bag and high-speed flight.
Summary of the invention
The objective of the invention is the weak point at existing aircraft, fire balloon and dirigible, propose a kind of by using a plurality of inflation buoyance lift air bags and electronic thrust screw propeller, according to aerodynamic principle, change the arrangement mode of buoyance lift air bag, reach the brand new technical scheme of the flight device of high-speed flight.
Technical scheme of the present invention is: this flight device comprises aircraft fuselage, buoyance lift air bag, electronic lifting propeller, balance wing, passenger cabin, driving compartment, equipment compartment, alighting gear and tire.A plurality of buoyance lift air bags are installed between the shell and hollow inner casing of aircraft fuselage, and passenger cabin is between the shell of hollow inner casing and aircraft fuselage, and driving compartment is positioned at the front end of passenger cabin.In the hollow inner casing electrical motor is installed, the thrust screw propeller is installed on the electrical motor, electrical motor is fixedly mounted on the hollow inner casing by motor bracket, and electronic lifting propeller is installed on the balance wing, on the operation bench in the driving compartment various control buttons and bearing circle is installed.A plurality of buoyance lift air bags in the aircraft fuselage are 6-8, center on the big half-turn that hollow inner casing has been arranged whole fuselage, have been full of unreactable gas in the buoyance lift air bag.The equipment compartment that is positioned at the passenger cabin below is equipped with gasoline engine generator and current distributor.The back fragment position is equipped with the yaw rudder of control heading between the hollow inner casing of aircraft fuselage.The present invention is the same with aircraft can normally to stop on the ground, need not need a large amount of ground staff to carry out mooring as dirigible and fix and safeguard.
Use when of the present invention, by the control button of installing on the driving compartment operating console, start gasoline engine generator, gasoline engine generator delivers power to the electronic lifting propeller that is positioned on the balance wing and is positioned at hollow inner casing thrust screw propeller by current distributor, effect by electronic lifting propeller and buoyance lift air bag, make the present invention at the original place VTOL function, do not need the such plane track of conventional airplane.After the lift-off, under the effect of thrust screw propeller fast rotational, fly, promote the present invention and fly fast.The present invention realizes by yaw rudder when changing direction by the pilot control bearing circle.When the present invention descended, the control by electronic button on the operating console and multi-channel remote device stopped the rotation of thrust propeller blade, gradually reduces the rotating speed of lifting propeller, slowly descended, until landing.Because the present invention has several buoyance lift air bags, the present invention also can sail on the water and be unlikely to sink.
The present invention has following remarkable result:
1, because the present invention mainly leans on nature clean energy resource-electric energy as power, meets the requirement of energy-saving and environmental protection and low-carbon economy;
2, the present invention has kept the characteristics that conventional dirigible load carrying ability is big, flight safety is high;
3, flying speed of the present invention is fast.Flying speed can be brought up to 400KM/ hour from 200KM/ hour of common aircraft;
4, the present invention not only can aloft fly, and also can advance at the water surface, has air-sea two function of dwelling;
5, the present invention can keep having a smooth flight because electronic lifting propeller symmetry is installed on the balance wing of fuselage both sides in-flight;
6, the present invention does not use the engine petrol of aircraft, and the most of space of fuselage is the buoyance lift air bag in addition, has significantly reduced deadweight of the present invention and oil consumption, has improved flight efficiency;
7, be hollow duct shape structure in the fuselage of the present invention, advance the thrust screw propeller that moves ahead that flies to waft to be installed in wherein, effectively brought into play the progradation that screw propeller rotates at a high speed;
8, because integral body of the present invention and air bag by the parcel of interior hard coat, have greatly improved wind loading rating of the present invention.
Brief Description Of Drawings
Fig. 1 is structural representation of the present invention.
Fig. 2 is fuselage longitudinal construction scheme drawing of the present invention.
As shown in the figure: the hollow inner casing 15-of the electronic lifting propeller 4-of 1-aircraft fuselage 2-buoyance lift air bag 3-balance wing 5-electrical motor bracing frame 6-electrical motor 7-thrust screw propeller 8-passenger cabin 9-equipment compartment 10-engine petrol 11-flight tire 12-alighting gear 13-current distributor 14-driving compartment 16-taper buoyance lift air bag head 17-yaw rudder 18-flight tire 19-alighting gear
The specific embodiment
The specific embodiment of the present invention is illustrated by reference to the accompanying drawings: as shown in the figure, this flight device comprises aircraft fuselage (1), buoyance lift air bag (2), electronic lifting propeller (3), balance wing (4), passenger cabin (8), driving compartment (15), equipment compartment (9), alighting gear and tire.A plurality of buoyance lift air bags (2) are installed between the shell and hollow inner casing (14) of aircraft fuselage (1), passenger cabin (8) is positioned between the shell of hollow inner casing (14) and aircraft fuselage (1), driving compartment (15) is positioned at the front end of passenger cabin, electrical motor (6) is installed in the hollow inner casing (14), thrust screw propeller (7) is installed on the electrical motor (6), electrical motor (6) is fixedly mounted on the hollow inner casing (14) by motor bracket (5), electronic lifting propeller (3) is installed on the fuselage both sides balance wing (4), on the operation bench in the driving compartment (15) various control buttons and bearing circle is installed.
The a plurality of buoyance lift air bags (2) that are installed in the aircraft fuselage (1) are 6-8, center on the big half-turn that hollow inner casing (14) has been arranged whole fuselage, and the buoyance lift air bag has been full of unreactable gas in (2).In the equipment compartment (9) of passenger cabin (8) below gasoline engine generator (10) and current distributor (13) are installed.The back fragment position is equipped with the yaw rudder (17) of control heading between the hollow inner casing (14) of aircraft fuselage (1).
