TW201600738A - The supercharging channel and method, to increase thrust of the vehicle, machinery that operate in the air - Google Patents

Abstract

This invention is using at least one supercharging channel, set on the vehicle, machinery that operate in the air, in no need fuel, heat or power cases, using the air kinetic energy already existed through the supercharging channel naturally, forming reversible adiabatic compression process and reversible adiabatic expansion process of air itself naturally, therefore increasing thrust of air kinetic energy acting on inner wall of supercharging channel naturally, so increasing thrust of vehicle, machinery that operate in the air, whereby to enhancing the operational efficiency or reduce consumption of energy.

Description

Pressurization channel and method for increasing the thrust of vehicles and implements operating in air

The technical principle of the present invention utilizes the adiabatic index of the gas = the natural characteristic of Cp/Cv , and the gas is governed by the polytropic process relationship P V ^α = constant = nRT natural characteristic law.

The present invention utilizes at least one pressurized passageway disposed on a carrier, a component, a structure or a structure of a machine that operates in the air, allowing the air to flow at an original flow rate without using additional fuel, heat, or power. The kinetic energy naturally flows into and out of the pressurized passage, and the constraint of the cross-sectional area reduction in the pressurized passage and the dynamic pressure of the kinetic energy of the original flow velocity of the air naturally form a reversible adiabatic compression process of the air itself, which is reversible. The thermal expansion process causes the air to naturally increase the absolute pressure, and the natural expansion recovery volume acts on the inner wall of the pressurized passage, so that the original kinetic energy of the air naturally increases the thrust acting on the inner wall of the pressurized passage, so that Vehicles and implements operating in the air increase the thrust to enhance the efficiency of operation in the air and save energy.

The adiabatic index of gas = Cp / Cv natural characteristics, or heat capacity ratio of gas, is commonly used in today's chemical engineering, mechanical engineering, for example: to enhance the chemical pipeline gas transport Speed, increase the steam pressure and speed in the steam engine's pipeline, improve the combustion efficiency of the rocket nozzle and ramjet nozzle to achieve supersonic jet fuel, improve the fuel intake speed, pressure and combustion efficiency of the engine and turbine, and improve the diesel engine's progress. Gas velocity, ignition efficiency, combustion efficiency, aerodynamic efficiency of the aircraft wing, aerodynamic efficiency of the rotating blades of the wind turbine, etc.

The present invention compares the prior patents of the Republic of China and the United States regarding the use of a gas adiabatic index γ (adiabatic index = Cp/Cv , or heat capacity ratio of a gas, the device of the patent case) The method, the method and the effect, and the pressure passage and method and the effect of the invention for increasing the thrust of the vehicle and the machine in the air are obviously different. The invention is searched and compared with the cited patent cases, including: the Republic of China Patent case number, including:

268591 natural wind blower structure

284829 Wind Rotating Device

345277 Improved natural force turbine ventilator

345278 One-piece synchronous structure of natural force turbo extractor

397198 electric exhaust fan

M263410 Modular Wind Power Plant

M437895 Windmill power generation and indoor heat removal function device

I 231840 Windmill for wind power generation

I 233466 Vertical axis low wind speed wind power generation device

I 305243 Combined fan blade for wind power generation and its fan blade

I 431228 ventilation unit

(Source: http://twpat-simple.tipo.gov.tw/tipotwoc/tipotwkm)

US patent case number, including:

588572 Windmill

537494 Windmill

3148848 Wingless supersonic aircraft

3279194 Aerothermodynamic duct and control means therefor

3280565 External expansion ramjet engine

3430446 External burning ramjet engine

3724784 Wing with thrust augmentor

4087196 Apparatus for deriving energy from moving gas streams

4132499 Wind driven energy generating device

4209148 Flying wing

4233815 Methods of supercharging a diesel engine, in supercharged diesel engines, and in supercharging units for diesel engines

