CN208393628U - Imitate formula ducted fan aircraft in ground - Google Patents

Abstract

Imitate formula ducted fan aircraft in ground, it mainly include ground effect wing chassis, water-drop-shaped cabin, four groups of self-balancing ducted fan/paddle devices, security system and electric power robot control system(RCS), the four groups of self-balancings ducted fan/paddle device is connect with ground effect wing chassis, and is symmetrically arranged in ground effect wing chassis two sides two-by-two；The water-drop-shaped cabin is fixed on ground effect wing chassis and collectively forms streamlined ground effect wing type body with ground effect wing chassis, and the streamlined ground effect wing type body is connect with self-balancing ducted fan/paddle device outer wall by smooth surface；The security system is fixed on water-drop-shaped cabin or in cabin, and the security system and four groups of ducted fan/paddle devices are electrically connected with the electric power robot control system(RCS) being fixed in water-drop-shaped cabin.It is highly-safe using the utility model, it can be achieved that VTOL, manipulation is simple and manipulation sense is strong, lift is provided using ground effect when high-speed flight, is suitable for flight experience and daily flight is gone on a journey.

Description

Imitate formula ducted fan aircraft in ground

Technical field

The utility model relates to vehicle technology fields, and in particular to imitate formula ducted fan aircraft a kind ofly.

Background technique

Currently, aircraft development make rapid progress, all kinds of aircraft take photo by plane, agricultural, plant protection, self-timer, express transportation, disaster The fields such as rescue, observation wild animal, monitoring, mapping, news report, electric inspection process, the disaster relief, movies-making, military affairs are related to extensively It is general, but the aircraft in each field mainly uses Large Scale Space Vehicle and small-sized or miniature unmanned vehicle at present, rarely has small-sized manned Aircraft does flight experience and daily life trip for ordinary people.Existing aircraft is broadly divided into fixed wing aircraft and cunning Xiang machine, heligyro and gyroplane, flapping-wing aircraft and tiltrotor, fixed wing aircraft and aerodone are generally required to longer Landing runway and expensive, be generally not suitable for that ordinary people does flight experience and daily life trip is preferred；Rotor is gone straight up to The larger and helicopter operation of the flight noise of machine and gyroplane vibration is complicated, is unfavorable for daily life trip flight and uses, and flies Row experience sense is very poor；Flapping-wing aircraft is that the general weight of bionic Aircraft is smaller, is relatively suitble to do unmanned plane use；Tiltrotor combines Fixed-wing and helicopter feature are as course of new aircraft, though having lot of advantages, its high cost and complex operations are uncomfortable Close ordinary people's routine use and flight experience.

Secondly, emerging carplane and rotorcycle are as a kind of novel flight tool, it is wide because can significantly utilize Airspace solve that crowded traffic congestion of the various trip of current surface car etc. is worried and the attention by numerous scientific workers, but at present Carplane or its technical application of rotorcycle it is still unsatisfactory, as Chinese patent CN201520891060 provides a kind of flight Electric vehicle by wheel, vehicle frame, vehicle body, propeller, engine, is bonded by the hinged wing of single hole with vehicle body, Be characterized in: wheel provides driving by the power-driven power system that driving force motor, power accumulator, speed setting controller are bonded Power, wheel are arranged by the control steering of manual steering mechanism, propeller, engine at flight electric vehicle rear portion, for flight electric vehicle There is provided airflight level power, wing be can collapse automatically, the triangle collapse wing or trapezoidal folding machine of Automatic-expanding It is connected between the wing, flight electric vehicle body hanger bracket and wing by hinge hanging ring, triangle operating lever operation control wing encloses Upper and lower before and after around hinge hanging ring, left and right rotates upwardly and downwardly the state of flight of control flight electric vehicle, this technology has the disadvantage that it One, manual control turns to and wing control bar turns to, adjustment, and manipulation is complicated, and operability is very poor；Second, due to its Operating Complexity and Easy damping safety prevention measure, is very easy to cause safety accident；Third, its flight electric vehicle does not meet aerodynamics There is very big air drag in principle, and it does not have comfort that can say, the method for being only capable of simply flying as one kind, practicability It is not high, it is very poor in particular for the practicability of people's trip and flight experience under current economic situation.Chinese patent CN201620295204.7 discloses a kind of carplane, including vehicle frame, is assemblied in the preceding duct group of vehicle frame front end along the vertical direction Part and the rear duct component for being assemblied in vehicle frame rear end along the vertical direction, vehicle frame, preceding duct component, in rear duct component three Axis is in same perpendicular, and the intracavity bottom of the intracavity bottom of preceding duct component and/or rear duct component is along level side To four groups of guiding subassemblies being distributed with for realizing the flare maneuver of carplane by the deflection water conservancy diversion that cooperates；Each group of water conservancy diversion Component is connected with individual tilt controller or same tilt controller controls four groups of guiding subassemblies respectively；This technology exists Following deficiency, first is that, using four groups of guiding subassembly adjustment duct module outlet sizes and wind direction, although air-flow is utilized Reaction force but wind outlet is done and is stopped, windage is not only increased but also increases power device load, energy consumption is big and more；Two It is that duct component spin power is unable to torsion self-balancing, needs to be symmetrical arranged to offset torque, and limitation is big, and additional increasing Add energy consumption；Third is that structure setting does not use aerodynamic principle, also only a kind of fly able scheme, be cannot achieve High-speed flight, flight experience are poor；Fourth is that being not provided with associated safety safeguard procedures, be easy to causeing in carrying people to fly can not Inverse damage and personal safety accident.