Claims (4)
1. high speed flight device, this flight device comprises aircraft fuselage (1), buoyance lift air bag (2), electronic lifting propeller (3), balance wing (4), passenger cabin (8), driving compartment (15), equipment compartment (9), alighting gear and tire, it is characterized in that: a plurality of buoyance lift air bags (2) are installed between the shell and hollow inner casing (14) of aircraft fuselage (1), passenger cabin (8) is positioned between the shell of hollow inner casing (14) and aircraft fuselage (1), driving compartment (15) is positioned at the front end of passenger cabin, electrical motor (6) is installed in the hollow inner casing (14), electrical motor is equipped with the thrust screw propeller on (6), electrical motor (6) is fixedly mounted on the hollow inner casing (14) by motor bracket, electronic lifting propeller (3) is installed on the balance wing (4), on the operation bench in the driving compartment (15) various control buttons and bearing circle is installed.
2. a kind of high speed flight device according to claim 1, the a plurality of buoyance lift air bags (2) that it is characterized in that being installed in the aircraft fuselage (1) are 6-8, center on hollow inner casing (14) and arranged the big half-turn of whole fuselage, the buoyance lift air bag has been full of unreactable gas in (2).
3. a kind of high speed flight device according to claim 1 is characterized in that the equipment compartment (9) that is positioned at passenger cabin (8) below is equipped with gasoline engine generator (10) and current distributor (13).
4. a kind of high speed flight device according to claim 1 is characterized in that the back fragment position is equipped with the yaw rudder (17) of controlling heading between the hollow inner casing (14) of aircraft fuselage (1).
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101338294A CN103192977A (en) | 2013-04-18 | 2013-04-18 | High-speed floating aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2013101338294A CN103192977A (en) | 2013-04-18 | 2013-04-18 | High-speed floating aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN103192977A true CN103192977A (en) | 2013-07-10 |
Family
ID=48715835
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN2013101338294A Pending CN103192977A (en) | 2013-04-18 | 2013-04-18 | High-speed floating aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN103192977A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428505A (en) * | 2016-11-14 | 2017-02-22 | 杨礼诚 | Flying aircraft with jet propeller |
| CN108622393A (en) * | 2018-05-10 | 2018-10-09 | 唐晓刚 | A kind of multiple-energy-source fusion aircraft and its control method |
| CN109319083A (en) * | 2017-07-31 | 2019-02-12 | 王树强 | A kind of axis change soft lighter-than-air flight device of buoyancy |
| CN110844039A (en) * | 2019-10-15 | 2020-02-28 | 中国特种飞行器研究所 | Electric airship |
| CN113931797A (en) * | 2021-09-22 | 2022-01-14 | 顿天瑞 | Suspension equipment and maintenance method |
Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB190918768A (en) * | 1909-08-14 | 1910-01-20 | Peter Jensen | Improvements relating to the Gas Bags of Balloons, Air Ships and the like. |
| CN2387032Y (en) * | 1999-08-04 | 2000-07-12 | 徐石 | Sack type airship with lifter |
| CN2516457Y (en) * | 2001-11-30 | 2002-10-16 | 于德荣 | Aircraft composed of hydrogen balloon and flying control device |
| CN1689913A (en) * | 2004-04-19 | 2005-11-02 | 张电红 | Gasbag culvert type propeller helicopter |
| CN2895244Y (en) * | 2005-12-17 | 2007-05-02 | 胡绍勇 | Dual-rotor mixed manned boat seaplane |
-
2013
- 2013-04-18 CN CN2013101338294A patent/CN103192977A/en active Pending
Patent Citations (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB190918768A (en) * | 1909-08-14 | 1910-01-20 | Peter Jensen | Improvements relating to the Gas Bags of Balloons, Air Ships and the like. |
| CN2387032Y (en) * | 1999-08-04 | 2000-07-12 | 徐石 | Sack type airship with lifter |
| CN2516457Y (en) * | 2001-11-30 | 2002-10-16 | 于德荣 | Aircraft composed of hydrogen balloon and flying control device |
| CN1689913A (en) * | 2004-04-19 | 2005-11-02 | 张电红 | Gasbag culvert type propeller helicopter |
| CN2895244Y (en) * | 2005-12-17 | 2007-05-02 | 胡绍勇 | Dual-rotor mixed manned boat seaplane |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428505A (en) * | 2016-11-14 | 2017-02-22 | 杨礼诚 | Flying aircraft with jet propeller |
| CN109319083A (en) * | 2017-07-31 | 2019-02-12 | 王树强 | A kind of axis change soft lighter-than-air flight device of buoyancy |
| CN108622393A (en) * | 2018-05-10 | 2018-10-09 | 唐晓刚 | A kind of multiple-energy-source fusion aircraft and its control method |
| CN110844039A (en) * | 2019-10-15 | 2020-02-28 | 中国特种飞行器研究所 | Electric airship |
| CN113931797A (en) * | 2021-09-22 | 2022-01-14 | 顿天瑞 | Suspension equipment and maintenance method |
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| C06 | Publication | ||
| PB01 | Publication | ||
| C10 | Entry into substantive examination | ||
| SE01 | Entry into force of request for substantive examination | ||
| C02 | Deemed withdrawal of patent application after publication (patent law 2001) | ||
| WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20130710 |