CN107672787A - Manned vehicle - Google Patents
Manned vehicle Download PDFInfo
- Publication number
- CN107672787A CN107672787A CN201710885716.8A CN201710885716A CN107672787A CN 107672787 A CN107672787 A CN 107672787A CN 201710885716 A CN201710885716 A CN 201710885716A CN 107672787 A CN107672787 A CN 107672787A
- Authority
- CN
- China
- Prior art keywords
- jet
- aircraft
- service creeper
- flight
- manned vehicle
- 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.)
- Pending
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/14—Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64C—AEROPLANES; HELICOPTERS
- B64C15/00—Attitude, flight direction, or altitude control by jet reaction
- B64C15/02—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets
- B64C15/12—Attitude, flight direction, or altitude control by jet reaction the jets being propulsion jets the power plant being tiltable
Abstract
The present invention is to provide manned vehicle, mainly solves simple one or double manned upper sky sightseeing or the war that fans the air;Project for tourism or war.Manufactured using the high bullet resistant material of the light weight electric jet plane of modern times invention and hard intensity, select the storage battery more than storing up electricity in light weight to power, light people operates aircraft using the body of health, protects itself using reflector layer or laser weapon or burns other side.Final realize eliminates the dream purpose that enemy protects oneself or tourism space sightseeing universe landscape, and suitable government investment production is promoted the use of.
Description
Technical field:The present invention is to provide manned vehicle, category aircraft field.
Background technology:So-called aircraft, is especially exclusively used in that manned aircraft is existing not to be had successfully, but for trying
The less successful aircraft tested but has varied, but how just can be designed that a successful manned vehicle
And be the fast and flexible that one uses, available for sightseeing or the bulletproof aircraft in battlefieldThis is that the present invention to be solved
Practical problem certainly.
The content of the invention:In order to invent it is a kind of be used to go sightseeing or battlefield, the shellproof double flexible manned vehicle of list,
Have to reference to cleverly dynamics Design scheme can just succeed using light-duty bullet resistant material first;According to current material selection just
It is more suitable to manufacture from carbon fibre material, in addition, power section is in addition to the line that conducts electricity is using metal material, remainder
It all should be manufactured using carbon materials, be advantageous to improve intensity and mitigate weight, including aircrew.Finally just it is hopeful
Succeed!Specific design allows the electronic light-duty jet for being located at carrier aircraft storehouse using lift form that is jet-propelled, rising subiculum
The gas that the puff prot of machine sprays is downward, in addition to recoil thrust upwards is provided to carrier aircraft, also by the air guide backward of three-dimensional coaming plate, makes
Generation thrust forward, when sucking air plus carrier aircraft front end air entry, due to the design air of also camber suction inlet enter it is fashionable
The strength of lifting forward and up can be produced, carrier aircraft front end can be made to be lifted up head, behind push away forward, bottom up liter, quickly
Carrier aircraft is just soared up to the sky, and heaven is flown with a loud crash, is gone sightseeing, is not influenceed by most on the service creeper of matrix of the people in carrier aircraft,
Can the flight of mobile operation carrier aircraft, can also freely operate various pressing switch, implementing to hit ground target for tasks.
Specific embodiment:In order to realize the purpose of the content of the invention, embodiment it is characterized in that:Using light material such as aluminium
The shellproof carrier aircraft service creeper of large, medium and small electronic jet plane made of alloy or carbon fibre material assembling, service creeper elastic cushion etc. zero
Part.