Utility model content

Technical problem to be solved in the utility model is that for overcome the deficiencies in the prior art, providing one kind can be vertical Landing, manipulation is simple, highly-safe, provides lift using airfoil body in flight and is suitable for flight experience and daily flies out Capable ducted fan aircraft.

Technical solution adopted by the utility model to solve its technical problems is formula ducted fan aircraft is imitated on ground, mainly Including ground effect wing chassis, water-drop-shaped cabin, four groups of self-balancing ducted fan/paddle devices, security system and electric power robot control system(RCS), institute It states four groups of self-balancing ducted fan/paddle devices to connect with ground effect wing chassis, and is symmetrically arranged in ground effect wing chassis two two-by-two Side；The water-drop-shaped cabin is fixed on ground effect wing chassis and collectively forms streamlined ground effect wing type body with ground effect wing chassis, described Streamlined ground effect wing type body is connect with self-balancing ducted fan/paddle device outer wall by smooth surface；The security system Be fixed on water-drop-shaped cabin or in cabin, the security system and four groups of ducted fan/paddle devices be fixed on water-drop-shaped cabin Interior electric power robot control system(RCS) electrical connection.

The ground effect wing chassis mainly includes baffle at bottom, two groups of side deflectors and front deflector and rear portion drainage The bottom surface front end of plate, the baffle at bottom is straight and tail portion arc is bent downwardly；The side edge of the baffle at bottom and two The top edge connection of group side deflector, the leading edge of baffle at bottom are connect with front flow guiding plate feather edge, baffle at bottom Back edge is connect with the feather edge of rear portion drainage plate, and ground effect wing chassis forms a front deflector and is used for preceding part wind, bottom Deflector is used for the baffle that tail portion air inducing and side deflector are used to keep out the wind both sides for wind-guiding, rear portion drainage plate, can have Effect generates downwash flow when aircraft advances and avoids the formation of vortex simultaneously, promotes aircraft lift, reduces energy loss.

The water-drop-shaped cabin mainly includes cockpit and equipment installation cabin, and the cockpit and equipment install cabin The exposed top surface in connection, the exposed top surface of cockpit and equipment installation cabin collectively forms the top surface in water-drop-shaped cabin, driver The exposed top surface in the exposed top surface of cockpit and equipment installation cabin is the cambered surface of evagination, and the exposed top surface of cockpit is most High point is higher than the highest point of the exposed top surface in equipment installation cabin, the exposed top surface of cockpit shape on the top surface in water-drop-shaped cabin At a cambered surface protrusion, while the outer convex globoidal in water-drop-shaped cabin reduces windage, the cambered surface protrusion can make to pass through water-drop-shaped Faster, pressure is smaller, further increases the lift of aircraft for the distinguished and admirable distinguished and admirable flow velocity of velocity ratio ground effect wing chassis of cabin top surface.

