CN106428559A - Disc type aircraft - Google Patents
Disc type aircraft Download PDFInfo
- Publication number
- CN106428559A CN106428559A CN201611080166.4A CN201611080166A CN106428559A CN 106428559 A CN106428559 A CN 106428559A CN 201611080166 A CN201611080166 A CN 201611080166A CN 106428559 A CN106428559 A CN 106428559A
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- CN
- China
- Prior art keywords
- exhaustor
- disk body
- aircraft
- air valve
- high pressure
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- 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.)
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Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C39/00—Aircraft not otherwise provided for
- B64C39/001—Flying saucers
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
- B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
- B64C29/0016—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by free or ducted propellers or by blowers
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- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Toys (AREA)
Abstract
The invention belongs to the technical field of flight equipment and relates to a disc type aircraft. The aircraft can vertically take off and land. A main body structure comprises a high-pressure air chamber, a disc body, a load bearing bin, exhaust pipes, landing supports, exhaust holes, a high-pressure air flow supply device and an air valve. The high-pressure air flow supply device controls high-pressure air flow to be sprayed along the upper surface of the disc body through the exhaust holes, so the disc body generates raising force larger than the gravity of the disc type aircraft, and the disc type aircraft starts to ascend and take off; The exhaust pipes at corresponding positions are controlled to be opened and closed through the air valve so that the disc type aircraft can fly in different directions, and the disc type aircraft can move forward and backward, hover, horizontally move and steer; the aircraft can be manufactured into a remote control toy, an air photography device, a low-altitude ground reconnaissance device, an agricultural condition inspection device, a disaster scene rescue device and an offshore area detection and rescue device. The aircraft is simple in structure, scientific and reasonable in principle, safe and reliable in performance, low in manufacturing and maintenance cost, and convenient to operate and maintain, and the flight environment is friendly.
Description
Technical field：
The invention belongs to flight equipment technical field, be related to a kind of disc aircraft, can vertical and landing takeoff, in sky
The flight of middle anterior-posterior translation, turn or hover, nose into as remote-control toy, aerophotography, low latitude ground reconnaissance, agricultural agriculture feelings, calamity
Ball is searched at difficult scene and coastal waters field detects and uses with searching and rescuing.
Background technology：
Aircraft refers to be manufactured by the mankind, can fly away from ground and in space flight, manual control in endoatmosphere or
The apparatus flying object flying in exoatmosphere space (space), is applied to the fields such as Science Explorations, ocean and military affairs；Aircraft is general
It is divided into airborne vehicle, spacecraft, rocket, guided missile and guided weapon five big class：It is referred to as airborne vehicle in the aircraft of endoatmosphere flight,
Including balloon, aerodone, dirigible, aircraft and helicopter, the air force of the quiet buoyancy by air or the generation of air relative motion
Lift-off flight；It is referred to as spacecraft in the aircraft of space arbitrarily flight, including artificial earth satellite, manned spaceship, space exploration
Device and space shuttle, obtain necessary speed under the promotion of carrier rocket and enter space, then complete rail under graviational interaction
Road moves；Rocket is the aircraft with rocket engine as power, can be in endoatmosphere, also can be in extra-atmospheric flight；Guided missile
Be equipped with the controllable rocket of warhead, including mainly the ballistic missile of extra-atmospheric flight, equipped with aerofoil in atmosphere
The surface-to-air ballistic missile of interior flight and cruise missile；Guided weapon be can carry out according to certain rule, fly in an atmosphere, high
Hit rate weapon, including Terminal munition and guided cartridge.At present, there are a lot of scientific research institutions and individual that aircraft is had deeper
Research, LMT of the U.S. release a be suitable for the single aerodynamic vehicle for 100,000 dollars for the manned marked price, but
China is also in the exploratory stage.Step someone with era development courageously proposes multiple flight scenario, in June, 2008, by
