CN103832582A

CN103832582A - Multifunctional helicopter

Info

Publication number: CN103832582A
Application number: CN201210490947.6A
Authority: CN
Inventors: 陈昌志
Original assignee: Individual
Current assignee: Individual
Priority date: 2012-11-28
Filing date: 2012-11-28
Publication date: 2014-06-04

Abstract

The invention discloses a multifunctional helicopter which is shown in the figure. A jet engine is movably arranged on a helicopter body or a tail horizontal wing, a jet engine 9 is movably arranged on the upper end of a tail vertical wing of a small helicopter, two propeller-type engines 3 are movably arranged on a front wing 4, and foldable extending supports are movably arranged on runner blades of the propeller-type engines. The jet engines and the propeller-type engines are capable of deviating at 0-90 degrees in a reciprocating manner under the control of a hydraulic device according to the taking-off and landing flight demand, and the helicopter is selected to take off or land vertically or in a gliding manner without being limited by an environmental site. The jet engines and the propeller type engines can be simultaneously used so that vertical taking off or landing and higher supersonic flight are realized. Oil tanks are arranged in the wings and a cabin, and a multilayer combined parachute is arranged on the top of the cabin at the middle. The helicopter has multiple functions and applications of a jet aircraft and a helicopter, and a novel helicopter has a development and application prospect.

Description

Multifunctional helicopter

Technical field:

The present invention manufactures relevant with Multifunction autogyro.

Background technology:

Now the aircraft of use be military with or civilian jet-propelled, two types of aircrafts of turbo-propeller formula because of driving engine be all hard-wired, in the time taking off, land, all be unable to do without airport and runway, the field of employment scope of aircraft is very limited, cannot realize a lot of natural environment location places on land and can glide or vertical takeoff and landing flight.As the jet-propelled opportunity of combat of modern military affairs, once outbreak of war, first must capture between ourselves and the enemy " mastery of the air " for winning the victory, airfield runway is the destruction target of standing in the breach, as long as airport and runway are destroyed, there are again many advanced aircrafts again just cannot take off to display one's ability and even go up and lose and make empty initiative.This class Multifucntional autogyro that has had jet engine+propeller type driving engine to form, enemy will capture " mastery of the air " and just may to blow up airport and runway.Though the armed autogyro landing of modern use is convenient, but flying speed is too slow, dry sound is easy to greatly be found easily to suffer that ground forces attack, only should make Rear-Service Support, the autogyro of simple function has not had development prospect, be not suitable with following modern war with fast, maneuverability is taken the needs of victory by force, so flying speed is slow, function is single again, can not be according to natural environment, working space selects the aircraft of landing mode can be eliminated by following development situation flexibly sooner or later, so only have the Multifucntional autogyro of jet engine+propeller type driving engine just promising.

Summary of the invention:

The present invention can not had airport and runway facility to limit when solving existing jet plane, propellor aircraft landing completely, change jet plane, propellor aircraft and autogyro three class takeoff and landing modes are single, function singleness, the landing advantage that can facilitate everywhere of jet plane, propeller type supersonic flight speed and autogyro is perfectly incorporated into an airplane, increase function and usage range of use, make aircraft on land on warship the work of a lot of natural environments place use, arbitrarily landing is easily parked.

Can manufacture the dual-use aircraft of all kinds of more advanced practicalities with the present invention.Civilianly do public and private commercial passenger and freight transportation, sightseeing tour, 119 disaster relief fire extinguishings, 120 rescues, rescue and relief work, the lifting of super-big and overweight type New Equipment Engineering mechanical execution.Military with making fighter-bomber, carrier-borne multi-functional fighter-bomber, tanker aircraft, electronic information communication reconnaissance patrol machine, Dakota, unmanned opportunity of combat, the multi-role fighters etc. scouted.

Aircraft safety practicality, function high-mobility, multipurpose, wheeled vehicle are wide, can hypersonic flight and swing to and fly, and keep up with and be eliminated over a long time from now on, jet engine+propeller type engine new autogyro has development prospect.