Self-balancing ducted fan/the paddle device mainly includes at least one set of torque self-balancing wind that can be reversely rotated Fan/blade, swing mechanism, power mechanism, swings power mechanism and external wind-guiding shell at duct tub, and every group can reversely rotate Torque self balancing fan/blade include at least two mutually opposing rotations torque self balancing fan/blade；The torque is certainly Balancing fan/blade is fixed in duct tub, and the duct tub is fixed in external ventilation case body, the swing engine Structure is fixed on ground effect wing chassis and its power output shaft is connected by swing mechanism and duct tub, and the power mechanism passes through Gear connect with torque self balancing fan/blade and provides reverse rotation power, and swing mechanism can be around swing power mechanism Power output shaft rotates, and the swing of torque self balancing fan/blade duct tub is set in swing mechanism drive, puts down certainly to realize Weighing apparatus ducted fan/paddle device swing.The power mechanism and swing power mechanism preferred motor, the swing mechanism are excellent Select the frame structure being fixed in duct tub.

The security system mainly includes driving safety prior-warning device and/or emergency rescuing protection device, the driving peace Full prior-warning device includes that weather monitoring unit, obstacle evade route planning unit, machine vision detection analysis unit, radar automatically Or at least one of infrared acquisition analytical unit.The weather monitoring unit includes that weather monitoring sensor and signal receive Processing unit, it includes obstacle monitoring sensor and signal processing unit, machine that obstacle evades route planning unit automatically Visual detection analytical unit includes visual detector and signal processing unit, and radar or infrared acquisition analytical unit include thunder Up to/infrared detector and signal processing unit, weather monitoring unit, obstacle evade route planning unit, machine view automatically Feel that detection analysis unit, radar or infrared acquisition analytical unit can share same signal processing unit, weather monitoring passes Sensor, obstacle monitoring sensor, visual detection, radar/infrared detector are directly connected to signal processing unit, gas As monitoring sensor or obstacle monitoring sensor or visual detector or radar/infrared detector are mostly installed at aircraft On outer surface, signal processing unit is fixed in the equipment installation cabin in water-drop-shaped cabin, can provide safety in real time for aircraft Warning information or the planning such as landing and route planning adjustment of taking off that aircraft is made according to information.The emergency rescuing protection dress It sets including panic averter and/or emergency buffer unit and/or emergency ramp-down device and driver protection device, the emergency Catapult-launching gear and/or emergency buffer unit and/or ramp-down device of meeting an urgent need are mounted in the equipment installation cabin in water-drop-shaped cabin, can endangered The measures such as slow drop buffering, protection aircraft security landing manually or automatically in emergency circumstances are made to aircraft in danger.The driving Member's protective device is mounted in cockpit, can in case of emergency automatic trigger, preventing mechanism, guarantor are made to personnel The safety of member.The preferred wind speed wind direction sensor of the weather monitoring sensor and Temperature Humidity Sensor etc.；The obstacle monitoring With the preferred laser sensor of sensor and ultrasonic sensor etc..

The electric power robot control system(RCS) mainly includes the energy storage device and electric control gear being fixed in equipment installation cabin, energy storage Device is electrically connected with electric control gear, and the electric control gear includes signal acquisition module, operation module, display module and processing mould Block, signal acquisition module and operation module are electrically connected with processing module, and processing module is electrically connected with display module, and self-balancing is contained The panic averter of road fan/paddle device swing power mechanism and power mechanism and emergency rescuing protection device is answered Anxious buffer unit, emergency ramp-down device are electrically connected with processing module, the signal acquisition module and driving safety prior-warning device The signal of acquisition is transmitted to processing module by signal processing unit connection, signal acquisition module, is handled simultaneously through processing module Cycle detection remove existence of redundant after, output shown or exported to display module to emergency rescuing protection device and/or from Balance ducted fan/paddle device execution is automatically brought into operation, or is issued instruction by operation module and exported after processing module is handled Manual operation is executed to emergency rescuing protection device and/or self-balancing ducted fan/paddle device.The energy storage device can be used The battery group of high-energy density with charge function mainly supplies each power equipment power.

Further, the electric power robot control system(RCS) can also be equipped with man machine language's interactive device, and man machine language's interactive device can be with Signal pickup assembly connection, the sound of the recognizable aircraft pilot of man machine language's interactive device simultaneously pass through acoustic control operation, The flight experience of high degree of comfort can be achieved.

Further, the electric power robot control system(RCS) can also be equipped with spare energy storage device, spare energy storage device and electric control gear electricity Connection is detecting that energy storage device breaks down or when power drain, not between cutting shift to spare energy storage device power supply, to guarantee Aircraft has sufficient power smooth flight or landing.

