CN102849209A - Composite power simple aircraft - Google Patents
Composite power simple aircraft Download PDFInfo
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- CN102849209A CN102849209A CN2012103287305A CN201210328730A CN102849209A CN 102849209 A CN102849209 A CN 102849209A CN 2012103287305 A CN2012103287305 A CN 2012103287305A CN 201210328730 A CN201210328730 A CN 201210328730A CN 102849209 A CN102849209 A CN 102849209A
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- aircraft
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- flight capsule
- boosting
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Abstract
The present invention provides a composite power simple aircraft, belongs to the field of aircrafts, and relates to a small aircraft conveniently used for emergency treatment, fire extinguishing and safe cruise. The aircraft comprises a flying cabin, an engine, a generator, a gas pump, a main screw propeller, an anti-rotation boost screw propeller and a turning boost nozzle, wherein a console, a rudder, a turning transmission chain, a storage battery, a high pressure gas hose, a transmission gear, a motor, an entrance, an exit and a fuel tank are arranged inside the flying cabin, the main screw propeller, the engine, the generator and the gas pump are arranged above the flying cabin, the anti-rotation boost screw propeller and the turning boost nozzle are arranged below the flying cabin, and the console is arranged on the cylinder wall of the flying cabin, and is provided with an oil operation valve, a gas operation valve, an electricity operation valve and the rudder. The aircraft of the present invention has characteristics of lightweight and convenience. With the present invention, the shortcoming of difficult takeoff and landing in urban areas due to the huge helicopter volume can be overcome.
Description
Technical field
The invention belongs to the aircraft field, relate to a kind of small aircraft of being convenient to first aid, fire extinguishing and the usefulness of cruising safely.
Background technology
Along with the accelerated development of urbanization process, it is more and more serious that city traffic stops up, give emergency vehicle, extinguishing vehicle normally travel and the police safety emergency management such as cruise is processed and has been brought the deuce to pay.Although helicopter can be avoided the traffic pressure on ground, because its volume is large, the band empennage, rotating back and forth between city high rise building has inconvenience more.
Summary of the invention
The present invention seeks to for a kind of vehicle of small-sized, easy low-latitude flying are provided, to solve modern city because the problem that traffic congestion is made troubles to the processing of emergency management.
The simple and easy aircraft of a kind of composite power is by flight capsule, driving engine, electrical generator, air pump, main screw, anti-rotation boosting screw propeller with turn to the boosting nozzle to form.Be provided with operator's station, yaw rudder in the flight capsule, turn to driving chain, storage battery, high pressure gas flexible pipe, transmission gear, electrical motor, gangway, fuel tank.Main screw, driving engine, electrical generator, air pump are above flight capsule, and operator's station is equipped with oil, gas, electric operating valve and yaw rudder on the operator's station on the barrel of flight capsule.Turn to driving chain closure rudder and turn to the boosting nozzle.Be provided with the gangway being provided with operator's station flight capsule barrel one side reversing sense.Transmission gear is welded on respectively on the gas ejector pipe of yaw rudder turning cylinder and lower end, and the two ends of gas ejector pipe are to turn to the boosting nozzle.Fuel tank links to each other with driving engine by delivery line, is arranged on the opposite side of underfloor, operator's station; Air pump links to each other with the gas ejector pipe of flight capsule lower end by the high pressure gas flexible pipe.Driving engine links to each other with electrical motor by wire, and electrical motor is located at anti-rotation boosting screw propeller top.
Principle of work:
1, drives main screw with the small portable gasoline and diesel engine and produce rising power, be aided with the lower end that the anti-rotation boosting screw propeller of small-sized electric places aircraft, rotate in the opposite direction with main screw, control aircraft rotation and the boosting that makes progress are finished the lift-off function by major-minor screw propeller cooperation.
2, with pressurized air as power, with 360 the degree turn to upper and lower, the front, rear, left and right of boosting Jet control aircraft to move.
Lay the light metal tracheae along aircraft base diameter direction, two ends are respectively installed nozzle and are stretched out the aircraft both sides, by rotate metal tube drive nozzle realize upwards, downwards, forward, jet backward, realize aircraft horizontally rotating to the left or to the right by the jet amount in the left and right two ends of Air Valve Control, the speed of the size control moving velocity by jet amount.
