CN204020446U - The pusher hovercar of screw wing - Google Patents
The pusher hovercar of screw wing Download PDFInfo
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- CN204020446U CN204020446U CN201320470440.4U CN201320470440U CN204020446U CN 204020446 U CN204020446 U CN 204020446U CN 201320470440 U CN201320470440 U CN 201320470440U CN 204020446 U CN204020446 U CN 204020446U
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Abstract
The utility model relates to the pusher hovercar of a kind of screw wing, by to independent multiple stage spiral pushing device in the pusher hovercar of screw wing, wheel transmission, wheel steering control system, image capturing device, radar detection induction installation, signal receiving and transmitting unit, the unique design of the structures such as telecommunication control system and annexation, overcome in prior art spiral wing huge, can only adopt fixed-wing, need to fix runway, screw propulsion power and precision deficiency, the departure that flight image acquisition inaccuracy causes is large, the unstable technical barrier that waits flies, realize the pusher structure Heliflying automobile of screw wing that a kind of volume is little, practicality is high, screw propulsion power is strong, precision is high, remote controlled.
Description
Technical field
The present invention relates to automobile Flight Design control modelling technique field, relate in particular to a kind of hovercar with screw wing, relate in particular the pusher hovercar of a kind of screw wing.
Background technology
Flourish along with computer technology, the communication technology and Eltec, in the world the research of automobile aerocraft is formed to upsurge gradually, but still in the design concept stage, many technical matterss is still difficult to solve.Helicopter relatively, Fixed Wing AirVehicle has that flight efficiency is high, flying speed is fast, flying distance is far away, system architecture is simple, lightweight, cost and the advantage such as usage charges are low, but Fixed Wing AirVehicle also has self inevitable defect, that is exactly in the time taking off and land, need to slide to run or utilize special transmitting regenerative apparatus.
Vertical takeoff and landing technology has aircraft to integrate the performance of helicopter and fixed-wing, the possibility of advantage.The more successful vertical takeoff and landing scheme of application mainly contains at present: tilting rotor formula, tilting duct formula, the fuselage formula of verting and rotor/wing change type.Wherein in first two scheme, thrust direction can be rotated around fuselage transverse axis, and fuselage keeps level awing substantially, the fuselage formula of verting can only realize short take-off and landing (STOL), and the rotor stall under horizontal flight pattern of rotor/wing change type changes into by screw propeller or the alternate manner such as jet thrust is provided.These schemes all have thrust switching mechanism or engine installation complexity, shortcoming that annex quality is large, are unfavorable for the small light of aircraft and the raising of flight efficiency.
Tail sitting posture, as another kind of vertical takeoff and landing scheme, is applied less.Have in early days the Heliwing of Boeing, Heliwing need to reach a certain height there is speed just can be from vertically transferring horizontal flight to, thereby its flight is subject to some restrictions; And from vertically also can moving with one " stall rolling " to the transition flight of level, this has just brought certain danger to flight.The crash of final first Heliwing in test flight, is cancelled this project.
The existing device of going straight up to can only aloft fly, can not travel on the ground, maneuvering performance is poor, steering operation control is insensitive, bring much inconvenience to user, while on the way particularly breaking down on road surface, be difficult to deal with, therefore its range of use only limits to army, public security department's operation, transport and salvage work.U.S. Patent application US-9067622A discloses a kind of carplane, is that one adds aircraft manufacturing technology by bicycle, can be on ground from running the goal of the invention that can fly again aloft to reach.But by its patent application specification, we can not find its concrete technical scheme, can be found out by its Figure of description, this carplane unreasonable structure, its main weight is concentrated front wheel, once driving engine et out of order, without countrmeasure, danger is very large again.French Patent (FRP) FR1265234 disclose a kind of not only can be at ground run but also the vehicle that can fly, but its version is comparatively single, can not meet multiduty needs.
The research of comprehensive existing document and existing correlation technique, the inventor finds the hovercar of reporting or realizing at present both at home and abroad, is substantially all fixed-wing, need to fix runway, greatly limits its application scenario.Existing screw wing implementation method is also substantially in theory stage, and screw wing wing is huge, is unfavorable for practical application.There is no a kind of feasible implementation method.
