CN103029833A - Novel aircraft - Google Patents
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- CN103029833A CN103029833A CN2012101077209A CN201210107720A CN103029833A CN 103029833 A CN103029833 A CN 103029833A CN 2012101077209 A CN2012101077209 A CN 2012101077209A CN 201210107720 A CN201210107720 A CN 201210107720A CN 103029833 A CN103029833 A CN 103029833A
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Abstract
The invention relates to a novel aircraft. The aerodynamic configuration of the novel aircraft and the orientation of a propeller of the novel aircraft can be changed, and the flight mode of the novel aircraft is relatively maneuverable and flexible. The novel aircraft in the first embodiment of the invention comprises a body, retractable wings and a propeller which can rotate by an angle of 180 degrees, the novel aircraft can take off and land vertically, fly at a high speed, perch in air and even retreat, one parts of the retractable wings are fixedly connected with the body of the novel aircraft by shafts, the other parts of the retractable wings are in wedge-shaped connected, the retractable wings are provided with a plurality of groups of vertical plates and further provided with a horizontal movement regulation mechanism of the propeller; a plurality of parts of the body of the novel aircraft are designed into downwards-inclined surfaces to overcome the pure resistance, and the novel aircraft is provided with anti-collision facilities such as a radar. The principle of the novel aircraft in the second embodiment of the invention is similar to the novel aircraft in the first embodiment in the principle, and only the wings are designed to be downwards foldable. The propellers of the novel aircrafts in the two embodiments can be designed as giant propellers arranged in the bodies of the novel aircrafts, and the propellers of the novel aircrafts are replaced by cylinders. Various aircrafts can be designed according to different needs. Particularly, an aircraft-mounted ship is bound to replace an aircraft carrier. The novel aircraft is low in cost, is safe to fly, can take off and land without being restricted by sites and even without an airport and is bound to replace the modern aircrafts.
Description
Technical field
The present invention relates to aviation aircraft, comprise fuselage, wing, screw propeller, empennage, transmission device and other electronic machine, substantially identical with existing aircraft, combine new structure design on this basis, make it to become a kind of aircraft that can the change of flight state.
Background technology
In the prior art, there is fixed wing the fuselage both sides of aircraft, and the arranged beneath of wing has screw propeller, screw propeller towards fixing, afterbody is equipped with empennage, this aircraft needs when taking off and land than long runway; Helicopter is subjected to again speed, the voyage restriction; The present invention is at utility model patent: a kind of type aircraft, improve on the basis of the patent No.: ZL200720000872.3, and make it to become the more superior aviation aircraft of a kind of performance.
Summary of the invention
The purpose of this invention is to provide a kind of type aircraft, its aerodynamic configuration and screw propeller towards can changing, flight attitude, flying method is maneuverability more, screw propeller can rotate by 180 degree, but vertical takeoff and landing, because wing can be taken down the exhibits, do not take up an area the face usable floor area, but vertical takeoff and landing does not need runway; There is wing can realize quick distance flight.Realize above-mentioned purpose, the present invention by the following technical solutions:
Embodiment one, and a kind of type aircraft has fuselage, the wing of can taking down the exhibits, can 180 the degree rotating screws, tailplane and the perpendicular wing etc.; The described wing of taking down the exhibits is connected in the fixed setting of fuselage with axle, a part is arranged to again the connection of contract type in addition, and the faster wing of speed is more steady, and wing arranges several groups of risers, the effect of existing reinforced rib, can improve raising force again, the length of wing is as the criterion with the fuselage forward position is concordant with after drawing in, and the outer of outer, the left and right sides and screw propeller is as the criterion, can be convenient to park, take down the exhibits with servomotor control, the bar of also can being arranged to stretch control also can be arranged to draw in backward; Described screw propeller can be that the cylindrical spiral oar also can be common screw propeller, screw propeller is with servomotor or other mechanical type control 180 degree rotations, to realize VTOL function, berth the speed row in the air, retreat, retreat and be suitable for speed and stop, screw propeller parallel motion regulating mechanism is set in addition, when load-carrying changes, be in all the time the center-of-gravity position of fuselage to guarantee screw propeller, ensure that complete machine was in horizontality when VTOL function berthed in the air, can be arranged to automatic adjusting and also can be arranged to manual regulation; About tailplane is arranged to two sections, adjustable respectively about angle, to regulate the state of flight of aircraft, be set together with the perpendicular wing of realizing turning function with rotatable, also can be separately positioned on the appropriate locations such as prow tail, also can be arranged to the turning facility of other form; Wheel can arrange damping spring, drive wheel can be set drive as car, is convenient to park, and also other alighting gear can be set as required; The front fuselage panel is arranged to lower inclined plane, can produce raising force when moving ahead; Overcome the pure resistance of conventional airplane, also dustpan shaped flanging can be set, to improve raising force; Outside all facilities of fuselage all design according to fluid mechanics principle; The position of wing and screw propeller can be adjusted as required, and wing and screw propeller all can be arranged to the form of many groups, and the anti-collision facility such as radar are set, and warns automatic dodging facility when wounding danger when arranging with the obstacle danger range; Other and conventional airplane are basic identical.