Further, the electric power robot control system(RCS) can also be equipped with energy management apparatus and wireless charging device, spare energy storage dress Set and be electrically connected with wireless charging device with energy storage device, spare energy storage device and energy storage device pass through energy management apparatus with Electric control gear electrical connection, can be in any one group of power supply, and another group ensures power supply, two groups of energy storage devices using wireless charging Can not between electric mutual backup.

Further, the aircraft can also be equipped with flight attitude sensor, and flight attitude sensor mainly includes three axis tops Spiral shell instrument, three axis accelerometer, three axle electronic compass etc., flight attitude sensor are connect with signal acquisition module, and processing module is also It connect, flight attitude sensor can be collected with balance ducted fan/paddle device power mechanism and swing power mechanism Signal be transmitted to processing module and carry out closed-loop control and adjust ducted fan/blade operating status, realize smooth flight, reduce empty Middle flow perturbation.

Further, the aircraft can also be equipped with take-off and landing device, and take-off and landing device is fixed on the bottom of external wind-guiding shell.It rises Dropping control device can be made of high-elastic elastic material.

Further, the water-drop-shaped cabin can be also olive shape or shuttle shape or semielliptical shape, in favor of reducing windage, and one Top pressure can be reduced under constant speed degree, improve lift.

Further, the emergency rescuing protection device of the security system of the aircraft is preferably met an urgent need ramp-down device.Emergency is slow Falling unit may include floatage body, and floatage body is in umbrella or balloon-like after inflation, and floatage body passes through pipeline and built-in high pressure The bottle body of helium connects, and control valve, the processing module connection of control valve and electric control gear are equipped on pipeline.Sensor monitors When significant trouble occurs in aircraft, the signal of the signal acquisition module acquisition sensor of controller for electric consumption is transferred to processing module, Processing module triggers control valve and opens, and high-pressure helium is filled with the floatage body of umbrella or balloon-like, and the instantaneous inflation of floatage body is Aircraft provides high buoyancy, interior in short-term that aircraft is made to be in flat floating state.

The utility model uses four groups of swingable self-balancing ducted fan/paddle devices to provide flight for aircraft and moves Power is small with windage with the ground effect wing chassis that drainage plate is constituted with each group deflector and meet aerodynamic water-drop-shaped cabin and connect Collectively form aircraft ground effect wing type body.After aircraft starting, specified altitude assignment is promoted to by setting path and swings self-balancing duct Fan/paddle device angle provides forward flight power while providing lift by self-balancing ducted fan/paddle device, The aircraft ground effect wing type body that ground effect wing chassis and water-drop-shaped cabin are constituted during flying before acceleration provides lift for complete machine, leads to Electric power robot control system(RCS) difference adjust automatically control self-balancing ducted fan/paddle device revolving speed or swing angle are crossed, realizes and flies The acceleration or steering of row device；While with flight attitude sensor real-time monitoring state of flight and self-balancing is controlled by processing module Ducted fan/paddle device revolving speed or swing angle reduce flow perturbation, increase flight stability.In addition, this aircraft is also Equipped with a variety of safety precautions: in terms of energy resource supply, be equipped with energy storage device and spare energy storage device, can not between electricity power supply protect Card safety；It is additionally provided with security system simultaneously, not only gives warning in advance using driving safety prior-warning device and makes planning and adjusting and keep away Exempt from danger occur, can be also automatic enabling emergency rescuing protection device, people on guarantee machine running out of steam or being in an emergency Member's safety.

Beneficial effect

1, this aircraft constitutes streamlined ground effect wing type body using ground effect wing chassis and water-drop-shaped cabin, while certainly flat with torque Ducted fan/blade of weighing apparatus be power, can VTOL and in flight using airfoil body provide lift, can not only reduce fixation The runway that rotor aircraft takes off, and be awing the lift that aircraft provides using fixed-wing, facilitate energy conservation.

2, the electric power robot control system(RCS) that this aircraft uses using energy storage device and spare energy storage device not between electricity automatically switch, Mutual backup guarantees energy resource supply and improves the voyage of aircraft.

3, the security system of this aircraft not only gives warning in advance using driving safety prior-warning device and makes planning and adjusting Danger is avoided the occurrence of, emergency rescuing protection device can be also enabled automatically when running out of steam or being in an emergency, it can be significantly The flight safety of aircraft is improved, while ensureing the safety of personnel on aircraft.

4, self-balancing ducted fan/blade that this aircraft uses can greatly inhibit noise, while use automation control Or human-computer interaction device closed-loop control, it realizes that smooth flight adjusts flight attitude in real time, gives comfortable flight experience and behaviour Vertical sense.