Harbin Shengshi Special Type Aerocraft Co., Ltd., China Aerospace Ke Gong group the 4th academy and Harbin Institute of Technology's aerospace
The single-blade circuit " flying saucer " of the common research and development of institute is succeeded in developing in Harbin, and this aircraft diameter is about 1.2 meters, using the dish-shaped ring wing
Configuration design and special formula aerodynamic arrangement, between 50 meters to 1000 meters, flight speed is 0 to 80 kilometer per hour to flying height
Weigh 10 kilograms, fill fuel and once can fly in the air 40 minutes, can apply take pictures in aviation, geological survey, accident
Illumination and build the aspects such as temporary communications platform, there is low latitude, low speed, VTOL and hovering, have concurrently helicopter and
The function of fixed wing airplane, can provide technical support for multiple fields, without geographical restrictions, flight track can set in advance for flight
Fixed, also can change at any time, can be widely applied to aviation take pictures, geological survey, ultra-high-tension power transmission line tour, oil filed pipeline inspection,
Freeway management, forest fire protection cruising, poison are reconnoitred, enforce the drug law, accident illumination, build temporary communications, first aid answered by platform
The aspect such as help and give first aid to；But its complex structure, manufacturing process are loaded down with trivial details, with high costs.Therefore, research and develop that a kind of structure is simple, make
Disc aircraft easy and with low cost, has good society and economic worth, has a extensive future.
Content of the invention：
It is an object of the invention to overcoming the shortcoming that prior art exists, design a kind of structure simply, applied range, system
Make simple process and disc aircraft with low cost.
To achieve these goals, the agent structure of disc aircraft according to the present invention includes plenum chamber, disk body, load
Weight storehouse, exhaustor, floor stand, steam vent, high pressure draught feedway and air valve；The upper surface center of the disk body of platy structure
Place is provided with the plenum chamber of hollow type streamlined structure, and at the position that plenum chamber is intersected with disk body, uniform intervals offer
The steam vent of 3-12 rectangular configuration, the inner space of plenum chamber is provided with high pressure draught feedway and air valve, high pressure gas
Stream supply device is electrically connected with air valve, and the lower surface center of disk body is provided with the carrying cabin of hollow type round rectangle structure, carries
The outer surface bottom even compartment in weight storehouse is provided with the floor stand of 3-6 telescopic structure, and the perimeter of disk body is uniform
Compartment is provided with the exhaustor of 8-24 root hollow type cylindrical structural, and exhaustor is stretched out by plenum chamber and extends to disk body
Outward flange, exhaustor and floor stand are electrically connected with air valve respectively.
Plenum chamber according to the present invention adopts fairshaped appearance and modeling, effectively reduces air drag；The shape of disk body
Including circle, ellipse, tetragon, polygon and casper, the surface of disk body includes plane, convex surface, concave surface and concavo-convex knot
The face closed；Carrying cabin can load remote control device, communications service equipment and imaging equipment or driving cabin and driver；Aerofluxuss
The set location of pipe includes upper surface or the lower surface of disk body, and exhaustor can also be embedded in the interlayer of disk body；Floor stand
In disc aircraft flight course, zoom state is in by Air Valve Control, floor stand in disc aircraft descent by
Air Valve Control is in extended configuration and provides support force for it after disc aircraft lands；Steam vent can coordinate high pressure draught
Taking off, land and hovering of disc aircraft realized by feedway；High pressure draught feedway includes compressed air, plasma
Stream and high temperature and high pressure gas generator and aerator, the flow velocity of the high pressure draught that high pressure draught feedway provides is according to dish-style
The weight of aircraft and size set；Air valve selects electromagnetic gas valve, the switch of Air Valve Control exhaustor, when air valve is opened, aerofluxuss
With high pressure draught feedway in electrical communication, high pressure draught sprays from exhaustor pipe, and when air valve is closed, high pressure draught stops spray
Go out, realize the opening and closing of exhaustor by controlling the opening and closing of air valve, the exhaustor by Air Valve Control disk body various location can
Realize advance, retrogressing, hovering, translation and the steering of disc aircraft.