Summary of the invention
The object of the invention is the deficiencies in the prior art for correlative technology field document, on the basis of a large amount of existing literature research and the long-term hovercar Development Practice of the inventor, by to independent multiple stage spiral pushing device in the pusher hovercar of screw wing, wheel transmission, wheel steering control system, image capturing device, radar detection induction installation, signal receiving and transmitting unit, the unique design of the structures such as telecommunication control system and annexation, overcome in prior art spiral wing huge, can only adopt fixed-wing, need to fix runway, screw propulsion power and precision deficiency, the departure that flight image acquisition inaccuracy causes is large, the unstable technical barrier that waits flies, realize a kind of volume little, practicality is high, screw propulsion power is strong, precision is high, the pusher structure Heliflying automobile of remote controlled screw wing.
For achieving the above object, the present invention is achieved by the following technical solutions:
The pusher hovercar of a kind of screw wing of the present invention, the pusher hovercar of this screw wing comprises described left back drive wheel, above-mentioned right back drive wheel, left front wheel flutter, right front wheel flutter, vehicle body matrix, above-mentioned four groups of independence multiple stage spiral pushing devices, two wheel transmissions, two wheel steering control system, three image capturing devices, radar detection induction installation, signal receiving and transmitting unit, telecommunication control system, it is characterized in that, described left front wheel flutter, right front wheel flutter, left back drive wheel, right back drive wheel is installed on respectively the symmetrical position of the front and back end of above-mentioned vehicle body matrix, described four groups of independence multiple stage spiral pushing devices are installed on respectively described left back drive wheel, right back drive wheel, left front wheel flutter, the central interior position of right front wheel flutter, described two wheel transmissions are built in respectively described left back drive wheel and described right back drive wheel inner bottom part midway location, each described wheel transmission comprises engine installation and multiple driving gear set, wherein, described left front wheel flutter and described right front wheel flutter are rotationally connected by left front deflecting bar and right front deflecting bar and described vehicle body matrix respectively, described two wheel steering control system are built in respectively above-mentioned left front deflecting bar and right front deflecting bar, an and side of close described left front wheel flutter and described right front wheel flutter respectively, described three image capturing devices are installed on vehicle body matrix front portion, afterbody and bottom, described radar detection induction installation is arranged on respectively described vehicle body matrix bottom, afterbody and two side positions, described signal receiving and transmitting unit is built in the forebody of above-mentioned vehicle body matrix inside, and described telecommunication control system is built in the latter half of of above-mentioned vehicle body matrix inside, wherein, described signal receiving and transmitting unit inside is equipped with signal receiving unit successively, acquisition of signal is sorted out accumulation unit, signal filter element, signal transmitter unit, described telecommunication control system comprises signal acquisition module, signal processing module, signal conversion module, signal transmission module, signal main control module, signal emission module successively.
Wherein, described independent multiple stage spiral pushing device comprises screw shaft, multiple screw propulsion sheet, screw propeller, wherein, described screw shaft is the quill shaft that is evenly provided with multiple air bleeders, described multiple screw propulsion sheet is multiple oval screw propulsion sheets, described screw propeller surfaces externally and internally multiple uneven oval hold down grooves of cutting sth. askew out, every two axial angles of uneven oval hold down groove are less than 5 degree and are greater than 3 degree, described multiple oval screw propulsion sheet correspondence is arranged in above-mentioned oval hold down groove, each described oval screw propulsion sheet is made up of multiple segmentation materials, and at least one segmentation material is prepared from by glass-epoxy panel, each described image capturing device inside comprises left end camera element from left to right successively, left end vibrationproof unit, graphicinformation receiving element, graphicinformation monitoring acquisition elements, graphicinformation converting unit, graphicinformation transmitter unit, right-hand member vibrationproof unit, right-hand member camera element, wherein, described left end vibrationproof unit and described right-hand member vibrationproof unit all comprise ellipticity annular elastomeric, multiple bar shaped triangle side friction supporting masses, angle orientation film, described ellipticity annular elastomeric upper surface is evenly provided with multiple circular protrusions portion, described circular protrusions deployed in described bar shaped triangle side friction supporting mass, described angle orientation film is fixed between described lug boss and described bar shaped triangle side friction supporting mass.