5, structure is simple, and applicability is good, and cost is lower, can VTOL, manipulation is simple and manipulation sense is strong, highly-safe, Lift is provided using ground effect when high-speed flight, ordinary person is applicable not only to and does manned experience, is further adapted to common Personnel make daily life trip tool, are conducive to substantially promotion and application.

Detailed description of the invention

Fig. 1 is the structural schematic diagram that formula ducted fan aircraft is imitated shown in the utility model embodiment 1；

Fig. 2 is the side view for imitating formula ducted fan aircraft as shown in Figure 1；

Fig. 3 is the structural schematic diagram of the ground effect wing chassis of the utility model；

Fig. 4 is self-balancing ducted fan/paddle device structural schematic diagram；

Fig. 5 is the power supply figure of the utility model electric power robot control system(RCS).

In figure, 1- ground effect wing chassis, 101- baffle at bottom, the side 102- deflector, the front 103- deflector, after 104- Portion's drainage plate, 2- water-drop-shaped cabin, 201- cockpit, 202- equipment installation cabin, 3- self-balancing ducted fan/paddle device, 301- torque self balancing fan/blade, 302- duct tub, 303- swing mechanism, 304- power mechanism, the outside 305- ventilation case Body, 306- swing power mechanism, 4- security system, 41- driving safety prior-warning device, 42 emergency rescuing protection devices, 5- electric power Robot control system(RCS), 51- energy storage device, 52- electric control gear, 521- signal acquisition module, 522- operation module, 523- display module, 524- processing module, the spare energy storage device of 53-, 54- energy management apparatus, 55- wireless charging device, 6- take-off and landing device.

Specific embodiment

The following is a further explanation of the present invention with reference to the accompanying drawings and embodiments.

Referring to Figures 1 and 2, formula ducted fan aircraft is imitated on ground, mainly includes ground effect wing chassis 1,2, four groups of water-drop-shaped cabin Self-balancing ducted fan/paddle device 3, security system 4 and electric power robot control system(RCS) 5, four groups of ducted fan/blades 3 with Ground effect wing chassis 1 connects, and is symmetrically arranged in 1 two sides of ground effect wing chassis two-by-two；The water-drop-shaped cabin 2 is fixed on ground effect wing chassis Streamlined ground effect wing type body, the ground effect wing type body and self-balancing ducted fan/paddle are collectively formed on 1 and with ground effect wing chassis 1 The outer wall of leaf device 3 is connected by smooth surface；The security system 4 is fixed on the cabin in water-drop-shaped cabin 3 or in cabin, the peace Total system 4 and four groups of ducted fan/paddle devices 3 are electrically connected with the electric power robot control system(RCS) 5 being fixed in water-drop-shaped cabin 2.

The ground effect wing chassis mainly includes 101, two groups of side deflectors 102 of baffle at bottom and front deflector 103 And rear portion drainage plate 104, the bottom surface of the baffle at bottom 101, front end is straight and tail portion arc is bent downwardly；It leads the bottom 101 side edge of flowing plate is connect with two groups of 102 top edges of side deflector, the leading edge and front flow guiding plate 103 of baffle at bottom 101 Feather edge connection, baffle at bottom 101 back edge connect with the feather edge of rear portion drainage plate 104, ground effect wing chassis 1 formed One front deflector 103 is used for tail portion air inducing for wind-guiding, rear portion drainage plate 104 for preceding part wind, baffle at bottom 101 And side deflector 102 is used for the baffle that both sides are kept out the wind, and downwash flow can be effectively generated when aircraft advances and is kept away simultaneously Exempt to form vortex, promote aircraft lift, reduces energy loss.

The water-drop-shaped cabin 2 is cockpit 201 and equipment installs cabin 202, and the cockpit 201 is pacified with equipment The exposed top surface in 202 connection of stowage, the exposed top surface of cockpit 201 and equipment installation cabin 202 collectively forms water-drop-shaped cabin 2 Top surface, the exposed top surface of cockpit 201 and equipment installation cabin 202 exposed top surface be evagination cambered surface, and drive The highest point of the exposed top surface of member's cockpit 201 is higher than the highest point of the exposed top surface in equipment installation cabin 202, cockpit 201 Exposed top surface a cambered surface protrusion is formed on the top surface in water-drop-shaped cabin 2, water-drop-shaped cabin 2 outer convex globoidal reduce windage While, the top of the cambered surface protrusion can make the distinguished and admirable flow velocity of distinguished and admirable velocity ratio ground effect wing chassis 1 by 2 top surface of water-drop-shaped cabin Faster, pressure is smaller, further increases the lift of aircraft.