4477039 Vented cowl variable geometry inlet for aircraft

4550259 Device for converting wind energy into another form of energy

5058826 Scramjet engine having a low pressure combustion cycle

5083901 Electricity generating wind turbine

5317866 Free-flying tubular vehicle

5380149 Wind turbine cross wind machine

5457346 Windmill accelerator

5553996 Wind power turbine

5852331 Wind turbine booster

6099249 Structure of output section of jet propulsion engine or gas turbine

6352473 Wind jet

6465899 omni-directional, vertical-axis windturbine

6966747 Wind turbine having airfoils for blocking and directing wind and rotors with or without a central gap

6981839 Wind powered turbine in a tunnel

7258302 Aircraft internal wing and design

7329965 aerodynamic-hybrid, vertical-axis windturbine

7573148 Boundary Layer Wind Turbine

8089173 Wind power nozzle with optimized intake length

8178990 Wind power nozzle with limits

(Source: http://patft.uspto.gov/netahtml/PTO/patimg.htm)

Announcement of patents in the United States, including:

US7000398 B2 Ramjet engine combustion chamber and ramjet engine equipped with same

20060275105 A1 Aerodynamic-hybrid vertical-axis wind turbine

20070224029 A1 Blades for a Vertical AxisWindTurbine, and the Vertical AxisWindTurbine

20080061559 A1 Use of Air Internal Energy and Devices

20100181775 A1 Windpower electricity generation system

20100196150 A1 Boundarylayer windturbine with tangential rotor blades

20110107684 A1 POLE MOUNTED ROTATION PLATFORM AND WIND POWER GENERATOR

20110206526 A1 Vertical-axiswindturbinehaving logarithmic curved airfoils

20110037268 A1 Adaptive Control Ducted Compound Wind Turbine

20110210211 A1 DISCRETE CO-FLOW JET (dCFJ) AIRFOIL

20130049373 A1 Vertical wind turbine generator with ventilator

20130334824 A1 Efficient systems and methods for construction and operation of mobile wind power platforms

20130343880 A1 TURBINE END INTAKE STRUCTURE FOR TURBOCHARGER, AND TURBOCHARGER COMPRISING THE SAME

20140030065 A1 Steam Turbine, and Steam Turbine Stationary Blade

(Source: http://appft.uspto.gov/netahtml/PTO/srchnum.html)

In summary, the present invention allows the air outside the pressurized passage to naturally flow into and out of the pressurized passage at the original flow velocity without the need to additionally use fuel, heat, and power, thereby naturally forming the air itself. The reversible adiabatic compression process and the reversible adiabatic expansion process enable the original kinetic energy of the air to naturally increase the thrust force on the inner wall of the pressurized passage, so that the carrier and the machine operating in the air increase the thrust, thereby enhancing Efficiency or energy-saving benefits of operating in air; devices, methods and methods that are different from previous patents using adiabatic index γ (adiabatic index) = Cp/Cv or gas heat capacity ratio Efficacy, with novelty and progress in creation, and value for industrial use.

The origin of the invention is to improve the aerodynamic efficiency of the rotating blades of the wind turbine and the wind turbine, and to use the pressurized passage which reduces the cross-sectional area in the passage, and is arranged on the rotating blades of the wind turbine and the wind ventilator, In the case of additional fuel, heat, and power, the air naturally flows into and out of the pressurized passage at the original natural flow velocity, and the dynamic pressure of the kinetic energy of the original natural flow velocity of the air is pushed and pressurized. The constrained reduction of the cross-sectional area allows the original natural flow velocity of the air to be naturally increased. The thrust acts on the inner wall of the pressurized passage (approximately higher than the natural flow velocity of the air. The kinetic energy flows through the rotating blade and acts naturally on the surface. The thrust is about 25%), so that the rotating blades of the pressurized passage are increased in thrust, so that the rotating blades of the wind turbine and the wind turbine increase the rotational thrust and the torque, so that the wind turbine can increase the efficiency of generating energy. The wind turbine can improve the efficiency of rotary ventilation and save energy.

In the same way, the pressurized passages with reduced cross-sectional area in the passage can be placed on the vehicles and implements that operate in the air, so that the vehicles and implements operating in the air increase the thrust, so that the vehicles operating in the air, The machine improves the efficiency of operation in the air and saves energy.