When disc aircraft according to the present invention uses, open high pressure draught feedway, high pressure draught is through steam vent
Along the upper surface injection of disk body, based on fluid mechanics principle, the pressure of high pressure draught is less than the pressure of low speed flow, works as high pressure
When air-flow flows through the upper surface of disk body, the pressure of disk body upper surface is less than the pressure of disk body lower surface, makes disk body produce rising
Power, the power of rising is more than the gravity of disc aircraft, and disc aircraft begins to ramp up and takes off, during due to exhaustor jet, dish-style
Aircraft will fly to the direction in opposite direction with exhaustor jet, and during setting height of flying, air valve opens the exhaustor of rear side,
Disc aircraft advances, and air valve opens the exhaustor of front side, and disc aircraft retreats, and air valve opens the exhaustor on right side, dish-style
Aircraft flies to the left, and air valve opens the exhaustor in left side, and disc aircraft flies to the right, after air valve closes exhaustor,
Disc aircraft hovers in the air, by the opening and closing of the exhaustor of Air Valve Control relevant position, makes disc aircraft to not Tongfang
To flight, realize advance, retrogressing, hovering, translation and the steering of disc aircraft.
Disc aircraft according to the present invention according to different structure proportions can be fabricated to remote-control toy, aerophotography,
Low latitude ground reconnaissance, agriculture agriculture feelings nose into, disaster scene is searched and rescued and coastal waters field detects and searches and rescues equipment；As remote-control toy
When, disk body is fabricated to casper, places cartoon driver moulding personage, increase the interest of toy in carrying cabin, as
Aerophotography, low latitude ground reconnaissance, agriculture agriculture feelings nose into, disaster scene is searched and rescued and coastal waters field detect with search and rescue use when,
Photographic goods, communications service, medicine flusher or relief equipment is placed in carrying cabin.
The present invention compared with prior art, high pressure draught feedway control high pressure draught through steam vent along disk body upper table
Face is sprayed, and makes disk body produce the power rising, the power of rising is more than the gravity of disc aircraft, disc aircraft has begun to ramp up
Fly, and by the opening and closing of Air Valve Control relevant position exhaustor, so that disc aircraft is flown to different directions, realize dish-style flight
The advance of device, retrogressing, hovering, translation and steering, can be fabricated to remote-control toy, aerophotography, low latitude according to different ratios
Agriculture feelings nose into, ball is searched in disaster scene and coastal waters field detects and search and rescue equipment for ground reconnaissance, agricultural；Its structure is simple, principle section
Learn rationally, performance safety is reliable, make and maintenance cost is low, operation and maintenance is convenient, flight environment of vehicle is friendly.
Brief description：
Fig. 1 is the agent structure principle schematic of the present invention.
Specific embodiment：
Below by embodiment and combine accompanying drawing the present invention is described further.
Embodiment：
The agent structure of the disc aircraft that the present embodiment is related to includes plenum chamber 1, disk body 2, carrying cabin 3, exhaustor
4th, floor stand 5, steam vent 6, high pressure draught feedway 7 and air valve 8；The upper surface center of the disk body 2 of platy structure sets
It is equipped with the plenum chamber 1 of hollow type streamlined structure, at the position that plenum chamber 1 is intersected with disk body 2, uniform intervals offer
The steam vent 6 of 3-12 rectangular configuration, the inner space of plenum chamber 1 is provided with high pressure draught feedway 7 and air valve 8, high
Stream supply device 7 of calming the anger is electrically connected with air valve 8, and the lower surface center of disk body 2 is provided with the load of hollow type round rectangle structure
Weight storehouse 3, the outer surface bottom even compartment of carrying cabin 3 is provided with the floor stand 5 of 3-6 telescopic structure, the week of disk body 2
Side periphery uniform intervals formula is provided with the exhaustor 4 of 8-24 root hollow type cylindrical structural, and exhaustor 4 is stretched out by plenum chamber 1
And extending to the outward flange of disk body 2, exhaustor 4 and floor stand 5 are electrically connected with air valve 8 respectively.
