CN106494619A - Movable wing formula aircraft-full spatial domain, global function, full rate that three complete empty days are straight - Google Patents

Abstract

Three complete empty days are straight, and movable wing formula aircraft is with a kind of brand-new operational mode, i.e. straight wing is flown in pointer angle movement with the driving cabin (fuselage) of wing central rotatable, collect the great achievement of multiple aircrafts, with the design of brevity and lucidity, it is made up of three big key element (three-major-items)：1st, around the straight wing of central shaft activity；2nd, driving cabin one coaxial with active force (the power extension set wing is upper and lower two kinds)；3rd, there is the servo power of small-sized Multidirectional-moving on the high aircraft wing both sides of large-scale or mobility, the platform speed scope is very wide in range, it is applied to all machines existing and space travel, especially wing box loading type, comparatively advantage is more, such as resistance is little, speed is fast, stealthy good, carrying capacity is big, loading species is more etc., can derive various multi-series multifunctional usage aircrafts with familial.Innovation does not just develop, this initiative flying platform, furthers and has obscured the restriction and boundary that flies between empty day, substantially increase utilization rate and degree of freedom to international spatial domain day domain, there is epoch-making meaning, the trend of world's sky day flight will be led.

Description

Movable wing formula aircraft-full spatial domain, global function, full rate that three complete empty days are straight

First, technical field

The aircraft of the present invention is that is, straight wing is flown in pointer angle movement with the driving cabin (fuselage) of wing central rotatable, and its maximum feature is with a kind of brand-new operational mode：

1st, velocity interval is very wide in range.

2nd, the platform is applied to all machines existing and space travel.

3rd, especially wing box loading type, comparatively advantage is more, and such as resistance is little, speed is fast, stealthy good, carrying capacity is big, loading species is more etc..

2nd, background technology

The shortcoming of prior art：

1st, wing formula aircraft advantage is more, but manipulates hardly possible, at present straight movable wing formula aircraft in the world also not truly, and only minority draws close design to which, B-2 such as made in U.S.A etc., but all speed is not high, and manipulation difficulty is big, and poor sensitivity, cost are high.

2nd, miscellaneous more than present aircraft species, technical limitations are more, such as the not winged high-altitude in low latitude, the not winged space flight in high-altitude etc., and substantially, technology span is big for boundary.

3rd, from the perspective of in speed, the not winged high speed of low speed, the not winged hypersonic speed of high speed is to space flight.

4th, speed is high or large aircraft needed for runway long, it is desirable to high, equal hardly possible low speed STOL, and most accidents occur in landing, poor stability.

5th, poor universality, most of aircrafts are unable to a tractor serves several purposes, and utilization rate is low, and machine is more, spare part is more and maintenance management complicated, barely satisfactory.

3rd, content of the invention

The great achievement of the multiple aircrafts of flying platform collection of the invention, with the design of brevity and lucidity, is made up of three big key element (three-major-items)：1st, around the straight wing of central shaft activity；2nd, driving cabin one coaxial with active force (the power extension set wing is upper and lower two kinds)；3rd, there is the servo power (accompanying drawing 1,2) of small-sized Multidirectional-moving on the high aircraft wing both sides of large-scale or mobility.

Possesses above feature, the platform just can derive various multi-series multifunctional usage aircrafts with familial, and this initiative flying platform has epoch-making significance, will lead the trend of world's sky day flight, and its advantage is as follows：

1, the aircraft speed scope is big and wide, with wing and driving cabin variable angle, speed can be from zero-Low-Medium-High-ultrahigh speed-space flight (accompanying drawing 7, 8), certainly, when hypersonic speed and space flight, body improves corresponding structural strength, thermally protective materials are installed additional and the corresponding power that changed the outfit, for example, with the carrier-borne aircraft (accompanying drawing 3) of the platform technology, can low speed or VTOL and hovering etc., and other aircrafts such as bomber, transporter, passenger plane, fuel charger etc., extension set body loads (accompanying drawing 4, 5) (accompanying drawing 6) two types are loaded with wing box, can STOL, flown with each speed and supersonic cruise.

2nd, the platform can be accomplished according to each machine needs：

(1) wing is changeable, changeable, can thickness can be thin, can width can be narrow；

(2) material is also different with structural strength；

(3) power matching is also different as requested, changeable, the amount doesn't matter, and active force is may be disposed on aerofoil under (accompanying drawing 2,5,10) or the wing (accompanying drawing 1,4,9), power species is also different, such as hypersonic speed when punching type or super combustion engine etc., with rocket-powered during space flight.Possess above feature, just made the function that can cover nearly all aircraft.For example：

1. make destroy, Hong machine, transporter, fuel charger, passenger plane etc., except can be in addition to STOL, can supersonic cruise, all faster than guided missile during high speed, because during high speed, resistance is minimum, it is equal to power to become speed, voyage and load is increased, has striven for a succession of good effect such as time again；

If 2. the platform increased structural strength and thermal protection, changed the outfit hypersonic speed power, can accomplish to beat within one hour all over the whole world in military affairs；

When 3. needing space flight, except strengthening and changed the outfit in addition to corresponding technical equipment, can by punching transmitting (accompanying drawing 7) on thrust-augmented rocket or large aircraft, during return can the full short distance of horizontal femto-ampere land；

4. the familial development of the platform, standardized production eliminate many troubles, simplify technique, reduce flow process and manpower, have saved fund, have accomplished that various parts intercommunication is exchanged, and easy care loss of weight amount etc. has a lot of advantages.

