CN105083553A - Dish-shaped vertical-flying type flight device - Google Patents
Dish-shaped vertical-flying type flight device Download PDFInfo
- Publication number
- CN105083553A CN105083553A CN201510560705.3A CN201510560705A CN105083553A CN 105083553 A CN105083553 A CN 105083553A CN 201510560705 A CN201510560705 A CN 201510560705A CN 105083553 A CN105083553 A CN 105083553A
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- China
- Prior art keywords
- chassis
- dish
- air
- air supply
- shaped vertical
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- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
Abstract
The invention belongs to the technical field of flight equipment and relates to a dish-shaped vertical-flying type flight device. A main body structure comprises a chassis, an air source system, an outer air source cover, jet pipelines, air vents, a flanging and insertion pins, wherein part of air flow generated by the air source system is constantly jetted through the jet pipelines to push the dish-shaped vertical-flying type flight device to move forwards, however, most of air flow flows through the upper surface of the chassis in an outward jetting manner, so that the pressure on the upper surface of the chassis is lower than that on the lower surface of the chassis, climbing power is provided for the dish-shaped vertical-flying type flight device, and the flight device can fly upwards, fly stably and vertically and hover in the air, is applied to unmanned type aerial detection and the agriculture field, is simple in structure, scientific and reasonable in principle, safe and reliable in performance, low in manufacturing and maintenance cost, convenient to operate and maintain and environment-friendly during flight.
Description
Technical field:
The invention belongs to flight equipment technical field, relate to a kind of dish-shaped Vertical Lift flight instruments, Absorbable organic halogens flies and goes straight up to and hover aerial, is applied to unmanned formula aerial reconnaissance and agricultural applications.
Background technology:
Aircraft refers to and is manufactured by the mankind, can fly away from ground and in spaceflight, the apparatus flyer flown in endoatmosphere or space, exoatmosphere (space) of manual control, is applied to the fields such as Science Explorations, ocean and military affairs; Aircraft is generally divided into the large class of aerocraft, spacecraft, rocket, guided missile and guided weapon five: be called aerocraft at the aircraft of endoatmosphere flight, comprise balloon, aerodone, dirigible, aircraft and helicopter, the aerodynamic force lift-off flight that quiet buoyancy or air relative motion by air produce; The aircraft flown arbitrarily in space is called spacecraft, comprises artificial earth satellite, manned spacecraft, space probe and space shuttle, obtains necessary speed and enters space, then under graviational interaction, complete orbiting motion under the promotion of carrier rocket; Rocket take rocket engine as the aircraft of power, can in endoatmosphere, also can in extra-atmospheric flight; Guided missile is the controollable rocket that warhead is housed, comprise mainly extra-atmospheric flight ballistic missile, surface-to-air ballistic missile and cruise missile that aerofoil flies in endoatmosphere are housed; Guided weapon be can carry out according to certain rule, fly in an atmosphere, high hit rate weapon, comprise Terminal munition and guided cartridge.At present, had a lot of scientific research institutions to have darker research with individual to aircraft, LMT of the U.S. releases the single aerodynamic vehicle that a applicable manned marked price is 100,000 dollars, but is also in the exploratory stage in China.Step along with era development has people courageously to propose multiple flight scenario, and in June, 2008, by Harbin Shengshi Special Type Aerocraft Co., Ltd., the single-blade circuit " flying saucer " that research institute of China Aerospace Ke Gong group the 4th and space flight institute of Harbin Institute of Technology research and develop jointly is succeeded in developing in Harbin, this aircraft diameter is about 1.2 meters, dish-shaped ring contour of flange is adopted to design and special formula aerodynamic arrangement, flying height is between 50 meters to 1000 meters, flying speed is 0 to 80 kilometer heavy 10 kilograms per hour, fill fuel once can aloft fly 40 minutes, aviation can be applied in and take pictures, geologic survey, accident is thrown light on and is built the aspects such as temporary communications platform, has low latitude, low speed, the feature of vertical takeoff and landing and hovering, has the function of helicopter and fixed wing aircraft concurrently, can provide technical support for multiple field, and flight does not limit by region, and flight track can preset, and also can change at any time, can be widely used in aviation and take pictures, geologic survey, ultra-high-tension power transmission line is maked an inspection tour, oil filed pipeline checks, freeway management, forest fire protection cruising, poison gas is reconnoitred, drug law enforcement, accident is thrown light on, build temporary communications, the aspects such as platform emergency management and rescue and rescue, but its complex structure, manufacturing process are loaded down with trivial details, with high costs.Therefore, research and develop the dish-shaped Vertical Lift flight instruments that a kind of structure is simple, simple for production and with low cost, have good society and economic value, have a extensive future.