Self-balancing ducted fan/the paddle device 3 includes at least one set of torque self balancing fan/paddle that can be reversely rotated Leaf 301, swing mechanism 303, power mechanism 304, swings power mechanism 306 and external wind-guiding shell 305 at duct tub 302, often Torque self balancing fan of the torque self balancing fan/blade 301 that group can reversely rotate including at least two mutually opposing rotations/ Blade；Torque self balancing fan/the blade is fixed in duct tub 302, and the duct tub 302 is fixed on external wind-guiding In shell 305, the swing power mechanism 306 is fixed on ground effect wing chassis 1 and its power output shaft passes through swing mechanism 303 It is connected with duct tub 302, the power mechanism 304 is connected by gear and the torque self balancing fan of reverse rotation/blade 301 Reverse rotation power is connect and provides, swing mechanism 303 can be around the power output shaft rotation for swinging power mechanism 306, oscillating machine Structure sets the swing of torque self balancing fan/blade duct tub in driving, to realize self-balancing ducted fan/paddle device 3 Swing.The power mechanism 304 and swing power mechanism 306 are motor, and the swing mechanism 303 is to be fixed on duct cylinder Frame structure on frame 302.

The security system 4 mainly includes driving safety prior-warning device 41 and emergency rescuing protection device 42, the driving Safety early warning device 41 is existing maturing appts, and the driving safety prior-warning device 41 includes that weather monitoring unit (does not show in figure Out), obstacle evades route planning unit (not shown), machine vision detection analysis unit (not shown), thunder automatically It reaches or infrared acquisition analytical unit (not shown)；The weather monitoring unit include weather monitoring sensor (in figure not Show) and signal processing unit (not shown), it includes laser sensor (figure that obstacle evades route planning unit automatically In be not shown) and signal processing unit, machine vision detection analysis unit include visual detector (not shown) and Signal processing unit, radar or infrared acquisition analytical unit include radar/infrared detector (not shown) and signal Processing unit is received, weather monitoring unit, obstacle evade route planning unit, machine vision detection analysis unit, radar automatically Or infrared acquisition analytical unit can share same signal processing unit, weather monitoring sensor, obstacle monitoring sensing Device, visual detection, radar/infrared detector are directly connected to signal processing unit, weather monitoring sensor or barrier Monitoring sensor or visual detector or radar/infrared detector is hindered to be mostly installed in aircraft outer surface, signal receives Processing unit be fixed on water-drop-shaped cabin 2 equipment installation cabin 202 in, can in real time for aircraft provide safe early warning information or according to Information makes the planning such as landing and route planning adjustment of taking off of aircraft.The emergency rescuing protection device 402 includes emergency Ramp-down device (not shown) and driver protection device (not shown), can be in case of emergency manually or automatically to winged Row device and driver make anti-protection mechanism, guarantee the safety for especially guaranteeing driver while aircraft security.The emergency Ramp-down device is mounted in the equipment installation cabin 202 in water-drop-shaped cabin 2, including floatage body (not shown), floatage body are being inflated It is in balloon-like after expansion, floatage body is connect with the bottle body (not shown) of built-in high-pressure helium by pipeline, installed on pipeline There is control valve (not shown), the connection of processing module 524 of control valve and electric control gear can be in critical manually Or automatic trigger high-pressure helium pours in balloon-like floatage body and instantaneously provides high buoyancy for aircraft, and aircraft is made to be in flat in short-term Floating state, protection aircraft security landing.The driver protection device is safety belt and air bag in cockpit, and driver is anti- Protection unit is mounted in cockpit 201, can in case of emergency automatic trigger, preventing mechanism is made to driver, is guaranteed The safety of driver.The emergency rescuing protection device may also include panic averter (not shown) and/or emergency is slow Flushing device (not shown), the panic averter and/or emergency buffer unit are mounted on the equipment installation in water-drop-shaped cabin 2 In cabin 202, the measures such as slow drop buffering manually or automatically can be made to aircraft in critical, protect aircraft security Landing.Panic averter and emergency buffer unit are existing maturing appts.The weather monitoring sensor includes wind speed Wind transducer (not shown) and Temperature Humidity Sensor (not shown) etc.；The obstacle monitoring sensor includes swashing Optical sensor (not shown) and ultrasonic sensor (not shown) etc..