Embodiment two, a kind of type aircraft, its aerodynamic configuration and screw propeller towards can changing, flight attitude, flying method is maneuverability more, not limited by the place, but vertical takeoff and landing, also fast horizontal flight has widely comformability.
Wing design of the present invention becomes can descend fold-type, connect with hinge or alternate manner, wing and fuselage connecting portion are designed to wedge, the faster wing of horizontal flight speed and fuselage connect more firm, the current limliting thin plate is set on the wing, can improve lift about 10%, arrange thus and can play the reinforced rib effect, wing can make sheet-type, leading edge flanging, economical with materials, also shouldn't this setting, adopt common wing, wing is taken down the exhibits with quarter butt control, quarter butt has the effect of support simultaneously, can reduce the requirement to wing; Screw propeller adopts the cylindrical spiral oar, common screw propeller also can, place the position, center of gravity place of fuselage both sides, screw propeller can 180 degree rotations, realizing VTOL function, fast horizontal flight is berthed in the air and is retreated; Wing and propeller root need to arrange to organize in different appropriate locations according to difference more; The horizontal tail of difference angle adjustable about machine top afterbody arranges, and the rotatable perpendicular wing, to adjust state of flight, horizontal tail and the perpendicular wing also can place front end or place respectively the front and back end; Be provided with the spring wheel at the bottom of the machine, be convenient to park, but also can be arranged to drive wheel, can as car, drive, also can be arranged to the floating box type alighting gear and add trundle; Setting is in the facility at the center of gravity position of complete machine all the time under different load conditions in order to propeller blades, be in horizontality to keep the complete machine landing stopping time, the position of screw propeller and wing as required front and back exchanges, and also can take prow and tail respectively to establish the form of one or one group screw propeller; The anti-collision facility such as radar are set.
The machine top is arranged to dustpan-shaped, produce negative pressure during horizontal flight, front end is arranged to inclined-plane shape, other establishes an angle adjustable sloping desk, with gemel connection in front panel, with the strut bar adjusting angle, back segment arranges the inclined-plane wing at the bottom of the car, the effect of wing is all played in these several settings, cooperates tailplane and the perpendicular wing, can not want wing realization VTOL function level and flies fast; When adopting lower folding wing, also shouldn't above-mentioned roof dustpan-shaped, front end adds sloping desk, three kinds of settings of tail end sloping desk at the bottom of the car; Adopt simultaneously all to arrange better.
The screw propeller of above-mentioned two examples all can be arranged to a huge screw propeller is arranged in the body, the screw propeller that replaces above-mentioned two examples with cylinder, cylinder can 180 the degree rotation, the cylinder of air-flow Jet with downward flow direction is set simultaneously, can be downwards jet-stream wind backward, get final product 90 degree rotations, also can be arranged to 180 degree rotations, to realize VTOL function, the speed row, berth in the air, even retreat; It is a plurality of that cylinder all can in position arrange many groups; Upper two routine wing moulding can become various shapes with different airplane design according to the body shape.