Summary of the invention:
The object of the invention is to the shortcoming overcoming prior art existence, design a kind of structure simple, the dish-shaped Vertical Lift flight instruments that manufacture craft is easy and with low cost.
To achieve these goals, agent structure of the present invention comprises chassis, air supply system, source of the gas outer cover, jet pipe, airflow orifice, flanging and grafting pawl, the circumferential edges downward bending on the chassis of circular configuration forms the flanging of 0-10cm height, the upper surface center on chassis is fixedly installed source of the gas outer cover, the inside of the source of the gas outer cover of hollow type structure is fixedly installed the air supply system of jet-propelled structure, air supply system is bolted the upper surface center being arranged on chassis, two jet pipes of parallel side-by-side are stretched out source of the gas outer cover by the center of air supply system along the downside on chassis and extend to the flanging on chassis, the trend of two jet pipes is parallel to the radius on chassis, the bottom margin of source of the gas outer cover has been equidistantly spaced grafting pawl, source of the gas outer cover is fixedly connected with by grafting pawl plug-in type with chassis, space formula airflow orifice is formed between grafting pawl and the upper surface on chassis, the air-flow ejection that air supply source system sends, each part fits forms dish-shaped Vertical Lift aircraft, realizes lift-off flight, turns to the skyborne function with steadily hovering.
The upper surface on the chassis that the present invention relates to is arc formula structure, the thickness on chassis is by excircle even progressive increase to center, the thickness of the center is not more than 2 times of outer circumferential edges place thickness, and the air-flow size that the radius on chassis produces according to the deadweight on chassis and air supply system is determined through theory calculate or flight test; Air supply system comprises combustion engine, electrical motor, solar power, blowing engine and powered by nuclear energy machine, and the center of air supply system overlaps with the center of circle on chassis.
When the dish-shaped Vertical Lift flight instruments that the present invention relates to uses, the power that air supply system provides makes chassis rotation take off and produce air-flow, fraction continues ejection and promotes the advance of dish-shaped Vertical Lift flight instruments from jet pipe, major part air-flow evenly flows out and along the upper surface jet flow on chassis from each airflow orifice, the upper surface pressure on chassis is made to be less than the lower surface pressure on chassis, for dish-shaped Vertical Lift flight instruments provides raising force to make it upwards fly, air supply system can regulate the size producing air-flow, and by controlling the speed of air-flow ejection jet pipe and airflow orifice, position and size realize turning to the skyborne function with steadily hovering.
The present invention compared with prior art, the fraction produced by air supply system continues the dish-shaped Vertical Lift flight instruments of ejection promotion by jet pipe and moves ahead, and most of air-flow is flow through along chassis upper surface external spraying type by each airflow orifice, the upper surface pressure on chassis is made to be less than the lower surface pressure on chassis, for dish-shaped Vertical Lift flight instruments provides raising force to make it upwards fly; Its structure is simple, and scientific in principle is reasonable, and performance safety is reliable, make and maintenance cost low, operation and maintenance is convenient, flight environment of vehicle close friend.
Accompanying drawing illustrates:
Fig. 1 is agent structure principle schematic of the present invention.
Detailed description of the invention:
Also by reference to the accompanying drawings the present invention is described further below by embodiment.
