CN110466759A

CN110466759A - A kind of stably and controllable saucer-like air vehicle and its lift are simultaneous to turn to engine transmission structure

Info

Publication number: CN110466759A
Application number: CN201910400447.0A
Authority: CN
Inventors: 秦天乐
Original assignee: Individual
Current assignee: Individual
Priority date: 2019-05-14
Filing date: 2019-05-14
Publication date: 2019-11-19

Abstract

The invention discloses a kind of stably and controllable saucer-like air vehicle, which additionally advances engine, ventral sledge shape undercarriage and adjustable air power part by central differential coaxial double-oar, circular bodies, pair of right and left upwards and guided missile hatchcover forms.The aircraft provides hover lower lift and steering and the lift elevation angle by differential coaxial double-oar, is fast forwarded through by advance engine and presses the angle of depression, tilted by ventral aerodynamic features.The advantage of the present invention compared with the prior art is: being provided simultaneously with: being owned by fast steering ability, fast speed under any circumstance, rapid vertical landing can hover, higher fuel utilization ratio, less exposed movable part, higher plate armour utilization rate, the tail of mountable reactive armor.

Description

A kind of stably and controllable saucer-like air vehicle and its lift are simultaneous to turn to engine transmission structure

Technical field

The present invention relates to a kind of dish-like flights for not depending on airport vertical lift, hovering, all around fly, fast forwarding through Device.

Background technique

The a wide range of conventional flying for long time mode for successfully creating lift known at present has fixed-wing, rotor and spray Gas, fixed-wing can rapid flight, rotor can hover can low-speed handing, directly use jet that can make arbitrarily in the short time as lift It operates but not necessarily stable also not lasting.

It is just very miserable that a wiping ground is just planted in existing most conventional fixed-wing stall, therefore dare not be too near to ground；Helicopter speed compared with Slowly feel insufficient and for the relatively fixed wing of the utilization efficiency of energy.

Summary of the invention

The purpose of the present invention is to overcome the above shortcomings and to provide the offline mode that one kind more balances.

The present invention is that a kind of use with one has enough lift resistance ratios left and right slightly from time positive air force under forward travel state Structure and possess under floating state enough lift return forward air inlet mouth reserved asymmetry circular bodies before and after position (for Consider that body possesses certain indent radian in central engine efficiency imagination, leading engine air inlet, which can enable, generates big model above more than half body Low pressure is enclosed, lower section generates a wide range of high pressure) (possesses for the possible unstable body of hovering of solution and centainly control back positive air force Furthermore shape can simultaneously be cooperated additional under pitching and ventral in hovering to the direction pressure release of secondary engine air admittance mouth by major-minor engine Aerodynamic features are voluntarily returned just) (see Fig. 1) to the front upper plus being located at ventral spiral shell by the imagination of generator control differential in center Paddle gas outlet position position air inlet to the rear is revolved, the coaxial double-oar exhausting of the turboaxle motor driving of the top gas outlet in tail portion is poor Fast propeller, left and right is plus whirlpool paddle or exhausting whirlpool paddle or turbojet engine, since be more likely to can be with for the generator on main screw Can be used be driven by electricity compressor the jet engine without puff prot turbine, even can deviate jet air inlet position Placement location propeller is made into the electric propeller punching engine that air inlet is flat or fan-shaped very little operating rate is very wide.

Drive mechanism needed for coaxial double paddle differential steerings be contemplated that two as it is similar with automobile differential (see Fig. 2) (black) engagement of at least six bevel pinion of structure clamp intermediate small two-sided conical ring (powder) again in the conelet of upper big ring (purple) Exported on lid under conelet (black) of (black) upper and lower big ring (purple) annulus (red, yellow) (conelet is independent rotated with big ring but with big ring list Solely connection), wherein one output annulus can pick out a pole (Huang) pass through the other end output ring reach greater density, away from The farther output of the freestone heart.Finally transmission shaft (green) (see Fig. 3) is connected between two big ring again.' later output end can be with Switchable generator is loaded onto when brake, generator can accelerate the other end to the deceleration of one end in the place of dress generator.'

The double paddle exhausting differential propeller positions of central coaxial are forward and body shape is to the height for accumulating it below body Pressure air is more likely to flow forward, for turning to, hovering, retreat and draw the elevation angle.

Left and right engine turbofan or propeller position are higher, provide the effect at the pressure angle of depression and low-speed forward, gas-blowing outlets position It sets normal.Or jet provides the angle of depression, paddle fan it is normal all can, can also be with there are also propeller is put partially.

Finally put adjustable air power plank in ventral or so control back just, can also when sledge shape undercarriage use, such as Fruit can also be when the protection cap of missile bay or protection weapon if needing.

It nearly anti-machine gun can be installed on the lower strafes backward in tail and shoot down air defence missile, the invention tail is even more to be very suitable for Reactive armor is installed.

Advantage of the present invention is the simultaneously fast steering that can hover for a long time, and the theoretical velocity upper limit is higher, can be flown not against aileron, Body latter half takes off and is exceedingly fast without weakness, and it is smaller to take up an area opposite helicopter, and it is higher to install armoring efficiency, protection with it is motor-driven comprehensive It is higher to close limit.

If stability deficiency can install spoiler or adjustable spoiler or empennage above and below tail.

This patent is a new and effective complete flight system, any to belong to this patent with the flight of this patent institute's how Protection scope, any improvement to this flight system have no effect on this patent protection.

All structures with innovation meaning of this patent, design be it is contemplated that, belong to this patent protection Range.

Detailed description of the invention:

Fig. 1 is the Freehandhand-drawing top view of aircraft general shape；

Fig. 2 is the part Freehandhand-drawing top view that opposite body quickly moved and itself had movable part；

Fig. 3 is the side view description figure of the drive position internal structure positioned at aircraft circular bodies center.

Claims

1. a kind of stably and controllable saucer-like air vehicle, it is characterised in that: possess and be used in combination to central differential coaxial double-oar reserved space Above and below the body that is generated by differential coaxial double-oar of body limitation the circular bodies of the additional lift of high-low pressure air flowing generation and according to The aircraft for being hovered and being turned to by central differential coaxial double-oar.

2. the stably and controllable saucer-like air vehicle of one kind according to claim one, a kind of stably and controllable saucer-like air vehicle needs to utilize Coaxial double-oar differential mechanism needed for central differential coaxial double-oar, which is characterized in that two annular tooths directly driven by driving shaft Wheel drives the dry planetary gear of promise for being connected to its inner wall by bearing, and a small annular tooth is clamped in engagement among two groups of planetary gears Output gear under taking turns and engage above the upper planetary gear upper output gear, engaging below lower planetary gear, output gear can connect A transmission shaft is connect across central annular gear and another group of output gear.

3. a kind of stably and controllable saucer-like air vehicle according to claim one, it is characterised in that: it is total to rely primarily on central differential The double paddle lift of axis hover and take off and possess additional fixed forward engine.

4. a kind of stably and controllable saucer-like air vehicle according to claim three, it is characterised in that: lift engine is forward and advances Engine air admittance mouth is top downward, and gas outlet or reinforcing gas outlet are on the lower.

5. according to a kind of controllable stable saucer-like air vehicle of claim one or three or four, it is characterised in that: ventral is equipped with can Serve as the adjustable air power part of sledge shape undercarriage and guided missile hatchcover.