Wherein, the pusher hovercar of described screw wing also can comprise two of left and right wing, former and later two vertical tails, fairing; Two of described left and right wing symmetry is arranged on above-mentioned vehicle body matrix left and right sidepiece, described former and later two vertical tail symmetries are arranged on sidepiece before and after above-mentioned vehicle body matrix, and front end is provided with rolling pitch control subsystem outer arcuate rudder face and arc rudder face is controlled in driftage outside each described wing; Outside each described vertical tail, front end is provided with rolling pitch control subsystem arc rudder face and driftage control outer arcuate rudder face.
The beneficial effect that the present invention also possesses:
This Heliflying automobile can be realized high-speed motion on the ground, can aloft fly, and clear an obstacle.Screw wing takes up space little, mobility strong.Vertical takeoff and landing mode, has reduced the requirement to place, ground, can be applicable to multiple occasion.The present invention further realizes tele-control system, can realize the task such as long range exploration, air transport under unmanned state, gathers around and holds out broad prospects; Compared to existing technology:
One, large scale crawler wheel drive, exercise in land route has very high-speed and very strong cross country power;
Two, screw wing space is little, can realize landing in little spatial dimension, mobility strong;
Three, wheel and screw wing are combined as a whole, and save space, easily manufactured;
Four, can realize remote control in the unmanned situation of aircraft.
Brief description of the drawings
Fig. 1 is the structural representation that the pusher hovercar of a kind of screw wing of the present invention is overlooked.
Wherein: 1 is right front wheel flutter; 2 is left front wheel flutter; 3 is right back drive wheel; 4 is left back drive wheel; 5 is vehicle body matrix; 6 is screw propulsion sheet.
Detailed description of the invention
Below in conjunction with Fig. 1 and detailed description of the invention, further set forth the present invention.
Embodiment 1:
The pusher hovercar of a kind of screw wing, the pusher hovercar of this screw wing comprises described left back drive wheel, above-mentioned right back drive wheel, left front wheel flutter, right front wheel flutter, vehicle body matrix, above-mentioned four groups of independence multiple stage spiral pushing devices, two wheel transmissions, two wheel steering control system, three image capturing devices, radar detection induction installation, signal receiving and transmitting unit, telecommunication control system, it is characterized in that, described left front wheel flutter, right front wheel flutter, left back drive wheel, right back drive wheel is installed on respectively the symmetrical position of the front and back end of above-mentioned vehicle body matrix, described four groups of independence multiple stage spiral pushing devices are installed on respectively described left back drive wheel, right back drive wheel, left front wheel flutter, the central interior position of right front wheel flutter, described two wheel transmissions are built in respectively described left back drive wheel and described right back drive wheel inner bottom part midway location, each described wheel transmission comprises engine installation and multiple driving gear set, wherein, described left front wheel flutter and described right front wheel flutter are rotationally connected by left front deflecting bar and right front deflecting bar and described vehicle body matrix respectively, described two wheel steering control system are built in respectively above-mentioned left front deflecting bar and right front deflecting bar, an and side of close described left front wheel flutter and described right front wheel flutter respectively, described three image capturing devices are installed on vehicle body matrix front portion, afterbody and bottom, described radar detection induction installation is arranged on respectively described vehicle body matrix bottom, afterbody and two side positions, described signal receiving and transmitting unit is built in the forebody of above-mentioned vehicle body matrix inside, and described telecommunication control system is built in the latter half of of above-mentioned vehicle body matrix inside, wherein, described signal receiving and transmitting unit inside is equipped with signal receiving unit successively, acquisition of signal is sorted out accumulation unit, signal filter element, signal transmitter unit, described telecommunication control system comprises signal acquisition module, signal processing module, signal conversion module, signal transmission module, signal main control module, signal emission module successively.