The electric power robot control system(RCS) 5 mainly includes the energy storage device 51 and automatically controlled dress being fixed in equipment installation cabin 202 52 are set, energy storage device 51 is electrically connected with electric control gear 52, and the electric control gear 52 includes signal acquisition module 521, operation module 522, display module 523 and processing module 524, signal acquisition module 521 and operation module 522 are electrically connected with processing module 524 It connects, processing module 524 is electrically connected with display module 523, self-balancing ducted fan/paddle device 3 306 He of swing power mechanism The panic averter of power mechanism 304 and emergency rescuing protection device 42, emergency buffer unit and emergency ramp-down device are equal It is electrically connected with processing module 524, the signal processing unit of the signal acquisition module 521 and driving safety prior-warning device 41 Collected signal is transmitted to processing module 522, handles through processing module 522 and recycle inspection by connection, signal acquisition module 521 After surveying removal existence of redundant, output, which is shown or exported to first aid to display module 523, helps protective device 42 and/or self-balancing The execution of ducted fan/paddle device 3 is automatically brought into operation, or defeated after the processing of processing module 524 by the sending of operation module 522 instruction Protective device 42 is helped to first aid out and/or self-balancing ducted fan/paddle device 3 executes manual operation.Signal acquisition module 521, operation module 522, display module 523 and processing module 524 are existing mature modules.The energy storage device 51 can be used The battery group of high-energy density with charge function, mainly supplies each electric power of equipment.

The installation of this aircraft devices is additionally provided with spare energy storage device 53, energy management apparatus 54 and wireless charging in cabin 202 Device 55, spare energy storage device 53 and energy storage device 51 are electrically connected with wireless charging device 55, spare energy storage device 53 and storage Energy device 51 is electrically connected by energy management apparatus 54 with electric control gear 52, by energy management apparatus 54 to energy storage device 51 Be monitored with spare energy storage device 53, and exhaust in energy storage device electric energy 51 or when failure not between cutting change, keep power supply to hold Continuous property, can be also that the energy storage device 51 for exhausting electric energy or spare energy storage device 53 charge by wireless charging device 55.This Aircraft is additionally provided with the take-off and landing device 6 of highly elastic material composition, and take-off and landing device 6 is fixed on the culvert of self-balancing ducted fan/blade 3 302 bottom of road tub.

Claims (10)

1. formula ducted fan aircraft is imitated on ground, which is characterized in that mainly include ground effect wing chassis, water-drop-shaped cabin, four groups of self-balancings Ducted fan/paddle device, security system and electric power robot control system(RCS), the four groups of self-balancings ducted fan/paddle device with The connection of ground effect wing chassis, and it is symmetrically arranged in ground effect wing chassis two sides two-by-two；The water-drop-shaped cabin is fixed on ground effect wing chassis And streamlined ground effect wing type body is collectively formed with ground effect wing chassis, the streamlined ground effect wing type body and self-balancing ducted fan/ The outer wall of paddle device is connected by smooth surface；The security system is fixed on water-drop-shaped cabin or in cabin, the safety system System and four groups of ducted fan/paddle devices are electrically connected with the electric power robot control system(RCS) being fixed in water-drop-shaped cabin.

2. imitating formula ducted fan aircraft according to claim 1ly, which is characterized in that the ground effect wing chassis mainly wraps Include baffle at bottom, two groups of side deflectors and front deflector and rear portion drainage plate, the bottom surface front end of the baffle at bottom Straight and tail portion arc is bent downwardly；The side edge of the baffle at bottom is connect with the top edge of two groups of side deflectors, bottom The leading edge of portion's deflector is connect with front flow guiding plate feather edge, and the back edge of baffle at bottom and the feather edge of rear portion drainage plate connect It connects, ground effect wing chassis forms a front deflector and is used for for preceding part wind, baffle at bottom for wind-guiding, rear portion drainage plate Tail portion air inducing and side deflector are used for the baffle that both sides are kept out the wind.

3. imitating formula ducted fan aircraft according to claim 1 or 2ly, which is characterized in that the water-drop-shaped cabin is main Cabin is installed including cockpit and equipment, the cockpit is connect with equipment installation cabin, the exposed top of cockpit The exposed top surface in face and equipment installation cabin collectively forms the top surface in water-drop-shaped cabin, the exposed top surface of cockpit and equipment installation The exposed top surface in cabin is the cambered surface of evagination, and the highest point of the exposed top surface of cockpit is higher than the exposed of equipment installation cabin The highest point of top surface, the exposed top surface of cockpit form a cambered surface protrusion on the top surface in water-drop-shaped cabin.