3, the electricity consumption of pressurized air and anti-rotation boosting screw propeller derives from minitype high voltage air pump and the small generator that gasoline and diesel engine drives.
Advantage of the present invention
Height rescue: fire of high-rise building is a metropolitan difficult problem always, and this aircraft is lightly convenient, can help the rescue group to arrive rapidly higher floor, solve helicopter can not near and the inaccessible high-rise rescue difficult problem of scaling ladder.
Leap is blocked up: in the highway section of burst traffic accident, often cause easily the local traffic paralysis, the traffic police is difficult to go to the scene, and utilize this aircraft traffic police and medical worker can within the fastest time, arrive at the scene, carry out traffic dispersion and Emergency Assistance, thereby improved efficient, striven for the time.
Security: in current bustling city, the density of population and building is all quite large, small capacity double vrille device, it is huger to overcome the helicopter volume, the shortcoming that is unfavorable for lifting in the urban district can be shuttled back and forth in certain height and zone, is convenient to warning, patrol and commander etc.
Description of drawings
Fig. 1 is agent structure scheme drawing of the present invention.
Each component names is among the figure: 1 driving engine, 2 operator's stations, 3 yaw rudders, 4 turn to driving chain, 5 storage batterys, 6 high pressure gas flexible pipes, 7 transmission gears, 8 anti-rotation boosting screw propellers, 9 electrical motors, 10 main screws, 11 flight capsules, 12 gangways, 13 fuel tanks, 14 to turn to boosting nozzle, 15 air pumps, 16 electrical generators.
The specific embodiment
The simple and easy aircraft of a kind of composite power is by flight capsule 11, driving engine 1, electrical generator 16, air pump 15, main screw 10, anti-rotation boosting screw propeller 8 with turn to boosting nozzle 14 to form.Be provided with operator's station 2, yaw rudder 3 in the flight capsule, turn to driving chain 4, storage battery 5, high pressure gas flexible pipe 6, transmission gear 7, electrical motor 9, gangway 12, fuel tank 13.Main screw 10, driving engine 1, electrical generator 16, air pump 15 are above flight capsule 11, and operator's station 2 is equipped with oil, gas, electric operating valve and yaw rudder 3 on the operator's station 2 on the barrel of flight capsule 11.Turn to driving chain 4 closure rudders 3 and turn to boosting nozzle 14.Be provided with gangway 12 being provided with operator's station flight capsule barrel one side reversing sense.Transmission gear 7 is welded on respectively on the gas ejector pipe of yaw rudder turning cylinder and lower end, and the two ends of gas ejector pipe are to turn to the boosting nozzle.Fuel tank links to each other with driving engine by delivery line, is arranged on the opposite side of underfloor, operator's station; Air pump 15 links to each other with the gas ejector pipe of flight capsule lower end by the high pressure gas flexible pipe; Electrical generator 16 links to each other with electrical motor 9 by wire, and electrical motor 9 is located at anti-rotation boosting screw propeller 8 tops.
Assembly function:
1, driving engine: adopting gasoline or diesel oil is fuel, for main screw provides power, drives simultaneously minitype high voltage air pump and small generator, is respectively to turn to assist system that pressurized air is provided and provide electric power for anti-rotation boosting screw propeller.
2, operator's station: finish respectively the control that main screw, 360 degree is turned to nozzle, anti-rotation boosting screw propeller by oil, gas, three operating valves of electricity.Wherein:
Fuel tap: i.e. throttle is used for controlling the rotating speed of main screw, control lift size;
Air valve: the mixed water valve that similar bathroom is used, the size that can adjust to tolerance realizes thrust control, the tolerance of two nozzles realizes turning about adjusting respectively again;
Electricity valve: regulate and control auxiliary screw propeller motor speed according to the rotating speed of main screw, prevent the aircraft rotation.
3, yaw rudder: the yaw rudder disc surfaces every 90 scale designations " on ", D score, four gears of 'fornt', 'back', during the rotation direction rudder, drive the lower end gas ejector pipe and nozzle rotates by driving chain, realizes jetly to different directions, the maximum rotation angle is 360 to spend.