The present invention can be made into small-sized private savings aircraft, large transport airplane, airliner, military aircraft according to different needs, unmanned plane, toy airplanes etc. are particularly suited for carrier-borne aircraft, to release aircraft carrier and release military stage, an aircraft carrier can be built several carrier aircraft warships, and the aircraft carrier change will become inevitable; Owing to the present invention can realize vertical takeoff and landing, the speed row berths in the air, even retreats, and does not need runway to make because the aircraft carrier that existed by the runway restriction loses and has necessity, and the carrier aircraft warship will replace; Because wing can take down the exhibits or vertical folding, do not account for usable floor area, so the carrier aircraft warship can be arranged to the many lattice of multilayer by the armoring type parking facilities of drawer type of being made by steel plate of department's dress system control, open drawer and be convenient to takeoff and landing; The filling of fuel and ammunition can take to change the form of fuel tank or ammunition box, can accelerate operation tempo; Not only safety cost but also low, collecting and distributing freedom is lost a number and can be gone on the war-path, and can improve the fight capability several times, and bow is taked V font design slanting, reduces resistance; Propelling unit is taked the cylindrical spiral oar, can improve thrust more than 10%, and the fried facility of metal net shaped protection can be set in addition, makes shell, and torpedo etc. explode on the net outside warship, reduce the loss of battleship.
Cost of the present invention is low, and driving safety is not limited by or not the place, does not need the airport, will replace existing aircraft.
Description of drawings
Fig. 1 is the structural principle scheme drawing of embodiments of the invention one.
Fig. 2 is the structural principle scheme drawing of wing.
Fig. 3 is the structural principle scheme drawing of embodiments of the invention two.
Fig. 4 is that lower flap is connected enlarged diagram with the wedge of fuselage.
Fig. 5 is the rod-type of the lower flap scheme drawing of taking down the exhibits.
The specific embodiment
Embodiment one: with reference to Fig. 1, Fig. 2, the present invention is a kind of type aircraft, has fuselage 1, the wing 3 of can taking down the exhibits, can 180 the screw propeller 2 of degree rotation, tailplane 6,8 and the perpendicular wing 7 etc.; The described wing 3 of taking down the exhibits is connected in axle 5 that fuselage 1 is fixed to arrange 18, a part is arranged to again contract type 4 and 13 connections in addition, the faster wing of speed 3 is more steady, wing 3 arranges several groups of risers 12, the effect of existing reinforced rib, can improve raising force again, the length of wing 3 with after drawing in concordant being as the criterion in fuselage 1 forward position, the outer of outer, the left and right sides and screw propeller 2 is as the criterion, can be convenient to park, take down the exhibits with servomotor control the bar of also can being arranged to stretch control, also can be arranged to draw in backward, 5 and 19 is connecting shaft holes of wing; Described screw propeller 2 can be that the cylindrical spiral oar also can be common screw propeller, screw propeller 2 is with servomotor or other mechanical type control 180 degree rotations, to realize VTOL function, berth the speed row in the air, retreat, retreat and be suitable for speed and stop, screw propeller 2 parallel motion regulating mechanisms are set in addition, when load-carrying changes, be in all the time the center-of-gravity position of fuselage 1 to guarantee screw propeller 2, ensure that complete machine was in horizontality when VTOL function berthed in the air, can be arranged to automatic adjusting and also can be arranged to manual regulation; About tailplane 6,8 is arranged to two sections, angle left 6 right 8 is adjustable respectively, to regulate the state of flight of aircraft, is set together with the perpendicular wing 7 of realizing turning function with rotatable, also can be separately positioned on the appropriate locations such as prow tail; Wheel 11 can arrange damping spring 10, drive wheel can be set drive as car, is convenient to park, and also other alighting gear can be set as required; Fuselage 1 front console is arranged to lower inclined plane 16,17, is provided with lower form on 17, and the 15th, be arranged at the transparent part for front sight on the inclined-plane 16, can produce raising force when moving ahead, overcome the pure resistance of conventional airplane, also dustpan shaped flanging can be set, to improve raising force; Outside all facilities of fuselage all design according to fluid mechanics principle; Wing 3 can be adjusted as required with the position of screw propeller 2, and wing 3 all can be arranged to the forms of organizing with screw propeller 2 more, and the radar collision facility is set; Other and conventional airplane are basic identical.
The present invention be its aerodynamic configuration of a kind of type aircraft and screw propeller towards changing, flight attitude, flying method are more
Add maneuverability, screw propeller can rotate by 180 degree, but vertical takeoff and landing because wing can be taken down the exhibits, do not take up an area the face usable floor area, but vertical takeoff and landing does not need runway; There is wing can realize quick distance flight, driving safety, cost is low, is worthy to be popularized.
