CN104139857A

CN104139857A - Non-shaft spin aircraft

Info

Publication number: CN104139857A
Application number: CN201310167313.1A
Authority: CN
Inventors: 苏汀荣
Original assignee: Individual
Current assignee: Individual
Priority date: 2013-05-09
Filing date: 2013-05-09
Publication date: 2014-11-12

Abstract

The invention discloses a non-shaft spin aircraft which is great in speed and completely different from current human aircrafts in flight mode and structure. The non-shaft spin aircraft is a cone structure, completely symmetrical high thrust engines are arranged on a chassis; the engines start, when the engine thrust resultant force is zero, the aircraft in situ accumulates and rotates, with the passage of time, the aircraft line speed is higher and higher, the accumulated kinetic energy is higher and higher; when tremendous aircraft kinetic energy is accelerated, by appropriate adjustment of each engine thrust, the aircraft is applied by a certain resultant force, and under the effect of the resultant force, the aircraft flights out in a huge initial velocity and the spiral trajectory. Due to the huge rotating speed, when an appropriate weapon system is installed, an excellent appropriate defensive system is formed; because the aircraft flight speed is greater than the current missile speed, the aircraft not only can instantly arrive an above target, enemy planes and guided missiles are unable to intercept, the aircraft is an excellent bomber. With the development of engines, aerospace materials and other technologies, the aircraft flight speed may reach thousands of times and tens of thousands of times of the speed of sound (in theory is more and more big, until is infinite), and the aircraft is a best tool to explore the universe and develop and use alien resources.

Description

Shaftless spin aircraft

This is a very fast vehicle technology, it is constantly to accumulate on the spot kinetic energy by aircraft, then by accumulated huge kinetic energy abrupt release being completed to very fast flight

We know, present artificial aircraft, substantially be all rectilinear flight, speed slowly increases by zero, be subject to fuel, material, atmospherical drag ... impact etc. various factors, flying speed and distance are subject to great restriction, and shaftless spin aircraft has adopted the principle of kinetic energy accumulation and outburst, aircraft is constantly accumulating in the process of kinetic energy on the spot, because being rotates on the spot, atmosphere is the friction force of atmosphere to aircraft surface to the resistance of aircraft, be that (P is atmospheric pressure to F=PS μ, S is the face area of aircraft, μ is friction coefficient), because aircraft rotates on the spot, P and S are definite value, like this, as long as aircraft surface smooth enough, when aircraft accumulation of energy, the energy that is subject to atmospherical drag and consumes is also just minimum, meanwhile, the initial velocity of aircraft can reach very huge, and aircraft neither rectilinear flight, but spiral track flight, this flying method, can greatly eliminate the resistance of atmosphere to aircraft, save a large amount of energy, made aircraft fly fartherly sooner.

The technical solution adopted for the present invention to solve the technical problems is:

1. kinetic energy accumulation: be first symmetric points aircraft manufacture Cheng Yiqi center-point, the cone structure of full symmetric, on the limit on its round chassis, completely symmetrically arrange some performances and the duplicate high thrust motor of thrust, and the thrust direction that all driving engines are produced is consistent on circumference, be all cw or be all conter clockwise, like this, when all driving engines start also synchronized operation simultaneously, to promote aircraft and do to accelerate on the spot rotation, at this moment, aircraft linear velocity is increasing, and kinetic energy is also increasing.

2. flight: can rotate on the spot accumulation of energy in order to meet aircraft, the driving engine of employing must be paired existence, full symmetric, it can be 2,4,6,8 ... Deng, according to aircraft performance and structural requirement, adopt 4 the most suitable, at this, take 4 driving engines and illustrate as example.When four driving engines move with all strength, two engine thrusts of every symmetry, take the center of underbody is symmetric points, equal and opposite in direction, opposite direction, making a concerted effort is zero, to take making a concerted effort that the center of underbody is symmetric points be also zero to the thrust of 4 driving engines, and aircraft accelerates rotation on the spot.When aircraft has accumulated enough kinetic energy and need to fly, suitably adjust the thrust of four driving engines, make it non-vanishing with joint efforts, aircraft, under force action, flies away the initial velocity with huge.Because aircraft now remains, rotating, resultant direction constantly changes, and so just makes aircraft do spiral flight towards a fixed-direction and advances.Because engine thrust size can be adjusted at any time, their size and Orientation of making a concerted effort also just can be adjusted at any time, and resultant direction can be adjusted into the unspecified angle on 360 degree circumference, thus aircraft can be at any time, change of flight direction arbitrarily.

The effect of patent of the present invention is, the flying speed of aircraft is to be determined by the kinetic energy of its accumulation substantially, as long as engine thrust is enough large, the time accumulates kinetic energy perhaps enough filling, its flying speed will be huge and surprising, for current world technology level, aircraft speed will reach 100 times of velocity of sound and still be relatively easy to, along with constantly advancing of world technology level, aircraft speed also will be increasing, theoretically, the light velocity can be reached until infinity is the theoretical foundation that aircraft flight speed increases development.

Below we are furthermore bright by reference to the accompanying drawings

Fig. 1 is engine position figure

Fig. 2 is basic structure front elevation

Fig. 3 is engine thrust figure

In Fig. 1,1 is #1 driving engine, and 2 is #2 driving engine, and 3 is #3 driving engine, and 4 is #4 driving engine, and 5 is that four driving engines of underbody are that full symmetric is arranged on underbody.

In Fig. 2,1 reinforced support that is aircraft skin, 2 is control cabin, and 3 is control cabin floor, and 4 is engine exhaust port, and 5 is access way, and 6 is Universal pulley, and 7 is bunker.

The structure of aircraft is cone, and for the skyborne stability of aircraft, the quality of the aircraft overwhelming majority should be placed in bottom, and bottom is driving engine and bunker, and middle part is control cabin, and for the ease of aircraft landing, engine exhaust port can be adjusted up and down; For the atmospherical drag that reduces to be subject to when aircraft moves in air environment, aircraft appearance must be very smooth smooth.Universal pulley is the same with the alighting gear of aircraft, can pack up in-flight.

Fig. 3 is four suffered engine thrust figure of aircraft, and 1 is #1 engine thrust, and 2 is #2 engine thrust, and 3 is #3 engine thrust, and 4 is #4 engine thrust.

Suppose that thrust 1,2,3,4 corresponding orientation are east, south, west, north, when aircraft will fly toward due east direction, can stop #2, #3, #4 engine operation simultaneously, now aircraft will be done the flight of spiral fast speed eastwards, when southeastwards direction flight of aircraft, can stop #3, #4 engine operation simultaneously, now aircraft is incited somebody to action southeastward direction and is done the flight of spiral fast speed, so analogize, by adjusting each engine thrust size, aircraft flight direction can be adjusted into 0 degree to 360 and spend direction at any angle.

Claims

1. the very fast aircraft that helical trajectory flies, its driving engine is arranged symmetrically on four limits on the round chassis of aircraft, by the mode of shaftless rotation, accumulates kinetic energy, and by adjusting the thrust size of driving engine, realizes the release of kinetic energy.

2. cone structure.

3. broken away from the constraint of axle, heading can freely be adjusted to unspecified angle between 360 degree at 0 degree at any time.