4, turn to driving chain: be used between the gear on yaw rudder back gear and the gas ejector pipe, transmitting manually-operated twisting resistance, finish yaw rudder to the control of air blast nozzle rotation direction.
5, storage battery: adopt lithium cell, be used for the power supply of emergency light, Warning light, illuminating lamp and communication tool, can be charged by electrical generator, also the available lithium cell that had filled electricity is changed.
6, high pressure gas flexible pipe: driven by yaw rudder and when rotating, this flexible pipe can play cushioning and protection to supply air line along with rotation at the lower end gas ejector pipe, prevent that pressure gas from revealing or air feed is interrupted.
7, transmission gear: be welded on respectively on the gas ejector pipe of yaw rudder turning cylinder and lower end, transmit manual operation power by chain.
8, anti-rotation boosting screw propeller: hand of rotation and main screw opposite direction, prevent the aircraft rotation, provide simultaneously thrust upwards, auxiliary lift-off action.
9, electrical motor: by generator powered, drive auxiliary screw propeller and rotate adjustable rotating speed.
10, main screw: under the driving of driving engine, provide major impetus for aircraft rises.
11, flight capsule: be this aircraft main manned, loading container, the flight capsule shell is made cylindric by case hardened glass or transparent organism glass, and the middle part lays light-duty floor and anti-rotation boosting screw propeller separates, and guarantees personal security.The buffering landing legs for trailers is arranged at the bottom.The flight capsule shell is outer can also to increase one deck anticollision air cushion, can alleviate when meeting accident collision and the impulsive force of exterior object.
12, gangway: for making things convenient for personnel to pass in and out and material handling, offered the gangway at bulkhead, closed during flight and lock assurance personnel and cargo security.
13, fuel tank: be driving engine supply fuel oil.For counterweight and safety, be arranged on the opposite side of underfloor, operator's station.
14, turn to the boosting nozzle: by controlling of yaw rudder, this nozzle can carry out upper and lower, forward and backward four direction 360 degree rotary jets, realizes turning to and boost function; Simultaneously, by regulating the different air demands of two side nozzles, realize left and right sides turning function.
15, air pump: by being arranged in gas piping on the bulkhead for turning to assist system that pressurized air is provided.
16, electrical generator: provide electric power for the electrical motor that drives auxiliary screw propeller, storage battery, lamp, communication tool etc. by the wire that is arranged on the bulkhead.
Claims (5)
1. the simple and easy aircraft of composite power is characterized in that aircraft by flight capsule (11), driving engine (1), air pump (15), electrical generator (16), main screw (10), anti-rotation boosting screw propeller (8) and turns to boosting nozzle (14) to form; Be provided with operator's station (2), yaw rudder (3) in the flight capsule, turn to driving chain (4), storage battery (5), high pressure gas flexible pipe (6), transmission gear (7), electrical motor (9), gangway (12), fuel tank (13); Main screw (10), driving engine (1), electrical generator (16), air pump (15) are in the top of flight capsule (11), and operator's station (2) is equipped with oil, gas, electric operating valve and yaw rudder (3) on the operator's station (2) on the barrel of flight capsule (11); Turn to driving chain (4) closure rudder (3) and turn to boosting nozzle (14); Be provided with gangway (12) being provided with operator's station flight capsule barrel one side reversing sense; Transmission gear (7) is welded on respectively on the gas ejector pipe of yaw rudder turning cylinder and lower end, and the two ends of gas ejector pipe are to turn to the boosting nozzle; Fuel tank links to each other with driving engine by delivery line; Air pump (15) links to each other with the gas ejector pipe of flight capsule lower end by high pressure gas flexible pipe (6); Driving engine links to each other with electrical motor by wire, and electrical motor is located at anti-rotation boosting screw propeller top.
2. the simple and easy aircraft of described a kind of composite power according to claim 1 is characterized in that fuel tank is arranged on the opposite side of underfloor, operator's station.
3. the simple and easy aircraft of described a kind of composite power according to claim 1 is characterized in that turning to the boosting nozzle: by controlling of yaw rudder, can carry out upper and lower, forward and backward four direction 360 degree rotary jets, realize turning to and boost function.