The present invention is achieved in that structural principle is as follows, on the postmedian body both sides of existing use aircraft as shown in Figure 7 or tail horizontal tail two ends two aircraft jet engines 1 of head as shown in Figure 5, head propeller type driving engine 10 on the two ends of wing 11 before fixing as shown in Figure 5, handling jet engine 1 through horizontal tail intrinsic deflection hydraulic efficiency gear can need reciprocating 0 to 90 to spend slowly deflection angle by landing flight, driving engine deflection principle is as Fig. 1, shown in 2, application hydraulic pressure inflector assembly is handled control engine and is reciprocating 0 to 90 and spends slowly deflection angle and realize the aircraft landing of taking off vertically.He is like this work, as shown in Figure 3, taking off vertically landing operation, through device normal limb 8 in as the manipulation of Fig. 1 deflection hydraulic efficiency gear, make jet engine 9 slowly deflection approximately 90 spend air nozzles vertically downward, state is as shown in 9 dotted lines in Fig. 3.Through installing in wing 4 as Fig. 1 deflection hydraulic efficiency gear is handled, 2 propjets 3 of device on wing 4 are slowly turn 90 degrees partially, state is shown in dotted line, can handle like this to use and start 3 installed driving engines, open the throttle wide increases lift slowly rises body, at this moment because driving engine position of orientation has changed 90 degree, just parallel thrust of advancing is become to lift entirely, according to aerodynamic principle, the lift vertically upward that driving engine produces is greater than aircraft gravity vertically downward, aircraft just can slowly rise and take off parking original place, when aircraft rises to after suitable flying height, handle in normal limb as Fig. 1 hydraulic pressure inflector assembly, make driving engine 9 to slowly deflection approximately 90 degree of heading, air nozzle is backward as shown in 9 solid lines in Fig. 3.Handling in jet engine and handling in wing as Fig. 1 hydraulic pressure inflector assembly, airscrew engine 3 on front wing 4 is turn 90 degrees partially, state is as shown in 3 solid lines in figure, and driving engine all turns to heading to fly forward.In the time that flight arrival destination needs vertical landing, at this moment need to control well before aircraft landing and the height flying speed heading on ground, in the time closing on the correct position in landing target overhead, in the operation of vertical wing as Fig. 1 hydraulic pressure inflector assembly make jet engine slowly deflection approximately 90 spend air nozzles vertically downward, state is as shown in 9 dotted lines in Fig. 3, operating control, as Fig. 1 hydraulic pressure inflector assembly in wing, makes propeller type driving engine 3 deflections approximately 90 degree again, and screw propeller is upwards as shown in 3 dotted lines in figure.Handle to control and reduce the power of driving engine, the lift that driving engine is produced is less than the gravity of aircraft, aircraft slowly vertical landing on target location.In large type jet engine can install postmedian position as shown in Fig. 71 on body, through device on body as Fig. 1 hydraulic pressure inflector assembly handle jet engine 1 slowly 2 (or 4) propeller type driving engines 7 of deflection an angle of 90 degrees degree and front wing with manipulation work use, together deflection an angle of 90 degrees degree and realize vertical takeoff and landing work slowly.Driving engine is all becoming parastate to make aircraft glide landing by direct control driving engine.

Aircraft glides, and taking off lands operates: jet engine is all being parastate, as shown in Fig. 5,7, start jet engine 1 at operator's compartment M/C or with the automatic control operation of computer, strengthen engine throttle, operation regulates on wing the landing flight of can gliding of elevating plane control apparatus.With the taking off landing operation of gliding of propeller type driving engine: start propeller type driving engine increasing power at operator's compartment M/C or with the automatic control operation of computer, and handle and regulate the elevation and subsidence regulating device installing on wing to take off.When glide landing, can handle and use a kind of engine operation.

Aircraft takes off vertically to land and operates: propeller type driving engine and jet engine are all together used, as shown in Figure 3, with handling as Fig. 2 deflection hydraulic efficiency gear in

wing

4,2 propeller type driving engines on front wing 4 are turn 90 degrees slowly partially, state is as shown in 3 dotted lines in Fig. 3.In manipulation normal limb, as Fig. 1 deflection hydraulic efficiency gear, jet engine 9 is also turn 90 degrees partially, state as shown in phantom in FIG..It is high-power that manipulation starts 3 driving engines to add, and slowly body risen to aerial proper height with the lift that engine operation produces, then handle deflection hydraulic efficiency gear and make slowly deflection an angle of 90 degrees degree of driving engine, and driving engine is parastate and can normally flies forward.The operation of vertical landing, handle with the interior hydraulic pressure inflector assembly manipulation of wing 4, by slowly deflection approximately 90 degree of propeller type driving engine 3 on front wing 4, state, as shown in 3 dotted lines in Fig. 3, is meanwhile handled hydraulic pressure inflector assembly in normal limb, and jet engine 9 is also slowly turn 90 degrees partially, state is as shown in 9 dotted lines in figure, handle to control and reduce gradually the power of driving engine, regulate and control flying speed short transverse, aircraft slowly vertical landing in target.

For flight safety, at middle part, top, cabin, parachute compartment is set, interior device multi-layer combined type parachute, as shown in Fig. 6

institute

11,12, need the used time in driving compartment action button, first launch out guiding drogue-parachute 11, after being opened by umbellule, take compound parachute the superiors ground floor gamp out of, open successively lower floor's gamp until every layer, whole group of umbrella all opens work, in order to using and protect aircraft and personal security at hour of danger.One group, minicomputer device, medium-and-large-sized machine is pressed load carrying ability suitable many devices group number and the umbrella number of plies.One machine has many group umbrellas, and when use, before the backward machine of slave, operation is opened successively.