Embodiment:
The agent structure of the dish-shaped Vertical Lift flight instruments that the present embodiment relates to comprises chassis 1, air supply system 2, source of the gas outer cover 3, jet pipe 4, airflow orifice 5, flanging 6 and grafting pawl 7, the circumferential edges downward bending on the chassis 1 of circular configuration forms the flanging 6 of 0-10cm height, the upper surface center on chassis 1 is fixedly installed source of the gas outer cover 3, the inside of the source of the gas outer cover 3 of hollow type structure is fixedly installed the air supply system 2 of jet-propelled structure, air supply system 2 is bolted the upper surface center being arranged on chassis 1, two jet pipes 4 of parallel side-by-side are stretched out source of the gas outer cover 3 by the center of air supply system 2 along the downside on chassis 1 and extend to the flanging 6 on chassis 1, the trend of two jet pipes 4 is parallel to the radius on chassis 1, the bottom margin of source of the gas outer cover 3 has been equidistantly spaced grafting pawl 7, source of the gas outer cover 3 is fixedly connected with by grafting pawl 7 plug-in type with chassis 1, space formula airflow orifice 5 is formed between the upper surface on grafting pawl 7 and chassis 1, the air-flow ejection that air supply source system 2 sends, each part fits forms dish-shaped Vertical Lift aircraft, realizes lift-off flight, turns to the skyborne function with steadily hovering.
The upper surface on the chassis 1 that the present embodiment relates to is arc formula structure, the thickness on chassis 1 is by excircle even progressive increase to center, the thickness of the center is not more than 2 times of outer circumferential edges place thickness, and the air-flow size that the radius on chassis 1 produces according to the deadweight on chassis 1 and air supply system 2 is determined through theory calculate or flight test; Air supply system 2 comprises combustion engine, electrical motor, solar power, blowing engine and powered by nuclear energy machine, and the center of air supply system 2 overlaps with the center of circle on chassis 1.
When the dish-shaped Vertical Lift flight instruments that the present embodiment relates to uses, the power that air supply system 2 provides makes chassis 1 rotation take off and produce air-flow, fraction continues ejection and promotes the advance of dish-shaped Vertical Lift flight instruments from jet pipe 4, major part air-flow evenly flows out and along the upper surface jet flow on chassis 1 from each airflow orifice 5, the upper surface pressure on chassis 1 is made to be less than the lower surface pressure on chassis 1, for dish-shaped Vertical Lift flight instruments provides raising force to make it upwards fly, air supply system 2 can regulate the size producing air-flow, and by controlling the speed of air-flow ejection jet pipe 4 and airflow orifice 5, position and size realize turning to the skyborne function with steadily hovering.
Claims (3)
1. a dish-shaped Vertical Lift flight instruments, is characterized in that agent structure comprises chassis, air supply system, source of the gas outer cover, jet pipe, airflow orifice, flanging and grafting pawl, the circumferential edges downward bending on the chassis of circular configuration forms the flanging of 0-10cm height, the upper surface center on chassis is fixedly installed source of the gas outer cover, the inside of the source of the gas outer cover of hollow type structure is fixedly installed the air supply system of jet-propelled structure, air supply system is bolted the upper surface center being arranged on chassis, two jet pipes of parallel side-by-side are stretched out source of the gas outer cover by the center of air supply system along the downside on chassis and extend to the flanging on chassis, the trend of two jet pipes is parallel to the radius on chassis, the bottom margin of source of the gas outer cover has been equidistantly spaced grafting pawl, source of the gas outer cover is fixedly connected with by grafting pawl plug-in type with chassis, space formula airflow orifice is formed between grafting pawl and the upper surface on chassis, the air-flow ejection that air supply source system sends, each part fits forms dish-shaped Vertical Lift aircraft, realizes lift-off flight, turns to the skyborne function with steadily hovering.
2. dish-shaped Vertical Lift flight instruments according to claim 1, it is characterized in that the upper surface on described chassis is arc formula structure, the thickness on chassis is by excircle even progressive increase to center, the thickness of the center is not more than 2 times of outer circumferential edges place thickness, and the air-flow size that the radius on chassis produces according to the deadweight on chassis and air supply system is determined through theory calculate or flight test; Air supply system comprises combustion engine, electrical motor, solar power, blowing engine and powered by nuclear energy machine, and the center of air supply system overlaps with the center of circle on chassis.