Technical principles of the present invention, based adiabatic exponent γ using gas (adiabatic index) = Cp / Cv natural characteristics, or said gas ratio of specific heats (heat capacity ratio), and the use of the gas to follow polytropic process (polytropic process) the relationship of P V α ⁼ constant = natural laws characteristic nRT.

The present invention provides a pressurized passage and method for increasing the thrust of a carrier and an instrument operating in the air, comprising: at least one pressurized passage; the pressurized passage having a plate-like passage wall having a slope inclined forwardly The air inlet has an exhaust port inclined obliquely to the rear, and has a polygonal and circular arc-shaped passage structure, and has a structure in which a cross-sectional area in the passage is reduced from an air inlet to an exhaust port; The maximum cross-sectional area of the intake port A _in > the minimum cross-sectional area _{in the} exhaust port A _out ⊥; the maximum cross-sectional area of the intake port of the pressurized passage A _in > the maximum cross-sectional area of the exhaust port A _out ; The maximum cross-sectional area of the exhaust port of the passage A _out ≧ the minimum cross-sectional area A _out内 in the exhaust port; the maximum cross-sectional area A _{in of the} intake port of the pressurized passage and the minimum cross-sectional area A _{out in} the exhaust port ⊥ Ratio 1<A _in /A _out ⊥≦27.435; using at least one pressurized passage to set the original flow rate of the air outside the pressurized passage on the vehicle, the components, structure or structure of the machine that operates in the air Kinetic energy can flow smoothly into and out of the pressurized passage; An outer case of fuel, thermal energy, power, so that the air outside the inner plenum to flow the kinetic energy of the original natural flows of the air intake plenum maximum sectional area A _in, an air flow rate of their original kinetic energy The pushing of the dynamic pressure and the constraint of reducing the cross-sectional area in the pressurized passage naturally form a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and exhausts the pressurized passage. The flow of the mouth; the natural increase of the absolute pressure of the air acts on the inner wall of the pressurized passage, so that the original kinetic energy of the air naturally increases the thrust acting on the inner wall of the pressurized passage, so as to connect the components of the pressurized passage. Increase the thrust of the structure or structure to increase the thrust of the vehicles and implements operating in the air.

And without the need to use additional fuel, heat, power, let the natural inflow into the maximum cross-sectional area A _in the inlet of the pressurized passage A _in the formation of its own reversible adiabatic compression process of the air, the natural outflow of the pressurized passage exhaust The minimum cross-sectional area A _{out in the} mouth is removed from the constraint of the cross-sectional area reduction in the pressurized passage, naturally forming a reversible adiabatic expansion process of the air itself, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, and restores the flow rate. The exhaust port of the pressure passage flows out; the natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the exhaust port of the booster passage, so that the original kinetic energy of the air naturally increases and acts on the exhaust port of the booster passage. The thrust of the inner wall is used to increase the thrust of the components, structures or structures that provide the pressurized passage, so as to increase the thrust of the vehicles and implements operating in the air; thereby enhancing the airborne vehicles and implements in the air. Operational efficiency and energy saving benefits.

