CN102991672A

CN102991672A - Variable power wing vertical short-range taking off and landing aircraft

Info

Publication number: CN102991672A
Application number: CN2012101545548A
Authority: CN
Inventors: 宋新民
Original assignee: Individual
Current assignee: Individual
Priority date: 2012-05-18
Filing date: 2012-05-18
Publication date: 2013-03-27

Abstract

The invention discloses a variable power wing vertical short-range taking off and landing aircraft. According to the aircraft, wings are formed by movably hinging a middle horizontal beam shaft, a vertical pressing tooth disc and a body, wherein the middle of a horizontal beam is fixed with the body; two sides of the horizontal beam stretch into the wings by a certain length; the end of a beam shaft and a key bearing group of a root roller are linked and supported; the working principle of the vertical pressing tooth disc is the same as the working principle of a movable ground disc or an excavator below a tank archibald tower and a horizontal movable ground disc below a crane, only two sides of the body are vertically hinged with the wing, and driven teeth of an inner turntable are driven through a transmission gearbox, so that the wings rotate forwards, upwards and downwards to finish various high-difficulty actions. The advantages of helicopters and fixed wing airplanes are integrated, and the aircraft takes off and lands within a vertical short range.

Description

The vertical short takeoff landing of variable power wing aircraft

This patent can be made all kinds aircraft, civil aircraft, can make various large, medium and small transport planes, fly loop wheel machine, produce various large, medium and small passenger planes, the airship of going sightseeing waterborne, dirigible, flying trapeze's device, unmanned plane, model airplane machine, also can make hovercar etc.

Military large, medium and small fighter plane, Unmanned Combat Aerial Vehicle, unmanned scout bomber, early warning plane, scout, the military multifunction transport machine of fuel charger, hydroairplane, rocket ship, the dirigible etc. made.

This patent divides: front power wing (canard wing), the medium power wing (main wing), rear power wing (empennage) and horizontally rotate vertical tail (can add rear upset), rear power wing can be installed on the vertical tail.

Can do various combination manufacturings by purposes produces.

This patent invention: the engine installation of the vertical short takeoff landing of variable power wing aircraft is located on the wing, can install screw propeller explosive motor, turbine, turbofan jet engine, rocket engine, electronic compressed air engine etc. and after the various propelling units that go out of new invention all can be used to as the power resources of installing on the wing.Wing links with vertical pressure fluted disc with the horizontal beam axle with body, and blimp can alone beam axle or pressure fluted disc.Change the wing angle by electrical motor and change speed gear box band dynamic pressure fluted disc passive tooth and upwards cooperate engine speed, vertically short takeoff landing and hovering, but changing the wing front and rear angles can turn to tune to the back upper place inverted flight, one on the other can about turn or rolling, forward can before fly to climb, finish various exceedingly difficult movements, point-to-point transporting.But horizontal take-off landing that heavy duty is fuel-efficient.Empennage steering capability for a change, the horizontal beam axle can make a variation into " V " type beam axle.Press the fluted disc same equal angles that also tilts.The wing strut bar is housed improves the landing functional stabilization that takes off.

Description of drawings

(Figure of description diagram)

Fig. 1: figure is the flat birds-eye view that flies of variable power wing aircraft.

Fig. 2: figure is the variable power wing aircraft landing hovering lateral plan that takes off vertically.

Fig. 3: figure is variable power wing back upper place inverted flight lateral plan, can aloft do to hover and turns to and the action such as tune as changing the wing angle again.

Fig. 4: figure is horizontal beam axle figure.

Fig. 5: figure is bow-backed beam axle figure.

Fig. 6: figure is hollow beam axle figure.

Fig. 7: figure is the beam axle figure that slightly attenuates.

Fig. 8: figure is taper beam axle figure.

Fig. 9: figure is inner sleeve two half beam axle figure.

Figure 10: figure is that inner sleeve is stirred beam axle figure mutually.

Figure 11: figure vertically presses fluted disc inner rotary table front elevation.

Figure 12: figure vertically presses fluted disc inner rotary table lateral plan.

Figure 13: figure is inner rotary table ball bearing of main shaft picture group.

Figure 14: figure vertically presses the outer cover plate front elevation of fluted disc.

Figure 15: figure vertically presses the outer cover plate lateral plan of fluted disc.

Figure 16: figure is internal and external disk combination sectional drawing.

Figure 17: figure is that the roller key is vertically pressed fluted disc inner-outer sleeve positive combination figure.

Figure 18: figure is that the roller key is vertically pressed fluted disc inner-outer sleeve side combination sectional drawing.

Figure 19: figure is that the roller key is pressed fluted disc internal and external disk and roller key combination sectional drawing.

Figure 20: figure is that roller is pressed fluted disc overcoat front elevation.

Figure 21: figure is that roller is pressed fluted disc internal tooth rotating disk front elevation.

Figure 22: figure presses fluted disc running roller front elevation.

Figure 23: figure presses fluted disc running roller lateral plan.

Figure 24: figure is that running roller is vertically pressed fluted disc overcoat and interior fluted disc and running roller combination front elevation.

Figure 25: figure is that running roller is vertically pressed fluted disc overcoat and interior fluted disc and running roller combination lateral plan.

Figure 26: figure is that the outer tooth disk running roller is pressed fluted disc overcoat figure.

Figure 27: figure is that the external tooth running roller is pressed fluted disc, inner rotary table front elevation.

Figure 28: figure is that the external tooth running roller is pressed fluted disc running roller front elevation.

Description of drawings

(Figure of description diagram)

Figure 29: figure is that the external tooth running roller is pressed fluted disc running roller lateral plan.

Figure 30: figure is that the external tooth running roller is pressed fluted disc assembling front elevation.

Figure 31: figure is that the external tooth running roller is pressed fluted disc assembling lateral plan.

1, horizontal beam axle.2, key bearing carrier ring.3, fuselage.4, inner sleeve.5, stir mutually the beam shaft sleeve.6, link wing.7, inner rotary table.8, outer cover plate.9, inner rotary table wing connecting bore.10, outer disk fuselage connecting bore.11, ball grooves.12, inner rotary table passive tooth.13, ball bearing of main shaft group.14, roller key bearing set.15, roller gear.

Claims

1. this patent is: power is on wing, wing links with vertical pressure fluted disc by the horizontal beam axle with body, wing can with the body vertical rotary, the aircraft of change of flight direction can be made the unprecedented aircraft aircraft such as various aircrafts, airship, dirigible, hovercar, unmanned aerial vehicle, model airplane machine, flying trapeze's device, rocket and hydroairplane.Can hold autogyro and fixed wing aircraft advantage, fly surely, load carrying ability is large, speed is fast, the multiple exceedingly difficult movements such as landing, hovering, inverted flight, upset of can taking off vertically.On the variable power wing wing various power engines can be installed, can fill single-shot, two and multiple-motor unit.Vertical tail can horizontally rotate driving engine be contained on the vertical fin can after the landing of overturning.But aircraft is Horizontal Take-off and Landing also, and distance is very short in airfield runway.The fuel-efficient usable runway landing of heavy duty.Can fill the support feeler lever on the wing and improve the landing functional stabilization that takes off.

The independent use of the various functions of above claim also can multinomially be used in combination.