Embodiment two: with reference to Fig. 3, and Fig. 4, Fig. 5, a kind of type aircraft has the wing 22 that can descend folding, and wing 22 is connected in modes such as hinges 34 with fuselage 20, wedge is arranged in the contact site, the recessed end 15 of wedge, nose 35, be provided with current limliting thin plate 23 on the wing 22, the machine top is designed to the dustpan shaped of flanging 24, produces negative pressure during horizontal flight, the fuselage front panel is arranged to inclined-plane shape, and other establishes the sloping desk 28 of angle adjustable, connects with hinge and front panel, with strut bar 36 adjusting angles, the 29th, window, the 30th, dustpan-shaped flanging, the 31st, be provided with the trundle of spring 32, can be arranged to drive wheel as drive, conveniently park, the 25th, about can distinguish horizontal tail and the rotatable perpendicular wing of hue angle, the 26th, sloping desk, 24,28,26,25 cooperate front bevel can not want wing 22 levels flies fast, can not want 24,28,26 by wing 22 yet; The 33rd, aircraft window, the 21st, can 180 the cylindrical spiral oar of degree rotation, also can use common screw propeller, to realize VTOL function, level is flown fast, berth in the air and retreat, the 36th, the strut bar that the control wing is taken down the exhibits has again the effect of strengthening wing.
The screw propeller of above-mentioned two examples all can be arranged to a huge screw propeller is arranged in the body, the screw propeller that replaces above-mentioned two examples with cylinder, cylinder can 180 the degree rotation, the cylinder of air-flow Jet with downward flow direction is set simultaneously, can be downwards jet-stream wind backward, get final product 90 degree rotations, also can be arranged to 180 degree rotations, to realize VTOL function, the speed row, berth in the air, even retreat; It is a plurality of that cylinder all can in position arrange many groups; Upper two routine wing moulding can become various shapes (not indicating among the figure) according to the body shape with different airplane design.
The present invention can be made into small-sized private savings aircraft, large transport airplane, airliner, military aircraft according to different needs, unmanned plane, toy airplanes etc. are particularly suited for carrier-borne aircraft, to release aircraft carrier and release military stage, an aircraft carrier can be built several carrier aircraft warships, and the aircraft carrier change will become inevitable; Owing to the present invention can realize vertical takeoff and landing, the speed row berths in the air, even retreats, and does not need runway to make because the aircraft carrier that existed by the runway restriction loses and has necessity, and the carrier aircraft warship will replace; Because wing can take down the exhibits or vertical folding, do not account for usable floor area, so the carrier aircraft warship can be arranged to the many lattice of multilayer by the armoring type parking facilities of drawer type of being made by steel plate of department's dress system control, open drawer and be convenient to takeoff and landing; The filling of fuel and ammunition can take to change the form of fuel tank or ammunition box, can accelerate operation tempo; Not only safety cost but also low, collecting and distributing freedom is lost a number and can be gone on the war-path, and can improve the fight capability several times, and bow is taked V font design slanting, reduces resistance; Propelling unit is taked the cylindrical spiral oar, can improve thrust more than 10%, and the fried facility of metal net shaped protection can be set in addition, makes shell, and torpedo etc. explode on the net outside warship, reduces the loss (not indicating among the figure) of battleship.
Cost of the present invention is low, and driving safety does not need the airport, has good potentiality to be exploited.
Claims (6)
1. type aircraft, it is characterized in that its aerodynamic configuration and screw propeller towards can changing, flight attitude, flying method is maneuverability more, screw propeller can rotate by 180 degree, but vertical takeoff and landing, because wing can be taken down the exhibits or lower folding, do not take up an area the face usable floor area, but vertical takeoff and landing does not need runway; There is wing can realize quick distance flight.