Brief description of the drawings:

Fig. 1 is the reciprocating deflection hydraulic actuated of separate unit driving engine schematic diagram, 1 hydraulic efficiency gear in figure, and 2 driving engine axis of deflection and gears, 3 hydraulic telescopic type racks, 4 support sliding grain, 5 hydraulic oil regulating controls, 6 fuel tanks, 7 oil pipes, 8 safety valves, 9 oil pumps.

Fig. 2 is the two reciprocating deflection hydraulic control unit of platform driving engine schematic diagrams, 1 driving engine axis of deflection and hydraulic efficiency gear gear in figure, 2 hydraulic telescopic type racks, 3 hydraulic efficiency gear telescopic shafts, 4 pistons, 5 hydraulic efficiency gear bodies, 6 support sliding grain, 7 hydraulic oil regulating controls, 8 safety valves, 9 oil pumps, 10 fuel tanks.

Fig. 3 is minicomputer glide, vertical takeoff and landing, flight lateral plan, 1 screw propeller in figure, 2 engine hydraulic axis of deflection, 3 turbo type engines, 4 wings, 5 driving compartments, 6 parachute compartments, 7 bodies, 8 tail normal limbs, 9 jet engines, 10 tail horizontal tails.

Fig. 4 is medium-and-large-sized state of flight lateral plan, 1 driving compartment in figure, 2 screw propellers, 3 turbine engines, 4 wings, 5 parachute compartments, 6 bodies, 7 engine hydraulic axis of deflection, 8 jet engines, 9 tail horizontal tails, 10 tail normal limb rudders.

Fig. 5 is the total layout front elevation one of medium-and-large-sized machine, 1 jet engine in figure, 2U type frame, 3 hydraulic pressure axis of deflection (dotted line), 4 tail horizontal tails, 5 tail normal limb yaw rudders, 6,7 hydraulic pressure inflector assembly, 8 bodies, 9 screw propellers, 10 turbine engines, 11 wings (fuel tank is inside set), 12 fuel tanks.

Fig. 6 is compound type parachute working state figure, 1 screw propeller in figure, 2 engine hydraulic axis of deflection, 3 turbine engines, 4 wings, 5 operator'ies compartment, 6 umbrella cabins, 7 bodies, 8 tail normal limbs (rudder fin), 9 jet engines, 10 tail horizontal tails, 11 umbellules, 12 compound type gamps.

Fig. 7 is medium-and-large-sized machine arrangement front elevation two, 1 jet engine in figure, 2U type frame, 3 horizontal tails, 4 vertical tails, 5 bodies, 6 screw propellers, 7 propjets, 8 wings (fuel tank is inside set), 9 fuel tanks.

Detailed description of the invention:

Embodiment example 1, body main structure layout as shown in Figure 7, by two jet engine 1 heads in body postmedian, two ends by propeller type driving engine 7 heads at fixed wing 8, on propeller type driving engine runner, propeller blade is equipped with umbrella frame posture and stretches that support Folding device is movable to be installed, runner bucket hydraulic efficiency gear manipulation on driving engine can be stretched support work and can folding be placed, runner bucket is handled and is stretched after support expansion through hydraulic efficiency gear, before engine operation, in rotating shaft, mechanical lock ingot device is controlled locking automatically, and driving engine can be started working.Driving engine is the level of state, and handles and uses the landing of taking off of can directly gliding of propeller type driving engine or jet engine.Take off vertically, the deflection hydraulic efficiency gear of handling driving engine side device on body turn 90 degrees driving engine 1 partially, and driving engine and body are in vertical state.Handle the hydraulic pressure inflector assembly of wing 8 interior devices, the propeller type driving engine 7 on front wing 8 two ends is spent through hydraulic efficiency gear operational deflection 90, driving engine and body are in vertical state.4 driving engines are started in manipulation, strengthen engine throttle, the lift that driving engine produces slowly rises to body in the air, when rising to after suitable flying height, handle deflection hydraulic efficiency gear and make slowly deflection approximately 90 degree of 4 driving engines, driving engine and body are parastate and can fly to advance and also can swing to flight.When aircraft completes after the complete normal parallel flight of vertical uplift take-off process, at this moment capable of saving fuel oil can use propeller type driving engine or jet engine flight.In the time of needs vertical landing, jet engine and propeller type driving engine are all worked to use through hydraulic pressure inflector assembly and handle and slowly partially turn 90 degrees, be all placed in the state of taking off vertically, control flying height and make slowly vertical safe falling of aircraft with direction.Minicomputer is provided with 2 fuel tanks and 2 cover propeller type engine hydraulic inflector assembly in wing.Medium-and-large-sized machine can arrange spare tank in cabin.