Then the beneath movable button button for large-scale jet plane being installed to streamlined recessed service creeper is consolidated, during for taking off, jet
The downward jet lifting carrier aircraft service creeper of mouth, then pulling jet plane to turn to spout, jet promotes carrier aircraft service creeper flight forward backward, to
Carrier aircraft service creeper wind-engaging holds in the palm the upward lifting of power of liter during preceding flight, as the effect aircraft wing, to high-altitude rapid flight;In order to allow
Manned vehicle, which can be realized, to be stayed aloft or steady slower flight, it is necessary to is installed in addition with two before and after among the bottom surface of carrier aircraft service creeper
Or corner is installed in addition with four miniature jet machines, one or two miniature two-way spray blower fan is installed among the front or rear end of carrier aircraft service creeper
Or afterbody installation wind direction rudder plate.When the former is used to stop jumble jet jet, starts two or four miniature jet machines are downward
Jet, carrier aircraft is allowed steadily to stay in the air;Or in jumble jet decelerating flight, utilize two or four miniature jet machines
Auxiliary jet downwards, the steady slower flight forward of adjustment carrier aircraft.The latter is used to adjust the leftward or rightward of manned vehicle or adjusted
The heading of head uses.Such as head mounted jet plane, jet, aircraft will fly to the right to the left, otherwise fly to the left,
Flight is reversed end for end as will be continuously turn-taked to left or right air injection aerial vehicle.As aircraft need to be allowed gently to land ground, using sliding
Or downward jet allows manned vehicle surely slow safety is landed in ground in right amount using big small-sized jet plane.It is manned in order to supply electricity to
Aircraft, using on center carrier aircraft service creeper, two high-energy batteries are installed in left and right on board the aircraft, i.e., existing storing up electricity weight is light
Storage battery, respectively the controlling switch with large, medium and small miniature jet plane electrically connect, for operating personnel's recumbency or crouch operation fly
The flight of row device is gone sightseeing or scouting of fighting, air battle or rescue refugee.In order to avoid manned vehicle is burnt up by laser weapon, should use
Patch reflector layer is filled at machine bottom, or installs laser weapon additional and is used to burn other side.In order to prevent the shell of adverse party or guided missile from shooting down load
People's aircraft, after big gun guided missile can be measured using airborne modern radar inductor, burnt up using laser irradiation in aerial.
Claims (2)
1. manned vehicle is mainly characterized by:Manned vehicle is manufactured from carbon fibre material, selects the most light Healthy People of body weight
Operation flight, select the storage battery power supply that the more body weight of storing up electricity are light;Specifically assembling its feature is successively:Using light material
The shellproof carrier aircraft service creeper of the large, medium and small electronic jet plane as made of aluminium alloy or carbon fibre material assembling, service creeper elastic cushion etc. zero
Part;Then the beneath movable button button for large-scale jet plane being installed to streamlined recessed service creeper is consolidated, during for taking off, puff prot to
Lower jet lifting carrier aircraft service creeper, then pulling jet plane to turn to spout, jet promotes carrier aircraft service creeper flight forward backward, flies forward
Carrier aircraft service creeper wind-engaging holds in the palm the upward lifting of power of liter during row, as the effect aircraft wing, to high-altitude rapid flight;It is manned in order to allow
Aircraft, which can be realized, to be stayed aloft or steady slower flight, it is necessary to is installed in addition with two or four before and after among the bottom surface of carrier aircraft service creeper
Angle is installed in addition with four miniature jet machines, and one or two miniature two-way spray blower fan or tail are installed among the front or rear end of carrier aircraft service creeper
Portion is installed by wind direction rudder plate;When the former is used to stop jumble jet jet, start two or four downward jets of miniature jet machine,
Carrier aircraft is allowed steadily to stay in the air;Or in jumble jet decelerating flight, it is downward using two or four miniature jet machines
Aid in jet, the steady slower flight forward of adjustment carrier aircraft;The latter is used for what is adjusted the leftward or rightward of manned vehicle or reverse end for end
Heading uses;Such as head mounted jet plane, jet, aircraft will fly to the right to the left, otherwise fly to the left, such as connect
Continue to turn-take to left or right air injection aerial vehicle and reverse end for end flight;As aircraft need to be allowed gently to land ground, using sliding or profit
With big small-sized jet plane, downward jet allows manned vehicle surely slow safety is landed in ground in right amount;In order to supply electricity to carry people to fly
Device, using on center carrier aircraft service creeper, two high-energy batteries, i.e., the light storage of existing storing up electricity weight are installed in left and right on board the aircraft
Battery, respectively the controlling switch with large, medium and small miniature jet plane electrically connect, for operating personnel's recumbency or the operation aircraft that crouches
Flight is gone sightseeing or scouting of fighting, air battle or rescue refugee.