4. imitating formula ducted fan aircraft according to claim 1 or 2ly, which is characterized in that the self-balancing duct wind Fan/paddle device mainly include at least one set of torque self balancing fan/blade that can be reversely rotated, duct tub, swing mechanism, Power mechanism swings power mechanism and external wind-guiding shell, and every group of torque self balancing fan/blade that can be reversely rotated includes extremely Torque self balancing fan/blade of few two mutually opposing rotations, the torque self balancing fan/blade are fixed on duct tub Interior, the duct tub is fixed in external ventilation case body, and the swing power mechanism is fixed on ground effect wing chassis and it is dynamic Power output shaft is connected by swing mechanism and duct tub, and the power mechanism passes through gear and torque self balancing fan/blade Connection.

5. imitating formula ducted fan aircraft according to claim 1 or 2ly, which is characterized in that the security system is main Including driving safety prior-warning device and/or emergency rescuing protection device, the driving safety prior-warning device includes weather monitoring list Member, obstacle are evaded in route planning unit, machine vision detection analysis unit, radar or infrared acquisition analytical unit extremely automatically Few one kind；The weather monitoring unit includes weather monitoring sensor and signal processing unit, and obstacle evades road automatically Line planning unit includes obstacle monitoring sensor and signal processing unit, and machine vision detection analysis unit includes vision Detector and signal processing unit, radar or infrared acquisition analytical unit include that radar/infrared detector and signal receive Processing unit, weather monitoring unit, obstacle evade route planning unit, machine vision detection analysis unit, radar or red automatically The outer same signal processing unit of detection analysis units shared, weather monitoring sensor, obstacle monitoring sensor, vision Detection, radar/infrared detector are directly connected to signal processing unit, and weather monitoring sensor or obstacle monitoring are used Sensor or visual detector or radar/infrared detector are mostly installed in aircraft outer surface, signal processing unit It is fixed in the equipment installation cabin in water-drop-shaped cabin；The emergency rescuing protection device includes that panic averter and/or emergency are slow Flushing device and/or emergency ramp-down device and driver protection device, the panic averter and/or emergency buffer unit and/ Or emergency ramp-down device is mounted in the equipment installation cabin in water-drop-shaped cabin, the driver protection device is mounted on cockpit It is interior.

6. imitating formula ducted fan aircraft according to claim 5ly, which is characterized in that the electric power robot control system(RCS) is main Including the energy storage device and electric control gear being fixed in equipment installation cabin, energy storage device is electrically connected with electric control gear, the electricity Controlling device includes signal acquisition module, operation module, display module and processing module, signal acquisition module and operation module with Processing module electrical connection, processing module are electrically connected with display module, self-balancing ducted fan/paddle device swing power mechanism With the panic averter of power mechanism and emergency rescuing protection device, emergency buffer unit and emergency ramp-down device with place Module electrical connection is managed, the signal reception of signal acquisition module and driving safety prior-warning device in the electric power robot control system(RCS) is handled Unit connection.

7. imitating formula ducted fan aircraft according to claim 1 or 2ly, which is characterized in that the electric power robot control system(RCS) It is additionally provided with spare energy storage device, spare energy storage device is electrically connected with electric control gear；The electric power robot control system(RCS) is additionally provided with can source capsule Reason device and wireless charging device, spare energy storage device and energy storage device are electrically connected with wireless charging device, spare energy storage dress It sets and passes through energy management apparatus with energy storage device and be electrically connected with electric control gear.

8. imitating formula ducted fan aircraft according to claim 6ly, which is characterized in that imitate formula ducted fan describedly and fly Row device is additionally provided with flight attitude sensor, and flight attitude sensor mainly includes three-axis gyroscope, three axis accelerometer and three axis Electronic compass, flight attitude sensor are connect with signal acquisition module.

9. formula ducted fan aircraft is imitated on ground described according to claim 1 or 2 or 6, which is characterized in that the aircraft is equipped with Take-off and landing device, take-off and landing device are fixed on the bottom of external wind-guiding shell.

10. formula ducted fan aircraft is imitated on ground described according to claim 1 or 2 or 6, which is characterized in that the water-drop-shaped cabin For olive shape or shuttle shape or semielliptical shape.