The plenum chamber 1 that the present embodiment is related to adopts fairshaped appearance and modeling, effectively reduces air drag；Disk body 2
Shape includes circle, ellipse, tetragon, polygon and casper, and the surface of disk body 2 includes plane, convex surface, concave surface and recessed
The face that umbo closes；Carrying cabin 3 can load remote control device, communications service equipment and imaging equipment or driving cabin and driving
Member；The set location of exhaustor 4 includes upper surface or the lower surface of disk body 2, and exhaustor 4 can also be embedded in the interlayer of disk body 2
In；Floor stand 5 is in zoom state by air valve 8 control in disc aircraft flight course, and floor stand 5 flies in dish-style
Controlled by air valve 8 in device descent and be in extended configuration and provide support force for it after disc aircraft lands；Steam vent 6
High pressure draught feedway 7 can be coordinated to realize taking off, land and hovering of disc aircraft；High pressure draught feedway 7 wraps
Include compressed air, plasma stream and high temperature and high pressure gas generator and aerator, the height that high pressure draught feedway 7 provides
The flow velocity of pressure gas stream sets according to the weight of disc aircraft and size；Air valve 8 selects electromagnetic gas valve, and air valve 8 controls exhaustor 4
Switch, when air valve 8 is opened, with high pressure draught feedway 7 in electrical communication, high pressure draught sprays from exhaustor 4 for exhaustor 4,
When air valve 8 is closed, high pressure draught stops spraying, and realizes the opening and closing of exhaustor 4 by controlling the opening and closing of air valve 8, is controlled by air valve 8
The exhaustor 4 of disk body 2 various location processed is capable of advance, retrogressing, hovering, translation and the steering of disc aircraft.
When the disc aircraft that the present embodiment is related to uses, open high pressure draught feedway 7, high pressure draught is through aerofluxuss
Along the upper surface injection of disk body 2, based on fluid mechanics principle, the pressure of high pressure draught is less than the pressure of low speed flow in hole 6, when
When high pressure draught flows through the upper surface of disk body 2, the pressure of disk body 2 upper surface is less than the pressure of disk body 2 lower surface, so that disk body 2 is produced
The raw power rising, the power of rising is more than the gravity of disc aircraft, and disc aircraft begins to ramp up and takes off, because exhaustor 4 sprays
During gas, disc aircraft will fly to the direction in opposite direction with exhaustor 4 jet, during setting height of flying, after air valve 8 is opened
The exhaustor 4 of side, disc aircraft advances, and air valve 8 opens the exhaustor 4 of front side, and disc aircraft retreats, and air valve 8 opens the right side
The exhaustor 4 of side, disc aircraft flies to the left, and air valve 8 opens the exhaustor 4 in left side, and disc aircraft flies to the right,
After air valve 8 closes exhaustor 4, disc aircraft hovers in the air, controls the opening and closing of the exhaustor 4 of relevant position by air valve 8,
So that disc aircraft is flown to different directions, realize advance, retrogressing, hovering, translation and the steering of disc aircraft.
The disc aircraft that the present embodiment is related to can be fabricated to remote-control toy, take the photograph in the air according to different structure proportions
Shadow, low latitude ground reconnaissance, agriculture agriculture feelings nose into, disaster scene is searched and rescued and coastal waters field detects and searches and rescues equipment；Play as remote control
During tool, disk body 2 is fabricated to casper, places cartoon driver moulding personage, increase the interest of toy in carrying cabin 3,
As aerophotography, low latitude ground reconnaissance, agriculture agriculture feelings nose into, disaster scene is searched and rescued and coastal waters field detects and uses with searching and rescuing
When, carrying cabin is placed photographic goods, communications service, medicine flusher or relief equipment.