2. the second feature of manned vehicle is:In order to avoid manned vehicle is burnt up by laser weapon, it should use and be filled at machine bottom
Reflector layer is pasted, or installs laser weapon additional and is used to burn other side, in order to prevent the shell of adverse party or guided missile from shooting down manned vehicle,
After big gun guided missile can be measured using airborne modern radar inductor, burnt up using laser irradiation in aerial.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710885716.8A CN107672787A (en) | 2017-09-25 | 2017-09-25 | Manned vehicle |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201710885716.8A CN107672787A (en) | 2017-09-25 | 2017-09-25 | Manned vehicle |
Publications (1)
Publication Number | Publication Date |
---|---|
CN107672787A true CN107672787A (en) | 2018-02-09 |
Family
ID=61138351
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201710885716.8A Pending CN107672787A (en) | 2017-09-25 | 2017-09-25 | Manned vehicle |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN107672787A (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN102105357A (en) * | 2008-05-30 | 2011-06-22 | 吉洛工业有限公司 | A flying machine comprising twin contra-rotating vertical axis propellers |
CN102186723A (en) * | 2008-10-20 | 2011-09-14 | 郑守铁 | Aircraft system that enables ground traveling |
GB2483933A (en) * | 2010-09-27 | 2012-03-28 | Lawrence Delcassian | Laser weapon mounted on aerial drone |
EP2463196A1 (en) * | 2010-12-10 | 2012-06-13 | Rheinmetall Waffe Munition GmbH | Passive protection for vehicles, in particular for flying objects and objects with at least one window |
US8827211B2 (en) * | 2007-10-23 | 2014-09-09 | Kevin Kremeyer | Laser-based flow modification to remotely control air vehicle flight path |
CN104925262A (en) * | 2015-07-10 | 2015-09-23 | 徐际长 | Electric flying saucer |
CN105584629A (en) * | 2014-10-19 | 2016-05-18 | 吴建伟 | Aircraft capable of vertically taking off and landing |
CN205770148U (en) * | 2016-05-21 | 2016-12-07 | 辽宁辽飞航空科技有限公司 | A kind of can the Fixed Wing AirVehicle of VTOL |
-
2017
- 2017-09-25 CN CN201710885716.8A patent/CN107672787A/en active Pending
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8827211B2 (en) * | 2007-10-23 | 2014-09-09 | Kevin Kremeyer | Laser-based flow modification to remotely control air vehicle flight path |
CN102105357A (en) * | 2008-05-30 | 2011-06-22 | 吉洛工业有限公司 | A flying machine comprising twin contra-rotating vertical axis propellers |
CN102186723A (en) * | 2008-10-20 | 2011-09-14 | 郑守铁 | Aircraft system that enables ground traveling |
GB2483933A (en) * | 2010-09-27 | 2012-03-28 | Lawrence Delcassian | Laser weapon mounted on aerial drone |
EP2463196A1 (en) * | 2010-12-10 | 2012-06-13 | Rheinmetall Waffe Munition GmbH | Passive protection for vehicles, in particular for flying objects and objects with at least one window |
CN105584629A (en) * | 2014-10-19 | 2016-05-18 | 吴建伟 | Aircraft capable of vertically taking off and landing |
CN104925262A (en) * | 2015-07-10 | 2015-09-23 | 徐际长 | Electric flying saucer |
CN205770148U (en) * | 2016-05-21 | 2016-12-07 | 辽宁辽飞航空科技有限公司 | A kind of can the Fixed Wing AirVehicle of VTOL |
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Legal Events
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PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
WD01 | Invention patent application deemed withdrawn after publication |
Application publication date: 20180209 |
|
WD01 | Invention patent application deemed withdrawn after publication |