In the above, the adiabatic index of the gas =the natural characteristic of Cp/Cv is the ratio of the isothermal heat capacity Cp of the gas to the heat capacity Cv of the gas; that is, the heating experiment of the gas, so that the inside of a container When the gas is raised to a certain temperature, the ratio of the heat capacity Cp added by the gas isostatic state to the heat capacity Cv added by the gas isotropic state, or the heat capacity ratio of the gas, that is, the well-known gas The volume has the natural characteristics of reversible thermal expansion and contraction; the gas has the natural characteristic of adiabatic index, because the degree of freedom of the gas molecular structure is due to the natural characteristic of heat; from the viewpoint of heat and force, the heat capacity of the gas It has reversible characteristics with the pressure of the gas; that is, under constant temperature and constant pressure, when the heat is applied to the gas, the gas expands the volume by absorbing heat energy, and when the heat is removed from the gas, the gas is reduced in volume due to the reduction of heat energy. Conversely, under constant temperature and constant pressure, when the pressure is applied to the gas, the gas compresses the volume due to the pressure increase, and at the same time releases the heat capacity absorbed by the original expansion volume. When the pressure is removed, the gas is pressed. The force is reduced and the expansion volume is recovered, and at the same time, the natural characteristics of the gas which is originally released by the compression volume due to the increase in pressure, and the natural characteristics of the gas adiabatic index γ can also be expressed by a gas compression experiment A. That is, in a constant temperature and constant pressure state, a container having a single opening of the piston causes the piston to push the gas in the container inwardly, thereby compressing the volume of the gas in the container, raising the absolute pressure, and simultaneously the gas And thus releasing the volume of the compressed portion, the heat capacity absorbed during the original expansion volume. If the force of the piston pushing force is large enough and the time is long, the container can be measured to raise the temperature; The force of the piston is removed, and the gas in the container is naturally expanded to recover the volume, and thus naturally absorbs back the part of the heat capacity released by the previously compressed volume, and pushes the piston outwardly by the expansion and recovery volume. Move outward to restore the absolute pressure of the gas. At this time, if the force of the original piston push is large enough and the time is long, the temperature of the container can be measured and thus reduced; That is, the working principle of the condensing compressor and the diesel engine, that is, a gas reversible adiabatic compression process and a reversible adiabatic expansion process; the natural property of the gas adiabatic index γ can also be expressed by another gas compression experiment B; That is, in a constant temperature and constant pressure state, an air inlet has an electric air blower and a passage having a cross-sectional area reduced exhaust port, and the gas flow velocity kinetic energy blown by the electric air blower of the air inlet pushes the gas inflow passage (as in experiment A). The force of the piston pushes the gas in the container inwardly. Due to the pushing of the kinetic energy of the gas flow rate and the reduction of the cross-sectional area of the pressure passage, the gas flowing into the passage thus increases the compression volume, the absolute pressure, and thus the gas. The volume of the compressed part, the heat capacity absorbed by the original expansion volume, and increase the flow rate to the exhaust port of the channel (ie, the Venturi effect phenomenon); then when the gas flows out of the channel exhaust port, the gas is intercepted by the channel The constraint of area reduction (as in Experiment A, then the force of the piston is removed), so the natural expansion recovery volume, the absolute pressure of recovery, the recovery The flow rate, which flows out of the exhaust port of the passage, naturally absorbs back the portion of the heat capacity that was released when the gas was previously compressed (as in Experiment A and absorbed back the portion of the heat capacity released from the previously compressed volume) At the same time, the gas and the outward expansion of the expansion volume of the expansion act on the inner wall of the channel exhaust port (as in Experiment A and the outward expansion force of the expansion recovery volume pushes the piston outward); this is the rocket nozzle, stamping The working principle of the engine is also the working principle of the present invention, that is, another form of gas reversible adiabatic compression process, reversible adiabatic expansion process; it is particularly emphasized that in the compression experiment B of the above gas, the compression volume of the gas The process of expanding the recovery volume is continuous, and the process of releasing and absorbing the heat capacity of the gas is also continuous, and is close to the equilibrium state of canceling each other. Therefore, it is not easy to measure the change of temperature, but the process is as The compression experiment A of the above gas occurred and existed in the same manner.

In the above, the polytropic process relationship P V ^α = constant = nRT is a polytropic process relationship of gas thermodynamics, wherein P is the absolute pressure of the gas, V is the volume of the gas, and α is Multi-relationship index, n is the gas mole number, R is the gas constant, T is the gas absolute temperature; in the ideal gas state, the gas compression and expansion process, the polytropic process relationship P V ^α = constant = nRT to P V = constant = nRT represents, that is, the multi-relationship index α = 1; in the present invention, the real gas state gas reversible adiabatic compression, expansion process, polytropic process relationship P V ^α = constant = nRT to P V ^γ = constant = nRT , that is, the adiabatic index of the multi-party relationship index α = γ gas; the difference is that the relationship between the compression and expansion processes of the ideal gas state gas P and V does not take into account the change of the gas adiabatic index γ. The reason is that in the general case, the lower pressure P or the lower gas natural flow kinetic energy and the relative flow velocity kinetic energy push the gas volume V to change The specific gravity of the body heat capacity Cp is relatively low, so the calculation is not considered for the specific gravity; in the present invention, the reversible adiabatic compression and expansion process of the gas in the real gas state, the relationship between P and V must be considered. The influence of the gas adiabatic index γ is due to the fact that the true gas state includes a lower, higher pressure P or lower, higher gas natural flow kinetic energy, and a relative flow kinetic energy push pressure to cause a reversible change in the volume V of the gas. At the same time, the heat capacity Cp of the gas is reversibly changed, and the reversible change relationship between P and V must therefore consider the specific gravity of the gas adiabatic index γ.

