Aircraft power design scheme

Abstract

The invention discloses an aircraft power design scheme, belongs to the field of aircraft power design, and aims to solve the problems of aircraft power, energy, acceleration and the like. On the basis of a previously applied patent'dynamic vacuum hemisphere theoretical technology ', two vacuum hemispheres are designed to be deep and shallow and are overlapped and vacuumized to be connected with a valve core of a valve to be connected with a spray pipe, ten pipelines are utilized to work and operate simultaneously, and the vacuum hemispheres are rotated by magnetic pole dislocation (or the vacuum hemispheres are rotated by magnetic suspension). Vortex polymerization is formed under the action of centripetal force and centrifugal force, the overall flowing direction of gaseous substances pressed on the surface of the hemisphere is changed, the gaseous substances are polymerized to solve the energy problem, internal energy of the gaseous substances is excited through friction collision and directly converted into energy to obtain internal pressure, and the power problem of the aircraft is solved. Front-back driving is provided for the aircraft through internal pressure, and the problem of aircraft acceleration is solved through mutual pushing pressurization between acting force and counter-acting force.

Description

Technical Field

[0001] The aircraft power design scheme belongs to the field of aircraft power design, which is a scheme designed using multiple production capacity working forms. Background Art

[0002] From the previously applied patent "Dynamic Vacuum Hemisphere Theory and Technology", we know that gaseous substances are affected by rotation in a special hemispherical structure to produce centripetal force and centrifugal force. The centripetal force has a polymerization effect, and the centrifugal force has a dispersion effect. In the vacuum hemispherical structure, the centripetal force can lead the gaseous substances to orderly friction and close-range collision energy production movement, while the centrifugal force can intensify the friction and collision of the disordered movement of the gaseous substances through eddy rotation and firmly bind them within the range of vacuum gravity. The two complement each other and need to play a polymerization effect during the rotation of the vacuum hemisphere. From the "Dynamic Vacuum Hemisphere Theory and Technology", we have mastered the application of gaseous substances. Although the earth's atmospheric environment is different from the space environment, it is only different in density relative to the earth's environment. Therefore, the vacuum hemisphere theory technology can also be applied in space. Using relative vacuum to deal with the space environment is the main basis for aircraft power design. Using the advantages of the rotation of the vacuum hemisphere structure to grasp the movement direction of gaseous substances is the core technology of aircraft power design. Using the "Dynamic Vacuum Hemisphere Theory and Technology" to obtain an energy-gathering system is also the core of aircraft design technology. The basis of these technologies needs to be extended from the background of "Dynamic Vacuum Hemisphere Theory and Technology". If the "Dynamic Vacuum Hemisphere Theory and Technology" alone is far from enough to meet the design of the aircraft, we can only learn from the Laval nozzle technology. The Laval nozzle technology cleverly uses large and small tubes to control the pressure shape of the water flow, which is also applicable to gaseous fluids. We only need to change the Laval nozzle into a conical structure plus a spherical structure to perfectly manipulate the movement of gaseous substances. Summary of the invention