4. the simple and easy aircraft of described a kind of composite power according to claim 1, it is characterized in that the flight capsule shell makes cylindric by case hardened glass or transparent organism glass, the middle part lays light-duty floor and anti-rotation boosting screw propeller separates, and the buffering landing legs for trailers is arranged at the flight capsule bottom.
5. the simple and easy aircraft of described a kind of composite power according to claim 1 is characterized in that the flight capsule shell is provided with one deck anticollision air cushion outward.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103287305A CN102849209A (en) | 2012-09-06 | 2012-09-06 | Composite power simple aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN2012103287305A CN102849209A (en) | 2012-09-06 | 2012-09-06 | Composite power simple aircraft |
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| CN102849209A true CN102849209A (en) | 2013-01-02 |
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| Application Number | Title | Priority Date | Filing Date |
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| CN2012103287305A Pending CN102849209A (en) | 2012-09-06 | 2012-09-06 | Composite power simple aircraft |
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| CN (1) | CN102849209A (en) |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103359284A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | Petrol-electric hybrid four-rotor unmanned aerial vehicle |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| CN104326084A (en) * | 2014-07-22 | 2015-02-04 | 深圳市先驰科技有限公司 | Dish-shaped aircraft |
| CN104554720A (en) * | 2014-12-31 | 2015-04-29 | 昆明天龙经纬电子科技有限公司 | Compound power helicopter |
| CN105129078A (en) * | 2015-08-24 | 2015-12-09 | 江苏绿源航天科技有限公司 | Foldable multi-power pesticide sprinkling aircraft |
| CN105217043A (en) * | 2015-11-11 | 2016-01-06 | 陆克勇 | A kind of multifunctional helicopter |
Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1073406A (en) * | 1991-12-14 | 1993-06-23 | 谭喜德 | Small-sized wing aircraft without the airport |
| US6789764B2 (en) * | 2002-09-24 | 2004-09-14 | The Boeing Company | Dual-flight mode tandem rotor wing |
| CN1869406A (en) * | 2005-05-23 | 2006-11-29 | 马同金 | Helicopter |
| CN101786503A (en) * | 2009-01-24 | 2010-07-28 | 葛振志 | Butterfly aircraft |
| CN102211661A (en) * | 2011-05-03 | 2011-10-12 | 陈洪国 | Helistat |
| CN202879793U (en) * | 2012-09-06 | 2013-04-17 | 北京工业大学 | Hybrid power simple aircraft |
-
2012
- 2012-09-06 CN CN2012103287305A patent/CN102849209A/en active Pending
Patent Citations (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN1073406A (en) * | 1991-12-14 | 1993-06-23 | 谭喜德 | Small-sized wing aircraft without the airport |
| US6789764B2 (en) * | 2002-09-24 | 2004-09-14 | The Boeing Company | Dual-flight mode tandem rotor wing |
| CN1869406A (en) * | 2005-05-23 | 2006-11-29 | 马同金 | Helicopter |
| CN101786503A (en) * | 2009-01-24 | 2010-07-28 | 葛振志 | Butterfly aircraft |
| CN102211661A (en) * | 2011-05-03 | 2011-10-12 | 陈洪国 | Helistat |
| CN202879793U (en) * | 2012-09-06 | 2013-04-17 | 北京工业大学 | Hybrid power simple aircraft |
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN103359284A (en) * | 2013-06-29 | 2013-10-23 | 天津大学 | Petrol-electric hybrid four-rotor unmanned aerial vehicle |
| CN103625632A (en) * | 2013-11-29 | 2014-03-12 | 陈科学 | Manned aircraft |
| CN104326084A (en) * | 2014-07-22 | 2015-02-04 | 深圳市先驰科技有限公司 | Dish-shaped aircraft |
| CN104554720A (en) * | 2014-12-31 | 2015-04-29 | 昆明天龙经纬电子科技有限公司 | Compound power helicopter |
| CN105129078A (en) * | 2015-08-24 | 2015-12-09 | 江苏绿源航天科技有限公司 | Foldable multi-power pesticide sprinkling aircraft |
| CN105217043A (en) * | 2015-11-11 | 2016-01-06 | 陆克勇 | A kind of multifunctional helicopter |
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| PB01 | Publication | ||
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| C12 | Rejection of a patent application after its publication | ||
| RJ01 | Rejection of invention patent application after publication |
Application publication date: 20130102 |