In the above, the gas refers to a single gas and a mixed gas, and the air in the atmospheric environment is a mixed gas.

In the above-mentioned articles, the vehicle and the machine that operate in the air refer to the vehicle, the machine that runs, moves, and rotates in the air, and utilizes the natural kinetic energy of the air, the relative flow kinetic energy, and the space. Vehicles and implements that run, move, and rotate in the air.

In the above, the vehicle includes: a vehicle, a ship, and an aircraft.

In the above, the machine includes: a machine, an appliance, and an appliance.

According to the present invention, the increased thrust includes: an increase in the thrust in the rotational direction, an upward force in the increase action, a downward thrust on the increase, a thrust on the left to the increase, and a lift on the right from the increase. The thrust that acts to the front and the thrust that increases the force to the rear; the increased thrust can be changed by the relative angle between the kinetic energy of the original flow velocity of the air and the maximum cross-sectional area A _in of the intake port of the booster passage. The maximum cross-sectional area of the air inlet of the channel A _in the degree of air circulation, in order to change the level of natural aversion of the self-reversible adiabatic compression, in order to change the natural increase of the original kinetic energy of the air to the pressurized channel The height of the inner wall; and the change of the natural minimum outflow area in the exhaust port A _out ⊥ air, naturally forming the level of reversible adiabatic expansion of the air itself, in order to change the natural kinetic energy of the air to increase naturally The thrust acts on the inner wall of the exhaust port of the booster passage to change the height of the vehicle and implements that operate in the air. High and low degree of force.

According to the above aspect of the present invention, the pressurized passage includes: a pressurized passage formed by a plate-shaped passage wall, a pressurized passage formed by a plate-shaped passage wall and a vehicle operating in the air, and a component of the implement, and a plate The pressurized passage formed by the channel wall and the carrier and the structure of the machine operating in the air, and the pressurized passage formed by the plate-shaped passage wall and the carrier working in the air and the structure of the implement; 1<A _in /A _out ⊥≦27.435, whose 27.435 ratio is calculated from the relation [(γ+1)/2] ^γ/(γ-1) /sin(4°), and the relation γ is The gas adiabatic index, the natural atmosphere of the air is γ ≒ 1.40 at 20 ° C, the relationship sin (4 °) ≒ 0.069, substituted into the relationship to obtain [(γ+1) / 2] ^{γ / (γ -1)} /sin(4°)≒1.893/0.069≒27.435; the relation [(γ+1)/2] ^γ/(γ-1) /sin(4°) can also be written as [2/(γ +1)] ^-γ/(γ-1) /sin(4°); the limit of 1<A _in /A _out ⊥≦27.435, the maximum ratio of 27.435 is the boost to avoid excessive reduction of air flow through the cross-sectional area Channel, beyond the volumetric compressibility of the air to form a blocking effect of air Causing air to bypass the flow of the pressurized passage to reduce the flow of air flowing through the pressurized passage, so that the air can flow through the pressurized passage at a higher flow rate, so that the kinetic energy of the air flow can increase the thrust force The inner wall of the pressurized passage.

In the above, the original kinetic energy of the air includes: the original natural flow velocity kinetic energy of the air and the original relative flow velocity kinetic energy of the air.