Claims (4)
1. a kind of disc aircraft is it is characterised in that agent structure includes plenum chamber, disk body, carrying cabin, exhaustor, lands and prop up
Frame, steam vent, high pressure draught feedway and air valve；The upper surface center of the disk body of platy structure is provided with hollow type streamline
The plenum chamber of type structure, at the position that plenum chamber is intersected with disk body, uniform intervals offer the row of 3-12 rectangular configuration
Pore, the inner space of plenum chamber is provided with high pressure draught feedway and air valve, high pressure draught feedway and air valve electricity
Connect, the lower surface center of disk body is provided with the carrying cabin of hollow type round rectangle structure, and the outer surface bottom of carrying cabin is equal
Even compartment is provided with the floor stand of 3-6 telescopic structure, and the perimeter uniform intervals formula of disk body is provided with 8-24 root
The exhaustor of hollow type cylindrical structural, exhaustor is stretched out and extended to by plenum chamber the outward flange of disk body, exhaustor and falling
Floor-engaging frame is electrically connected with air valve respectively.
2. disc aircraft according to claim 1 is it is characterised in that described plenum chamber is made using fairshaped outward appearance
Type, effectively reduces air drag；The shape of disk body includes circle, ellipse, tetragon, polygon and casper, disk body
Surface includes plane, the face of convex surface, concave surface and concavo-convex combination；Carrying cabin can load remote control device, communications service equipment
With imaging equipment or driving cabin and driver；The set location of exhaustor includes upper surface or the lower surface of disk body, and exhaustor is also
Can be embedded in the interlayer of disk body；Floor stand is in zoom state by Air Valve Control in disc aircraft flight course,
Floor stand is it after being in extended configuration in disc aircraft descent by Air Valve Control and landing in disc aircraft
Support force is provided；Steam vent can coordinate high pressure draught feedway to realize taking off, land and hovering of disc aircraft；High pressure
Air-flow feedway includes compressed air, plasma stream and high temperature and high pressure gas generator and aerator, and high pressure draught supplies
The flow velocity of the high pressure draught providing to device sets according to the weight of disc aircraft and size；Air valve selects electromagnetic gas valve, gas
Valve controls the switch of exhaustor, and when air valve is opened, with high pressure draught feedway in electrical communication, high pressure draught is from exhaustor for exhaustor
Middle ejection, when air valve is closed, high pressure draught stops spraying, and realizes the opening and closing of exhaustor by controlling the opening and closing of air valve, by gas
Valve controls the exhaustor of disk body various location to be capable of advance, retrogressing, hovering, translation and the steering of disc aircraft.
3. disc aircraft according to claim 1 is it is characterised in that when using, opening high pressure draught feedway, high
Pressure gas stream sprays along the upper surface of disk body through steam vent, and based on fluid mechanics principle, the pressure of high pressure draught is less than low speed
The pressure of air-flow, when high pressure draught flows through the upper surface of disk body, the pressure of disk body upper surface is less than the pressure of disk body lower surface,
Disk body is made to produce the power rising, the power of rising is more than the gravity of disc aircraft, disc aircraft begins to ramp up and takes off, due to row
During trachea jet, disc aircraft will fly to the direction in opposite direction with exhaustor jet, and during setting height of flying, air valve is opened
Open the exhaustor of rear side, disc aircraft advances, air valve opens the exhaustor of front side, disc aircraft retreats, air valve is opened right
The exhaustor of side, disc aircraft flies to the left, and air valve opens the exhaustor in left side, and disc aircraft flies to the right, gas
After valve cuts out exhaustor, disc aircraft hovers in the air, by the opening and closing of the exhaustor of Air Valve Control relevant position, makes dish-style
Aircraft flies to different directions, realizes advance, retrogressing, hovering, translation and the steering of disc aircraft.