For protecting flight safety, be provided with parachute compartment 6 in nacelle top as shown in Figure 6, one group of multiple field combination parachute is housed, 11 is guiding umbellule, 12 is compound type work gamp, and when work, action button is first launched out umbellule and taken every layer of gamp out of again, until one group of combination parachute standard-sized sheet.

In the time of needs hypersonic flight, 4 driving engines can use simultaneously, and on machine, all manipulation control all arranges manually and automatic two covering device management systems.Computer automatic operation control for automatic operation control apparatus system.Aircraft instrument used is all installed at driving compartment with manual and automatic two covering device management systems.

Embodiment example 2, body main structure is arranged as shown in Figure 5, by two jet engine 1 heads afterbody horizontal tail 4 two ends after body.As shown in Figure 3, by 1 jet engine head in afterbody normal limb after minicomputer topmost as shown in Fig. 39.As Fig. 5 by propeller type driving engine head on the two ends of fixed wing 11, driving engine is the level of state, and needs that gliding takes off and can handle to use the propeller type driving engine l0 landing of taking off of directly gliding.Need to take off vertically, handling afterbody horizontal tail or normal limb intrinsic deflection hydraulic efficiency gear makes jet-propelled starting need to partially turn 90 degrees by taking off vertically, state is as shown in 9 dotted lines in Fig. 3, propeller type driving engine 3 on front wing two ends will be turn 90 degrees partially through hydraulic efficiency gear operation, state is as shown in 3 dotted lines in Fig. 3, the lift that open the throttle wide 3-4 platform driving engine produces slowly rises to body in the air, when rising to after suitable flying height, operation hydraulic efficiency gear makes slowly deflection approximately 90 degree of 3-4 platform driving engine, state, as shown in 9 and 3 solid lines in Fig. 3, can advance by normal flight.When being that capable of saving fuel oil at this moment can be with the flight of propeller type driving engine or jet engine after aircraft normal flight.While wanting vertical landing, jet engine and propeller type driving engine are slowly turn 90 degrees to Fig. 39,3 dotted line states that are placed in partially, control flying height and make slowly vertical safe falling of aircraft with direction.In wing, be provided with 2 fuel tanks and 2 cover engine hydraulic deflection handling device.In horizontal tail or the in-built driving engine deflection angle hydraulic control unit that is equipped with of normal limb.With 1, on top, cabin, compound type parachute compartment is set.In the time of needs hypersonic flight, 4 driving engines use simultaneously, on machine, all manipulation control all arranges manually and computer control two covering device management systems automatically, and aircraft instrument used is all installed at driving compartment with manual and automatic two covering device management systems.

Claims

1. Multifunctional helicopter is in two jet engines of body postmedian both sides head, at two propeller type driving engines of two ends head of both sides, body middle part wing, in wing He in cabin, fuel tank is set, at body afterbody, horizontal tail and normal limb are set, cab device have aircraft instrument, manually and computer automatically control operating control; The jet engine of body postmedian device is handled through hydraulic efficiency gear, can spend slowly deflection angle by the needs of aircraft glide landing or vertical takeoff and landing and flight reciprocating 0 to 90; 2 propeller type driving engines of two ends head of wing before body, the deflection hydraulic efficiency gear installing in wing is handled, and starts reciprocating 0 to the 90 degree deflection angle of function to make aircraft vertical takeoff and landing; Can utilize and on machine, start function deflection angle to realize to swing to flight, in the time of needs vertical takeoff and landing before and after driving engine use simultaneously, aircraft can be at different environment fields selected glide or vertical takeoff and landing, driving engine all uses the aircraft can hypersonic speed flight simultaneously.

2. microminiature Multifunctional helicopter two propeller type driving engines of head on the two ends of front flight wing, jet engine driving engine of top head on afterbody normal limb, hydraulic efficiency gear maneuvering engine can reciprocating 0 to 90 be spent slowly deflection angle by aircraft need to being of landing or vertical takeoff and landing flight of gliding in premenstrual wing and in afterbody normal limb.

3. Multifunctional helicopter propeller type driving engine propeller blade is movable installs, umbrella frame posture is housed and stretches support Folding device, runner bucket is handled and can be stretched support work and can folding place through hydraulic efficiency gear, runner bucket through hydraulic efficiency gear handle stretch support launch after on runner shaft mechanical lock ingot device automatically control locking.

4. Multifunctional helicopter has one or more parachute compartments at cabin main body middle part ejection device, in umbrella cabin, there is one group of compound type parachute, there is a guiding umbellule in the Mei Zu multi-layer umbrella the superiors, when use in driving compartment action button, first launch out umbellule, open rear guiding by umbellule and take last layer gamp out of, after being opened by the superiors' gamp, drive and open lower surface layer gamp successively, until multiple layer combination gamp opens work entirely.