Embodiment 2:
The pusher hovercar of a kind of screw wing, the pusher hovercar of this screw wing comprises described left back drive wheel, above-mentioned right back drive wheel, left front wheel flutter, right front wheel flutter, vehicle body matrix, above-mentioned four groups of independence multiple stage spiral pushing devices, two wheel transmissions, two wheel steering control system, three image capturing devices, radar detection induction installation, signal receiving and transmitting unit, telecommunication control system, it is characterized in that, described left front wheel flutter, right front wheel flutter, left back drive wheel, right back drive wheel is installed on respectively the symmetrical position of the front and back end of above-mentioned vehicle body matrix, described four groups of independence multiple stage spiral pushing devices are installed on respectively described left back drive wheel, right back drive wheel, left front wheel flutter, the central interior position of right front wheel flutter, described two wheel transmissions are built in respectively described left back drive wheel and described right back drive wheel inner bottom part midway location, each described wheel transmission comprises engine installation and multiple driving gear set, wherein, described left front wheel flutter and described right front wheel flutter are rotationally connected by left front deflecting bar and right front deflecting bar and described vehicle body matrix respectively, described two wheel steering control system are built in respectively above-mentioned left front deflecting bar and right front deflecting bar, an and side of close described left front wheel flutter and described right front wheel flutter respectively, described three image capturing devices are installed on vehicle body matrix front portion, afterbody and bottom, described radar detection induction installation is arranged on respectively described vehicle body matrix bottom, afterbody and two side positions, described signal receiving and transmitting unit is built in the forebody of above-mentioned vehicle body matrix inside, and described telecommunication control system is built in the latter half of of above-mentioned vehicle body matrix inside, wherein, described signal receiving and transmitting unit inside is equipped with signal receiving unit successively, acquisition of signal is sorted out accumulation unit, signal filter element, signal transmitter unit, described telecommunication control system comprises signal acquisition module, signal processing module, signal conversion module, signal transmission module, signal main control module, signal emission module successively, described independent multiple stage spiral pushing device comprises screw shaft, multiple screw propulsion sheet, screw propeller, wherein, described screw shaft is the quill shaft that is evenly provided with multiple air bleeders, described multiple screw propulsion sheet is multiple oval screw propulsion sheets, described screw propeller surfaces externally and internally multiple uneven oval hold down grooves of cutting sth. askew out, every two axial angles of uneven oval hold down groove are less than 5 degree and are greater than 3 degree, described multiple oval screw propulsion sheet correspondence is arranged in above-mentioned oval hold down groove, each described oval screw propulsion sheet is made up of multiple segmentation materials, and at least one segmentation material is prepared from by glass-epoxy panel, each described image capturing device inside comprises left end camera element from left to right successively, left end vibrationproof unit, graphicinformation receiving element, graphicinformation monitoring acquisition elements, graphicinformation converting unit, graphicinformation transmitter unit, right-hand member vibrationproof unit, right-hand member camera element, wherein, described left end vibrationproof unit and described right-hand member vibrationproof unit all comprise ellipticity annular elastomeric, multiple bar shaped triangle side friction supporting masses, angle orientation film, described ellipticity annular elastomeric upper surface is evenly provided with multiple circular protrusions portion, described circular protrusions deployed in described bar shaped triangle side friction supporting mass, described angle orientation film is fixed between described lug boss and described bar shaped triangle side friction supporting mass.
Embodiment 3:
The pusher hovercar of a kind of screw wing, the pusher hovercar of this screw wing comprises described left back drive wheel, above-mentioned right back drive wheel, left front wheel flutter, right front wheel flutter, vehicle body matrix, above-mentioned four groups of independence multiple stage spiral pushing devices, two wheel transmissions, two wheel steering control system, three image capturing devices, radar detection induction installation, signal receiving and transmitting unit, telecommunication control system, it is characterized in that, described left front wheel flutter, right front wheel flutter, left back drive wheel, right back drive wheel is installed on respectively the symmetrical position of the front and back end of above-mentioned vehicle body matrix, described four groups of independence multiple stage spiral pushing devices are installed on respectively described left back drive wheel, right back drive wheel, left front wheel flutter, the central interior position of right front wheel flutter, described two wheel transmissions are built in respectively described left back drive wheel and described right back drive wheel inner bottom part midway location, each described wheel transmission comprises engine installation and multiple driving gear set, wherein, described left front wheel flutter and described right front wheel flutter are rotationally connected by left front deflecting bar and right front deflecting bar and described vehicle body matrix respectively, described two wheel steering control system are built in respectively above-mentioned left front deflecting bar and right front deflecting bar, an and side of close described