In the above-mentioned invention, the natural formation of the air itself is reversible adiabatic compression process, so that the natural compression volume of the air, the increase of the absolute pressure, the increase of the flow rate, and the flow to the exhaust port of the pressurized passage means the natural flow into the pressurized passage. The air in the maximum cross-sectional area A _in the air port is restrained by the dynamic pressure of the original kinetic energy of the air and the reduction of the cross-sectional area in the pressurized passage. Therefore, the adiabatic index of the gas is followed. Cp/Cv natural characteristics, and polytropic process relationship P V ^γ = constant = nRT natural characteristic law, the natural formation of air itself reversible adiabatic compression process, so that the air inside the pressurized channel is therefore a natural compression volume temporarily The release of the air's own isobaric heat capacity, and therefore naturally temporarily increase the absolute pressure, increase the flow rate, and flow to the exhaust passage exhaust port.

In the above-mentioned invention, the natural formation of the air itself is reversible adiabatic expansion process, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and flows out of the exhaust port of the pressurized passage, which means that the exhaust passage is exhausted. The air with the smallest cross-sectional area A _out口 in the mouth is constrained by the reduction of the cross-sectional area in the pressurized passage, so the adiabatic index of the gas is calculated = the natural characteristics of Cp/Cv , and the polytropic process The relationship P V ^γ = constant = nRT natural characteristic law, the natural formation of the air itself reversible adiabatic expansion process, so that the natural outflow of the minimum cross-sectional area in the exhaust passage of the pressure passage A _out ⊥ the air, so the natural absorption The air returns to its own isobaric heat capacity to expand the recovery volume, and thus naturally restores the absolute pressure, the return flow rate, and flows out of the pressurized passage exhaust port.

In the above, the vehicle and the machine that operate in the air are improved in the efficiency of operation in the air, and the energy-saving effect refers to the improvement of the vehicle and the machine for running, moving and rotating in the air. The efficiency of operation, movement and rotation, and the benefits of energy conservation.

In summary, the present invention makes the pressurized passage and method for increasing the thrust of the vehicle and the machine in operation in the air, and is simple and practical, and can be widely used on vehicles and implements that operate in the air without using additional fuel. In the case of heat energy and power, let the air flow naturally through the pressure passage at the original flow velocity, naturally forming a reversible adiabatic compression process and a reversible adiabatic expansion process of the air, thus making the original flow velocity of the air naturally The increased thrust acts on the inner wall of the pressurized passage, which can increase the thrust of the vehicles and implements operating in the air, thereby enhancing the efficiency of the operation of the air or the energy saving effect of the vehicles and implements operating in the air. It has the novelty, progress, and value for the use of the industry, and the patent application of the invention is filed according to the Patent Law of the Republic of China.

10‧‧‧Train channel

11‧‧‧air inlet

12‧‧‧Exhaust port

13‧‧‧ plate-shaped channel wall

14‧‧‧Maximum cross-sectional area of the air inlet A _in

15‧‧‧Minimum cross-sectional area in the exhaust port A _out ⊥

16‧‧‧Maximum cross-sectional area of the exhaust port A _out

17‧‧‧The natural kinetic energy and relative flow kinetic energy of the air

18‧‧‧Formation of a reversible adiabatic compression process of air

19‧‧‧Forming a reversible adiabatic expansion process of air

20‧‧‧High thrust

21‧‧‧Air natural flow velocity kinetic energy, relative flow kinetic energy flow angle and pressure channel A _in