4. disc aircraft according to claim 1 it is characterised in that can be fabricated to distant according to different structure proportions
Control toy, aerophotography, low latitude ground reconnaissance, agriculture agriculture feelings nose into, disaster scene is searched and rescued and coastal waters field detects and rescue device
Material；During as remote-control toy, disk body is fabricated to casper, places cartoon driver moulding personage in carrying cabin, increases and plays
The interest of tool, as aerophotography, low latitude ground reconnaissance, agriculture agriculture feelings nose into, disaster scene is searched and rescued and coastal waters field detects
During with searching and rescuing use, carrying cabin is placed photographic goods, communications service, medicine flusher or relief equipment.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611080166.4A CN106428559A (en) | 2016-11-30 | 2016-11-30 | Disc type aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201611080166.4A CN106428559A (en) | 2016-11-30 | 2016-11-30 | Disc type aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN106428559A true CN106428559A (en) | 2017-02-22 |
Family
ID=58224209
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN201611080166.4A Pending CN106428559A (en) | 2016-11-30 | 2016-11-30 | Disc type aircraft |
Country Status (1)
| Country | Link |
|---|---|
| CN (1) | CN106428559A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108180898A (en) * | 2017-12-28 | 2018-06-19 | 佛山市仲淳伟业科技有限公司 | A kind of flow measurement unmanned plane |
| 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 |
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| US4214720A (en) * | 1979-02-26 | 1980-07-29 | Desautel Edwin R | Flying disc |
| GB2270510A (en) * | 1992-09-11 | 1994-03-16 | Charles John Cochrane | Lift device. |
| CN1107113A (en) * | 1993-10-01 | 1995-08-23 | 杨文宇 | Disc shape flight device |
| CN2437594Y (en) * | 2000-05-17 | 2001-07-04 | 高恒伟 | Annular-wing helicopter |
| US6270036B1 (en) * | 1997-01-24 | 2001-08-07 | Charles S. Lowe, Jr. | Blown air lift generating rotating airfoil aircraft |
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| CN102310944A (en) * | 2011-06-24 | 2012-01-11 | 东北大学 | Disc type aircraft |
| CN104071331A (en) * | 2014-06-24 | 2014-10-01 | 谭燕斌 | Jet-propelled type airship stabilized by spinning tops |
| CN105083553A (en) * | 2015-09-07 | 2015-11-25 | 吴锜 | Dish-shaped vertical-flying type flight device |
| CN206231623U (en) * | 2016-11-30 | 2017-06-09 | 吴锜 | A kind of disc aircraft |
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| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US4014483A (en) * | 1975-09-15 | 1977-03-29 | Macneill Roderick M | Lighter-than-air craft |
| US4214720A (en) * | 1979-02-26 | 1980-07-29 | Desautel Edwin R | Flying disc |
| GB2270510A (en) * | 1992-09-11 | 1994-03-16 | Charles John Cochrane | Lift device. |
| CN1107113A (en) * | 1993-10-01 | 1995-08-23 | 杨文宇 | Disc shape flight device |
| US6270036B1 (en) * | 1997-01-24 | 2001-08-07 | Charles S. Lowe, Jr. | Blown air lift generating rotating airfoil aircraft |
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| CN2765859Y (en) * | 2005-01-25 | 2006-03-22 | 资解生 | Dynamic flying saucer |
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| CN105083553A (en) * | 2015-09-07 | 2015-11-25 | 吴锜 | Dish-shaped vertical-flying type flight device |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN108180898A (en) * | 2017-12-28 | 2018-06-19 | 佛山市仲淳伟业科技有限公司 | A kind of flow measurement unmanned plane |
| 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 |
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Application publication date: 20170222 |
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| RJ01 | Rejection of invention patent application after publication |