left front wheel flutter and described right front wheel flutter respectively, described three image capturing devices are installed on vehicle body matrix front portion, afterbody and bottom, described radar detection induction installation is arranged on respectively described vehicle body matrix bottom, afterbody and two side positions, described signal receiving and transmitting unit is built in the forebody of above-mentioned vehicle body matrix inside, and described telecommunication control system is built in the latter half of of above-mentioned vehicle body matrix inside, wherein, described signal receiving and transmitting unit inside is equipped with signal receiving unit successively, acquisition of signal is sorted out accumulation unit, signal filter element, signal transmitter unit, described telecommunication control system comprises signal acquisition module, signal processing module, signal conversion module, signal transmission module, signal main control module, signal emission module successively, described independent multiple stage spiral pushing device comprises screw shaft, multiple screw propulsion sheet, screw propeller, wherein, described screw shaft is the quill shaft that is evenly provided with multiple air bleeders, described multiple screw propulsion sheet is multiple oval screw propulsion sheets, described screw propeller surfaces externally and internally multiple uneven oval hold down grooves of cutting sth. askew out, every two axial angles of uneven oval hold down groove are less than 5 degree and are greater than 3 degree, described multiple oval screw propulsion sheet correspondence is arranged in above-mentioned oval hold down groove, each described oval screw propulsion sheet is made up of multiple segmentation materials, and at least one segmentation material is prepared from by glass-epoxy panel, each described image capturing device inside comprises left end camera element from left to right successively, left end vibrationproof unit, graphicinformation receiving element, graphicinformation monitoring acquisition elements, graphicinformation converting unit, graphicinformation transmitter unit, right-hand member vibrationproof unit, right-hand member camera element, wherein, described left end vibrationproof unit and described right-hand member vibrationproof unit all comprise ellipticity annular elastomeric, multiple bar shaped triangle side friction supporting masses, angle orientation film, described ellipticity annular elastomeric upper surface is evenly provided with multiple circular protrusions portion, described circular protrusions deployed in described bar shaped triangle side friction supporting mass, described angle orientation film is fixed between described lug boss and described bar shaped triangle side friction supporting mass, the pusher hovercar of described screw wing also can comprise two of left and right wing, former and later two vertical tails, fairing, two of described left and right wing symmetry is arranged on above-mentioned vehicle body matrix left and right sidepiece, described former and later two vertical tail symmetries are arranged on sidepiece before and after above-mentioned vehicle body matrix, and front end is provided with rolling pitch control subsystem outer arcuate rudder face and arc rudder face is controlled in driftage outside each described wing, outside each described vertical tail, front end is provided with rolling pitch control subsystem arc rudder face and driftage control outer arcuate rudder face.
Embodiment 4:
Novel Heliflying automobile can be simplified and comprises the built-in screw wing framed structure of wheel, aircraft mounted control system, tele-control system.Described framed structure comprises large scale crawler type vehicle wheel, independent spiral wing propeller, it is characterized in that, large scale crawler type vehicle wheel is placed in both sides, car front and back, and independent spiral propelling unit is placed in large scale crawler type vehicle wheel;
Large scale crawler type vehicle wheel, by rear drive wheel and front steering wheel two parts.Drive wheel by power system, wheel transmission, realize hovercar enforcement on land and drive; Steered wheel is realized the control of exercising direction by steering control system; Drive wheel and wheel flutter possess drag function;
Between screw wing propelling unit, work alone, by master control system distributed power separately, distribute by the thrust between screw wing controller, realize lifting, the direction to control of aircraft;
Common drive system between large scale crawler type vehicle wheel and spiral propeller, under enforcement pattern and offline mode, completes the automatic switchover of driving by master control system;
Aircraft mounted control system of the present invention, comprises manual control equipment, signal conversion equipment and airborne master control system.Under manual control pattern, by manual control equipment, by signal conversion equipment, manipulation instruction transformation is become to the manipulation signal of master control system identification, control hovercar;
Further, hovercar of the present invention also comprises tele-control system, and described tele-control system comprises the image capture device, image-signal processor, airborne wireless signal sending and receiving equipment, airborne master control system, controller of aircraft, terrestrial wireless signal sending and receiving equipment and the ground control system that are installed on hovercar.Tele-control system is realized the transmission of remote image transmitting-receiving, data transmit-receive and control signal by terrestrial wireless signal sending and receiving equipment, the ground control signal receiving is transferred to the master control system in hovercar by airborne wireless signal sending and receiving equipment, there is master control system to send instructions to controller of aircraft, realize the Long-distance Control to hovercar.By above-mentioned tele-control system, hovercar of the present invention can be realized the task such as long range exploration, air transport under unmanned state.