[0003] The technology to be solved; because the previously applied patent "Dynamic Vacuum Hemisphere Theory Technology" can only obtain the flow direction of gaseous substances, it has not been applied in the field of aerospace, and cannot aggregate gaseous substances to form a systematic technology to solve the problems of aircraft energy supply, suspension, power engine, speed-up, etc., the present invention discloses a new "Aircraft Power Design Scheme" to add multiple production lines to aggregate gaseous substances to form an internal pressure power circulation system to solve the design requirements of aircraft under the new situation. Technical solution: Design a disc base, ten vacuum hemispheres, configure ten valves and valve cores, configure ten magnetic dislocation devices (or magnetic suspension devices) connected to ten improved Laval nozzles, of which eight vacuum hemispheres are connected to eight improved Laval nozzles and laid flat on the disc base and parallel to the central ball structure, and the nozzles connected to the other two vacuum hemispheres are vertically connected to the spherical structure respectively, and are perpendicular to the disc base. The overall front view is a gyroscope shape. 1. The design of ten pipelines is based on the improvement of the Laval nozzle, in order to make the gaseous substance flow faster and make the friction and collision more intense. 2. Each vacuum hemisphere is designed with a wind blade on its outer wall, the purpose of which is to receive the internal pressure airflow and increase the rotation speed of the vacuum hemisphere. 3. There is a surrounding windshield on the outside of the vacuum hemisphere, the purpose of which is to use the internal pressure airflow to guide the centrifuged gaseous substances to generate vortex flow and form space pressure. 4. The design of the vacuum hemisphere is improved with reference to the syringe, so that the internal connection does not exceed the inner bottom of the hemisphere. The tube is hollow and its function is to flexibly extend and retract to control the vacuum degree. 5. A pair of pipelines are set as the power engine, and a sail cover is designed at the connection between the vacuum hemisphere and the circular base. The sail cover is semicircular, with a small round hole in the middle that can be controlled to close, the purpose of which is to allow the force flow between the action force and the reaction force to be unimpeded, and reduce the damage caused to the aircraft by vibration during acceleration. Beneficial effects: Compared with current aircraft technology, the power system and energy utilization of the present invention completely surpass current aerospace aircraft. (1) Multiple pipeline technologies are used to aggregate gaseous substances to provide energy supply for the aircraft. (2) During the rotation of the vacuum hemisphere, the centripetal force and centrifugal force are fully utilized to form external air pressure, providing sufficient guarantee for the aggregation of gaseous substances to form internal pressure. (3) The simultaneous front and rear driving during flight fully utilizes the relationship between the action force and the reaction force to solve the vibration problem caused by the flight speed increase. (4) Because the power system can directly obtain internal pressure from gaseous substances through pressure without generating high temperature and high pressure, the requirements for materials do not need to be too high. (5) Because the aircraft power design model is gyroscope-shaped, the aircraft's posture is similar to that of a gyroscope during flight, and its flight angle is controlled, which increases the stability of the aircraft. BRIEF DESCRIPTION OF THE DRAWINGS The present invention is further described below in conjunction with the accompanying drawings and embodiments. Figure 1 This is a schematic diagram of the front design of the present invention. Figure 2It is a top view design schematic diagram of the present invention. Figure 3 Schematic diagram of the vacuum hemisphere design. Figure 4 Schematic diagram of nozzle acceleration during aircraft flight. (1) (2) (3) (4) (5) (6) (7) (8) (11) (12) are vacuum hemispheres, (9) are circular bases, (10) are spherical structures, (13) are wind blades, (14) are wind deflectors, and (15) are nozzles. DETAILED DESCRIPTION [Example 1] Connect ten (15) nozzles to the vacuum hemisphere (1)(2)(3)(4)(5)(6)(7)(8)(11)(12), wherein the nozzles connected to the vacuum hemisphere (1)(2)(3)(4)(5)(6)(7)(8) are parallel to and docked with the central (10) spherical structure and fixed flat on the (9) disc base. The two nozzles connected to the vacuum hemisphere (11)(12) are perpendicular to and docked with the (10) spherical structure and perpendicular to the (9) disc base. When observed from the front, Figure 1 Like a gyroscope model. [Example 2] Magnetic dislocation (or magnetic levitation) is used to provide initial power for the vacuum hemisphere (1) (2) (3) (4) (5) (6) (7) (8) (11) (12). Under the action of centrifugal force, the gaseous material generates a vortex flow between the outside of the vacuum hemisphere and the (14) windshield, pushing the wind blades (13) on the outside of the vacuum hemisphere to increase the rotation speed of the hemisphere. Under the action of centripetal force and due to inertia, the vortex pressure generated by the rotation of the gaseous material with the vacuum hemisphere is introduced into ten (15) nozzles and converged into the central (10) spherical structure through the nozzles. [Example 3] When the aircraft is flying, Figure 4 It is learned that on the (9) disc base, the front and rear drive (3) (7) one-way arrows, the front and rear two relative (15) nozzle valves are opened, the front valve has a small opening, and the rear valve has a large opening, and the air pressure is released from the two relative (15) nozzles. Because the rear opening is larger than the front opening, the reaction force obtained is also greater than the front reaction force. Using the backflow force formed by the front and rear reaction forces to speed up the aircraft is a secret technology of action and reaction force.

Claims

1. The aircraft power design scheme solves the problems of energy, suspension, structure, power and speed increase, and its characteristics are Improve the design of the vacuum hemisphere and design wind blades on the outside of the hemisphere to aggregate gaseous matter. Use multiple nozzles to form an energy-gathering system, and use forward and rearward drive to increase the speed of the aircraft.

2. According to claim 1, the vacuum hemisphere design is improved and wind blades are designed on the outside of the hemisphere, characterized in that The dynamic structure is used to change the dynamic mode of the gaseous substance itself, stimulate the internal energy of the substance, and use the internal energy to speed up the vacuum hemisphere with the help of wind blades.

3. The polymerized gaseous substance according to claim 1, characterized in that The centripetal force and centrifugal force are used to generate a vortex space, form a vortex pressure, increase the flow speed of gaseous substances, make disordered gaseous substances form orderly movement, and promote the collision, friction and aggregation of gaseous substances.

4. The energy focusing system formed by using multiple nozzles according to claim 1 is characterized in that A little bit adds up to a lot. Provide a basis for obtaining internal energy to meet energy supply.

5. The method of claim 1, wherein the front and rear drive is used to increase the speed of the aircraft, characterized in that Use the subsequent force of action and reaction to increase speed.

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