3rd, the use to the flying platform, this according to grafting and displacement that task and demand carry out modularity task bag at any time, can accomplish a tractor serves several purposes as buffet, and efficiency high militarily can be used as the beforehand research platform of opportunity of combat after surpassing for six generations.

4th, not high to airport requirements, because of its horizontal winged STOL, special machine can also VTOL (accompanying drawing 3), also have stealthy function, be wing box loading type such as passenger/cargo transport, bomber, reconnaissance plane etc. (accompanying drawing 6) by which.

5th, the Flight Vehicle Design and manufacture difficulty are relatively low, and most machines can make multiple innovative, the aircraft of high-performance high performance-price ratio with existing ripe technology and equipment in the short time, the stealth bomber which is made can carry out high-altitude strategic core Maneuver Penetration at a high speed.

6th, because of the design of its uniqueness, multiple exceedingly difficult movements are awing done and is brought to a halt in the air, inverted flight, horizontal movement overhead, reversely flight of turning around, arbitrarily etc., have a vector spout can hovering and VTOL and instantaneous maneuver etc. for radius of turn.Little airport can two low-powers regurgitate short distance landing.

7th, the appearance of the flying platform, furthers and has obscured the restriction and boundary that flies between empty day, substantially increase utilization rate and degree of freedom to international spatial domain day domain, the existing Advanced Aircraft that other country brags about is thrown on one side far away, not worth mentioning, Chinese emergence is made, strengthen the army rich people.

4th, illustrate

Fig. 1,2 be schematic diagram, be the three-major-items (key element) of this flying platform i.e.：1. wing；2. fuselage and active force；3. two low-power of wing two ends.Fig. 1 is active force low-laying type, and Fig. 2 is active force top loaded type.

Fig. 3 is schematic diagram, is the VTOL type of this aircraft series.

Fig. 4,5 are three-view diagram, are that passenger-cargo fuselage loads series, and Fig. 4 is active force low-laying type, and Fig. 5 is active force top loaded type.

Fig. 6 is schematic diagram, is that passenger-cargo the banging of wing boxes of wings load mode waits large aircraft series.

Fig. 7 is schematic diagram, is the radiation pattern with this flying platform as maternal space shuttle, is 1. rocket launching, 2. launches for large aircraft.

Fig. 8 is three-view diagram, is the movable wing formula space shuttle (in order to illustrate wing slightly long) of the present invention.

Fig. 9,10 are three-view diagram, are as a example by destroying Hong machine and the power facilities of general aircraft, are arranged based on Fig. 9 under power wing, and Figure 10 is arranged on aerofoil for active force.

5th, specific embodiment

When the platform is horizontal winged awing, wing and wing center driving cabin free to rotate into 90 jiaos, now, aircraft drag is maximum, lift is maximum, speed is minimum, and as angle is tapered into, then resistance is also diminishing, speed becomes big, when angle is zero, fastest in the case that power is constant.And gesture stability, in addition to the control panel of wing west, because driving cabin interactive as circumference angle of cultrating in aerofoil center and wing, two little servo powers are placed in wing both sides, can also coordinate and do angle increase and decrease, also active force is manipulated with the vector jet of 2 low-powers, such as scalar potential spout, 2 low-powers can be set to spray outside universal posture Three-dimensional movable, and such many kinds of force cooperates to reach flight optimization state.Also wing both sides low-power can be not provided with according to purposes and the machine for needing, such as the not high aircraft of small-sized or maneuverability requirement.

Claims (6)

1. straight aerofoil centrally disposed can circular-rotation driving cabin.

2. active force is synchronous with driving cabin consubstantiality.

3. active force may be disposed at aerofoil up or down.

4. two servo low-powers are placed in wing both sides, can simultaneously or independently do the movement of multi-angle spout or the movement of vector spout, flexibly effectively to match somebody with somebody The needs of flight attitude and speed controlling are closed, and two servo low-powers calculate reinforcing during full speed, and motor-driven or speed reduction in landing is calculated when regurgitating.

5. loading form is divided into：(1) wing box is loaded；(2) fuselage is loaded；(3) wing box fuselage combined shipment.

6. the unique offline mode for being formed by above key element.