3. dish-shaped Vertical Lift flight instruments according to claim 1, when it is characterized in that using, the power that air supply system provides makes chassis rotation take off and produce air-flow, fraction continues ejection and promotes the advance of dish-shaped Vertical Lift flight instruments from jet pipe, major part air-flow evenly flows out and along the upper surface jet flow on chassis from each airflow orifice, the upper surface pressure on chassis is made to be less than the lower surface pressure on chassis, for dish-shaped Vertical Lift flight instruments provides raising force to make it upwards fly, air supply system can regulate the size producing air-flow, and by controlling the speed of air-flow ejection jet pipe and airflow orifice, position and size realize turning to the skyborne function with steadily hovering.
Priority Applications (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510560705.3A CN105083553A (en) | 2015-09-07 | 2015-09-07 | Dish-shaped vertical-flying type flight device |
| CN201610148046.7A CN105620751B (en) | 2015-09-07 | 2016-03-15 | A kind of dish-shaped Vertical Lift flight instruments |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201510560705.3A CN105083553A (en) | 2015-09-07 | 2015-09-07 | Dish-shaped vertical-flying type flight device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN105083553A true CN105083553A (en) | 2015-11-25 |
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Family Applications (2)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201510560705.3A Pending CN105083553A (en) | 2015-09-07 | 2015-09-07 | Dish-shaped vertical-flying type flight device |
| CN201610148046.7A Active CN105620751B (en) | 2015-09-07 | 2016-03-15 | A kind of dish-shaped Vertical Lift flight instruments |
Family Applications After (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201610148046.7A Active CN105620751B (en) | 2015-09-07 | 2016-03-15 | A kind of dish-shaped Vertical Lift flight instruments |
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| Country | Link |
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| CN (2) | CN105083553A (en) |
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106428559A (en) * | 2016-11-30 | 2017-02-22 | 吴锜 | Disc type aircraft |
| CN106516108A (en) * | 2016-05-12 | 2017-03-22 | 王金海 | Atmospheric pressure anti-gravity device |
| CN109319114A (en) * | 2018-09-06 | 2019-02-12 | 武汉豪岩照明电子有限公司 | A kind of dish gas curtain aeromodelling aerocraft |
Family Cites Families (9)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5170963A (en) * | 1991-09-24 | 1992-12-15 | August H. Beck Foundation Company | VTOL aircraft |
| CN1224681A (en) * | 1998-09-25 | 1999-08-04 | 何惠平 | Flying disc with rotary hull |
| GB2387158B (en) * | 2002-03-01 | 2005-08-10 | Robert John Collins | Aerial devices |
| CN1669875A (en) * | 2004-03-20 | 2005-09-21 | 梁良 | Principle of a disk-shaped aircraft and an engine and method for realizing the principle |
| CN1693139A (en) * | 2004-05-06 | 2005-11-09 | 李泽奇 | Dish type aircraft and its application |
| CN101823558A (en) * | 2009-03-03 | 2010-09-08 | 武汉鼎超科技开发有限公司 | Inverse gravity aircraft |
| CN201712789U (en) * | 2010-05-11 | 2011-01-19 | 邓志平 | Wingless aircraft |
| CN103419935B (en) * | 2013-07-24 | 2016-08-24 | 南京航空航天大学 | Dish-shaped layout vertically taking off and landing flyer based on novel high-lift device |
| CN104417751A (en) * | 2013-09-03 | 2015-03-18 | 雷万军 | Disc type airplane with pneumatic wings |
-
2015
- 2015-09-07 CN CN201510560705.3A patent/CN105083553A/en active Pending
-
2016
- 2016-03-15 CN CN201610148046.7A patent/CN105620751B/en active Active
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN106516108A (en) * | 2016-05-12 | 2017-03-22 | 王金海 | Atmospheric pressure anti-gravity device |
| CN106428559A (en) * | 2016-11-30 | 2017-02-22 | 吴锜 | Disc type aircraft |
| CN109319114A (en) * | 2018-09-06 | 2019-02-12 | 武汉豪岩照明电子有限公司 | A kind of dish gas curtain aeromodelling aerocraft |
Also Published As
| Publication number | Publication date |
|---|---|
| CN105620751A (en) | 2016-06-01 |
| CN105620751B (en) | 2017-06-06 |
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Application publication date: 20151125 |