Embodiment 5:
Four crawler type vehicle wheels before and after novel Heliflying automobile can be reduced to equally, in concrete application if any specific demand, can expand to 68 even more, the present invention is taking four-wheel aircraft as example.Under the form pattern of land, after two be drive wheel, before two be wheel flutter, screw wing propeller screw oar is fixed mode, cannot rotate, ensure land exercise safety.The power that power system produces, drives Caterpillar tyre by driving gear set.Wheel flutter is realized turning function under steering controller control.
Four groups of screw wing propelling units are worked alone, and between adjacent screw propeller, hand of rotation is contrary, and control system distributes different power values to realize the various flight controls of aircraft.Be specially: when lifting, four groups of propelling units obtain identical thrust, and aircraft steadily rises or lands.When left-hand rotation, the two groups of propelling units in aircraft the right obtain than two groups, the left side larger thrust of aircraft, contrary when right-hand rotation; While advancing, after two groups of recommendation phases obtain larger thrusts than two groups of aircraft above, contrary while retreating.
For realizing safety and light and handy performance, vehicle body main body adopts high strength light quality material, and skin adopts outer fibre layer, foamed plastic core filled composite material; Described chassis adopts glass-epoxy panel, polyurethane core filled composite material.Along with material technology is updated, material is not limited to upper type.
In the present invention, exercise and airflight in aircraft land route, adopts same group of engine installation, adopts at present lithium Electronmotive Force mode, and by control system, according to manually or automatically manipulating instruction, by electronic governor, distributed power is to drive wheel or screw wing propelling unit.
In tele-control system of the present invention, image capture device is the eyes of aircraft, form by being installed on aircraft two high definition high-speed camera heads, cradle head controllors anterior and bottom, convert through signal processor the vision signal collecting to be applicable to transmitting digital signal and send to ground control terminal through airborne wireless signal sending and receiving equipment; The ground control signal receiving is transferred to the master control system in hovercar by airborne wireless signal sending and receiving equipment, realizes the Long-distance Control to hovercar; In machine, wireless transmitting-receiving equipments can be received and dispatched picture signal simultaneously, realizes the transmission of bidirectional picture signal.
Radar detecting equipment is equipped with in aircraft body bottom, afterbody and both sides, in the time that offline mode starts, whether radar afterbody and both sides radar detecting equipment have the people or the thing that affect flight in monitoring periphery certain distance automatically, in the time having people or thing within the scope of aircraft security landing, system is warned before can pointing out flight; The effect of aircraft bottom radar is in aircraft land process, provides accurate ground clearance parameter, auxiliary landing.
Hovercar model test machine of the present invention completes, and successfully carries out land form and test flight; The present invention is not only applicable to 4 and takes turns, and 6 takes turns, 8 takes turns, being suitable for too of symmetrical structure.
The present invention is not limited to above-mentioned specific embodiment, is not deviating under spirit of the present invention and real situation thereof, and those of ordinary skill in the art can make according to the present invention various corresponding changes and distortion.Within these corresponding changes and distortion all should belong to the protection domain of claims of the present invention.
Claims (3)
1. the pusher hovercar of screw wing, the pusher hovercar of this screw wing comprises left back drive wheel, right back drive wheel, left front wheel flutter, right front wheel flutter, vehicle body matrix, four groups of independence multiple stage spiral pushing devices, two wheel transmissions, two wheel steering control system, three image capturing devices, radar detection induction installation, signal receiving and transmitting unit, telecommunication control system, it is characterized in that, described left front wheel flutter, right front wheel flutter, left back drive wheel, right back drive wheel is installed on respectively the symmetrical position of the front and back end of above-mentioned vehicle body matrix, described four groups of independence multiple stage spiral pushing devices are installed on respectively described left back drive wheel, right back drive wheel, left front wheel flutter, the central interior position of right front wheel flutter, described two wheel transmissions are built in respectively described left back drive wheel and described right back drive wheel inner bottom part midway location, each described wheel transmission comprises engine installation and multiple driving gear set, wherein, described left front wheel flutter and described right front wheel flutter are rotationally connected by left front deflecting bar and right front deflecting bar and described vehicle body matrix respectively, described two wheel steering control system are built in respectively above-mentioned left front deflecting bar and right front deflecting bar, an and side of close described left front wheel flutter and described right front wheel flutter respectively, described three image capturing devices are installed on vehicle body matrix front portion, afterbody and bottom, described radar detection induction installation is arranged on respectively described vehicle body matrix bottom, afterbody and two side positions, described signal receiving and transmitting unit is built in the forebody of above-mentioned vehicle body matrix inside, and described telecommunication control system is built in the latter half of of above-mentioned vehicle body matrix inside, wherein, described signal receiving and transmitting unit inside is equipped with signal receiving unit successively, acquisition of signal is sorted out accumulation unit, signal filter element, signal transmitter unit, described telecommunication control system comprises signal acquisition module, signal processing module, signal conversion module, signal transmission module, signal main control module, signal emission module successively.