2. a kind of type aircraft according to claim 1, embodiment one, it is characterized in that having fuselage, and the wing of can taking down the exhibits can 180 degree rotating screws, tailplane and the perpendicular wing etc.; The described wing of taking down the exhibits is connected in the fixed setting of fuselage with axle, a part is arranged to again the connection of contract type in addition, and the faster wing of speed is more steady, and wing arranges several groups of risers, the effect of existing reinforced rib, can improve raising force again, the length of wing is as the criterion with the fuselage forward position is concordant with after drawing in, and the outer of outer, the left and right sides and screw propeller is as the criterion, can be convenient to park, take down the exhibits with servomotor control, the bar of also can being arranged to stretch control also can be arranged to draw in backward; Described screw propeller can be that the cylindrical spiral oar also can be common screw propeller, screw propeller is with servomotor or other mechanical type control 180 degree rotations, to realize VTOL function, berth the speed row in the air, retreat, retreat and be suitable for speed and stop, screw propeller parallel motion regulating mechanism is set in addition, when load-carrying changes, be in all the time the center-of-gravity position of fuselage to guarantee screw propeller, ensure that complete machine was in horizontality when VTOL function berthed in the air, can be arranged to automatic adjusting and also can be arranged to manual regulation; About tailplane is arranged to two sections, adjustable respectively about angle, to regulate the state of flight of aircraft, be set together with the perpendicular wing of realizing turning function with rotatable, also can be separately positioned on the appropriate locations such as prow tail, also can be arranged to the turning facility of other form; Wheel can arrange damping spring, drive wheel can be set drive as car, is convenient to park, and also other alighting gear can be set as required; The front fuselage panel is arranged to lower inclined plane, can produce raising force when moving ahead; Overcome the pure resistance of conventional airplane, also dustpan shaped flanging can be set, to improve raising force; Outside all facilities of fuselage all design according to fluid mechanics principle; The position of wing and screw propeller can be adjusted as required, and wing and screw propeller all can be arranged to the form of many groups, and the anti-collision facility such as radar are set, and warns automatic dodging facility when wounding danger when arranging with the obstacle danger range; Other and conventional airplane are basic identical.
3. a kind of type aircraft according to claim 1, embodiment two, it is characterized in that wing design of the present invention becomes can descend fold-type, connect with hinge or alternate manner, wing and fuselage connecting portion are designed to wedge, and the faster wing of horizontal flight speed and fuselage connect more firm, and the current limliting thin plate is set on the wing, can improve lift about 10%, arrange thus and can play the reinforced rib effect, wing can make sheet-type, leading edge flanging, economical with materials, also shouldn't this setting, adopt common wing, wing is taken down the exhibits with quarter butt control, quarter butt has the effect of support simultaneously, can reduce the requirement to wing; Screw propeller adopts the cylindrical spiral oar, common screw propeller also can, place the position, center of gravity place of fuselage both sides, screw propeller can 180 degree rotations, realizing VTOL function, fast horizontal flight is berthed in the air and is retreated; Wing and propeller root need to arrange to organize in different appropriate locations according to difference more; The horizontal tail of difference angle adjustable about machine top afterbody arranges, and the rotatable perpendicular wing, to adjust state of flight, horizontal tail and the perpendicular wing also can place front end or place respectively the front and back end; Be provided with the spring wheel at the bottom of the machine, be convenient to park, but also can be arranged to drive wheel, can as car, drive, also can be arranged to the floating box type alighting gear and add trundle; Setting is in the facility at the center of gravity position of complete machine all the time under different load conditions in order to propeller blades, be in horizontality to keep the complete machine landing stopping time, the position of screw propeller and wing as required front and back exchanges, and also can take prow and tail respectively to establish the form of one or one group screw propeller; The anti-collision facility such as radar are set; The machine top is arranged to dustpan-shaped, produce negative pressure during horizontal flight, front end is arranged to inclined-plane shape, other establishes an angle adjustable sloping desk, with gemel connection in front panel, with the strut bar adjusting angle, back segment arranges the inclined-plane wing at the bottom of the car, the effect of wing is all played in these several settings, cooperates tailplane and the perpendicular wing, can not want wing realization VTOL function level and flies fast; When adopting lower folding wing, also shouldn't above-mentioned roof dustpan-shaped, front end adds sloping desk, three kinds of settings of tail end sloping desk at the bottom of the car; Adopt simultaneously all to arrange better.
4. according to claim 1,2,3 described a kind of type aircrafts, the screw propeller that it is characterized in that above-mentioned two examples all can be arranged to a huge screw propeller is arranged in the body, replaces the screw propeller of above-mentioned two examples with cylinder, and cylinder can 180 degree rotations, the cylinder of air-flow Jet with downward flow direction is set simultaneously, can be downwards jet-stream wind backward, get final product 90 degree rotations, also can be arranged to 180 degree rotations, to realize VTOL function, the speed row berths in the air, even retreats; It is a plurality of that cylinder all can in position arrange many groups; Upper two routine wing moulding can become various shapes with different airplane design according to the body shape.