22‧‧‧Cylindrical channel wall assembly

23‧‧‧Disc shaped channel wall assembly

24‧‧‧Rotation direction

25‧‧‧Wing wheel type electric ventilator

26‧‧‧Wing-wheel electric ventilator with pressurized passage

27‧‧‧Top cover parts

28‧‧‧Fan-blade electric ventilator

29‧‧‧Fan-blade electric ventilator with pressurized passage

30‧‧‧ wind ventilator

31‧‧‧ curved curved blades

32‧‧‧Wind ventilator with pressurized passage

33‧‧‧ wall-mounted electric ventilator

34‧‧‧Cylindrical parts

35‧‧‧Wall-mounted electric ventilator with pressurized passage

36‧‧‧Horizontal axis wind turbines

37‧‧‧Rotating blades

38‧‧‧Horizontal shaft wind turbine with pressurized passage

39‧‧‧Vertical shaft wind turbine

40‧‧‧Horizontal shaft wind turbine with pressurized passage

41‧‧‧Ship

42‧‧‧A ship with a pressurized passage

43‧‧‧ hovercraft

44‧‧‧Hovering hovercraft with pressurized passage

45‧‧‧Kite

46‧‧‧Set the kite for the pressurized channel

47‧‧‧Parachute

48‧‧‧Set the parachute of the pressurized channel

49‧‧‧Parachute structure

50‧‧‧Rocket

51‧‧‧Set rocket for pressurized passage

52‧‧‧ Structure

53‧‧‧Split aircraft

54‧‧‧Split aircraft with pressurized passage

55‧‧‧Unpowered glider

56‧‧‧Unpowered glider with pressurized passage

57‧‧‧Aircraft

58‧‧‧Aircraft with pressurized passage

59‧‧‧propeller

60‧‧‧Set the propeller of the pressurized passage

61‧‧‧propeller blades

62‧‧‧ helicopter

63‧‧‧Helicopter with pressurized passage

64‧‧‧ trucks

65‧‧‧Setting truck with pressurized passage

66‧‧" bus

67‧‧‧Set the bus for the booster channel

68‧‧‧Travel Car

69‧‧‧Travel car with pressurized passage

70‧‧‧Sedan

71‧‧‧Set the car with pressurized passage

The first picture represents the map

The second picture is a perspective view of the pressurized channel.

The third picture is the perspective of the pressurized passage, sectional view 2

The fourth picture is a perspective view of the pressurized passage, and a sectional view III.

Figure 5: Perspective, section 4 of the pressurized passage

Figure 6: Perspective and section view of the pressurized passage

Figure 7 Schematic diagram of the plate-shaped channel wall

Eighth embodiment

The ninth figure

Figure 10 Embodiment 3

Eleventh embodiment

Twelfth figure, the fifth embodiment

Thirteenth embodiment

Fourteenth embodiment

Fifteenth embodiment

Figure 16 Embodiment 9

Figure 17 Embodiment 10

Eighteenth embodiment

Nineteenth embodiment

Figure 20 Embodiment 13

Twenty-first figure embodiment fourteen

Twenty-second figure

Twenty-third figure embodiment sixteen

Twenty-fourth embodiment

Twenty-fifth figure

Twenty-sixth embodiment

Twenty-seventh embodiment

Twenty-eighth embodiment

Twenty-ninth figure embodiment twenty two

Thirtieth Embodiment Example Twenty-three

As shown in the first figure, a 10-pressure passage has an 11-way inlet that slopes forwardly and has a 12-venting opening that slopes rearwardly and has a plate-like passage wall having a polygonal or circular shape. Channel structure.

As shown in the second to fifth figures, the 10 pressure passage has a structure in which the cross-sectional area in the passage is reduced from the intake port to the exhaust port, and the maximum cross-sectional area of the inlet port of the 10 boost passage is A _in >15 exhaust port. The minimum cross-sectional area within the A _out ⊥; 10 the maximum cross-sectional area of the 14 inlets of the booster channel A _in >16 The maximum cross-sectional area of the exhaust port A _out ; 10 The maximum cross-sectional area of the 16 exhaust ports of the booster channel A _Out ≧15 The minimum cross-sectional area A _out ⊥ in the exhaust port.