2. the pusher hovercar of screw wing according to claim 1, is characterized in that: described independent multiple stage spiral pushing device comprises screw shaft, multiple screw propulsion sheet, screw propeller, wherein, described screw shaft is the quill shaft that is evenly provided with multiple air bleeders, described multiple screw propulsion sheet is multiple oval screw propulsion sheets, described screw propeller surfaces externally and internally multiple uneven oval hold down grooves of cutting sth. askew out, every two axial angles of uneven oval hold down groove are less than 5 degree and are greater than 3 degree, described multiple oval screw propulsion sheet correspondence is arranged in above-mentioned oval hold down groove, each described oval screw propulsion sheet is made up of multiple segmentation materials, and at least one segmentation material is prepared from by glass-epoxy panel, each described image capturing device inside comprises left end camera element from left to right successively, left end vibrationproof unit, graphicinformation receiving element, graphicinformation monitoring acquisition elements, graphicinformation converting unit, graphicinformation transmitter unit, right-hand member vibrationproof unit, right-hand member camera element, wherein, described left end vibrationproof unit and described right-hand member vibrationproof unit all comprise ellipticity annular elastomeric, multiple bar shaped triangle side friction supporting masses, angle orientation film, described ellipticity annular elastomeric upper surface is evenly provided with multiple circular protrusions portion, described circular protrusions deployed in described bar shaped triangle side friction supporting mass, described angle orientation film is fixed between described lug boss and described bar shaped triangle side friction supporting mass.
3. the pusher hovercar of screw wing according to claim 1, is characterized in that: the pusher hovercar of described screw wing also can comprise two of left and right wing, former and later two vertical tails, fairing; Two of described left and right wing symmetry is arranged on above-mentioned vehicle body matrix left and right sidepiece, described former and later two vertical tail symmetries are arranged on sidepiece before and after above-mentioned vehicle body matrix, and front end is provided with rolling pitch control subsystem outer arcuate rudder face and arc rudder face is controlled in driftage outside each described wing; Outside each described vertical tail, front end is provided with rolling pitch control subsystem arc rudder face and driftage control outer arcuate rudder face.
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| CN201320470440.4U CN204020446U (en) | 2013-08-04 | 2013-08-04 | The pusher hovercar of screw wing |
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| CN201320470440.4U CN204020446U (en) | 2013-08-04 | 2013-08-04 | The pusher hovercar of screw wing |
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Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103350624A (en) * | 2013-08-04 | 2013-10-16 | 付佃华 | Propelling type flying car with spiral wings |
| RU2807493C1 (en) * | 2023-05-10 | 2023-11-15 | федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский университет науки и технологий" | Small unmanned aircraft with capability of movement over the earth's surface |
-
2013
- 2013-08-04 CN CN201320470440.4U patent/CN204020446U/en not_active Expired - Lifetime
Cited By (3)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103350624A (en) * | 2013-08-04 | 2013-10-16 | 付佃华 | Propelling type flying car with spiral wings |
| CN103350624B (en) * | 2013-08-04 | 2015-06-03 | 付佃华 | Propelling type flying car with spiral wings |
| RU2807493C1 (en) * | 2023-05-10 | 2023-11-15 | федеральное государственное бюджетное образовательное учреждение высшего образования "Уфимский университет науки и технологий" | Small unmanned aircraft with capability of movement over the earth's surface |
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