5. a kind of type aircraft according to claim 1, it is characterized in that the present invention can be made into small-sized private savings aircraft according to different needs, large transport airplane, airliner, military aircraft, unmanned plane, the various aircrafts such as toy airplane are particularly suited for carrier-borne aircraft, and aircraft carrier is released military stage, the aircraft carrier change will become inevitable, and the armoring carrier aircraft warship of drawer type will become twin patent of invention of the present invention.
6. a kind of type aircraft according to claim 1 is characterized in that can realizing vertical takeoff and landing owing to the present invention, and the speed row berths in the air, even retreats, and does not need runway to make because the aircraft carrier that existed by the runway restriction loses and has necessity, and the carrier aircraft warship will replace; Because wing can take down the exhibits or vertical folding, do not account for usable floor area, so the carrier aircraft warship can be arranged to the many lattice of multilayer by the armoring type parking facilities of drawer type of being made by steel plate of department's dress system control, open drawer and be convenient to takeoff and landing; The filling of fuel and ammunition can take to change the form of fuel tank or ammunition box, can accelerate operation tempo; Not only safety cost but also low, collecting and distributing freedom is lost a number and can be gone on the war-path, and can improve the fight capability several times, and bow is taked V font design slanting, reduces resistance; Propelling unit is taked the cylindrical spiral oar, can improve thrust more than 10%, and the fried facility of metal net shaped protection can be set in addition, makes shell, and torpedo etc. explode on the net outside warship, reduce the loss of battleship.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012101077209A CN103029833A (en) | 2011-10-08 | 2012-04-07 | Novel aircraft |
Applications Claiming Priority (3)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN201110311041.9 | 2011-10-08 | ||
| CN201110311041 | 2011-10-08 | ||
| CN2012101077209A CN103029833A (en) | 2011-10-08 | 2012-04-07 | Novel aircraft |
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| CN103029833A true CN103029833A (en) | 2013-04-10 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN2012101077209A Pending CN103029833A (en) | 2011-10-08 | 2012-04-07 | Novel aircraft |
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Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416586A (en) * | 2015-12-07 | 2016-03-23 | 安宇 | Performance stage capable of achieving flying |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1190072A (en) * | 1997-02-08 | 1998-08-12 | 贺瑞华 | Fish herding airplane |
| CN1544289A (en) * | 2003-11-21 | 2004-11-10 | 骞 穆 | Oneman vertical takeoff and landing aerial craft with double leaning and rotating culvert fan |
| CN200995782Y (en) * | 2007-01-17 | 2007-12-26 | 赵文志 | Airplane |
| CN101314409A (en) * | 2008-07-10 | 2008-12-03 | 周武双 | Swallow type inclined rotation rotorcraft |
| CN101885295A (en) * | 2010-07-19 | 2010-11-17 | 杨朝习 | Land and air double-used aircraft |
| CN102126553A (en) * | 2010-01-12 | 2011-07-20 | 北京航空航天大学 | Vertically taking off and landing small unmanned aerial vehicle |
-
2012
- 2012-04-07 CN CN2012101077209A patent/CN103029833A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1190072A (en) * | 1997-02-08 | 1998-08-12 | 贺瑞华 | Fish herding airplane |
| CN1544289A (en) * | 2003-11-21 | 2004-11-10 | 骞 穆 | Oneman vertical takeoff and landing aerial craft with double leaning and rotating culvert fan |
| CN200995782Y (en) * | 2007-01-17 | 2007-12-26 | 赵文志 | Airplane |
| CN101314409A (en) * | 2008-07-10 | 2008-12-03 | 周武双 | Swallow type inclined rotation rotorcraft |
| CN102126553A (en) * | 2010-01-12 | 2011-07-20 | 北京航空航天大学 | Vertically taking off and landing small unmanned aerial vehicle |
| CN101885295A (en) * | 2010-07-19 | 2010-11-17 | 杨朝习 | Land and air double-used aircraft |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN105416586A (en) * | 2015-12-07 | 2016-03-23 | 安宇 | Performance stage capable of achieving flying |
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Application publication date: 20130410 |