As shown in the second to sixth figures, the air outside the pressure passage is kinetic energy and relative flow velocity kinetic energy of the original air flow rate of 17 air without additional use of fuel, heat, and power, and naturally flows into the 10 pressure passage 14 The maximum cross-sectional area of the air inlet is within A _in , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural inflow 10 pressure passage 14 The maximum cross-sectional area of the air inlet A _in the air, the natural 18 forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage. The natural pressure of the air is used to increase the absolute pressure on the inner wall of the 10 pressure passage. Therefore, the natural flow rate of the 17 air and the relative flow velocity kinetic energy are naturally increased by 20 to the thrust of the inner wall of the 10 pressure passage, so that 10 plenum increased thrust; the case and without additional fuel, energy, power, so that naturally flows into the plenum 10 of the intake port 14 the maximum cross-sectional area a _in, 18 to form an air itself Inverse air adiabatic compression process, the natural outflow of the minimum cross-sectional area A inside the exhaust port 10 pressurizing passage 15 _out ⊥, so that the air from the natural constraints cross-sectional area of the reduced pressure intensification passage 10, so that the natural outflow 10 The minimum cross-sectional area of the exhaust passage 15 in the exhaust port A _out ⊥ the air, the natural 19 forms a reversible adiabatic expansion process of the air itself, so that the air thus naturally expands the volume, restores the absolute pressure, restores the flow rate, and is pressurized by the passage The exhaust port flows out, and the natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the 12 exhaust port. Therefore, the natural flow rate of the 17 air and the relative flow velocity kinetic energy are naturally increased by 20 to the 10 pressure passage 12 The thrust of the inner wall of the exhaust port is such that the 10 booster passage increases the thrust.

As shown in the second to sixth figures, the natural flow velocity kinetic energy of the change 21 air, the relative flow velocity kinetic energy flow angle with the pressure increase channel A _in is used to change the natural flow rate of the 17 air, and the relative flow velocity of the kinetic energy of the natural inflow 10 pressure passage 14 The maximum cross-sectional area of the air inlet A _{in the} amount of flow, in order to change the level of the self-reversible adiabatic compression process, the reversible adiabatic expansion process, to change the air flow kinetic energy 20 increase the thrust on the inner wall of the 10 pressure passage The degree of high and low, and change the air flow kinetic energy 20 to increase the height of the thrust on the inner wall of the 10 pressure passage exhaust port.

As shown in the seventh figure, the passage wall of the 10 pressure passage has different shapes, 13 plate-shaped passage walls, 22 cylindrical passage wall assemblies composed of a plurality of plate-like passage walls, and 23 circles composed of a plurality of plate-like passage walls. Disc channel wall assembly.

As shown in the eighth figure, the 25-wing wheel type electric ventilator uses a plurality of 13-plate-shaped passage walls and 22 cylindrical-shaped passage wall assemblies, and the upper cover member of the 25-wing type electric ventilator is turned over by 90°. A plurality of 10 pressurized passages constitute a 26-wing electric ventilator with a pressurized passage; as shown in the second figure, the air outside the pressurized passage is 17 air without additional use of fuel, heat, and power. The original natural flow velocity kinetic energy, the relative flow kinetic energy, the natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy and 10 The restriction of the cross-sectional area in the pressurized passage is such that the natural inflow of air into the maximum cross-sectional area A _in the inlet of the 10-pressure passage 14 naturally forms a reversible adiabatic compression process of the air, thereby making the air natural. The compression volume, the increase of the absolute pressure, the increase of the flow rate, the flow to the exhaust port of the pressurized passage, the natural increase of the absolute pressure of the air acts on the inner wall of the 10 pressurized passage, thus the natural flow rate and relative flow of the 17 air. The natural acceleration of the quick-acting energy acts on the thrust of the inner wall of the 10-pressure passage to increase the thrust of the 10-pressure passage; and allows the natural flow into the 10-pressure passage without additional use of fuel, heat, and power. 14 The maximum cross-sectional area of the air inlet A _in , 18 forms the air of the air itself reversible adiabatic compression process, the natural outflow 10 pressure channel 15 the smallest cross-sectional area in the exhaust port A _out ⊥, let the air naturally detach 10 The restriction of the cross-sectional area in the pressurized passage is such that the natural outflow 10 of the exhaust passage 15 has the smallest cross-sectional area A _out ⊥ of the air, and the natural 19 forms a reversible adiabatic expansion process of the air itself, so that the air is naturally The expansion recovery volume, the return absolute pressure, the recovery flow rate, and the exhaust port of the pressurized passage flow out, and the natural expansion of the air is used to recover the volume and expand outward to act on the inner wall of the 12 exhaust port, thus making the 17 air original natural The natural flow 20 of the flow rate and relative flow kinetic energy acts on the thrust of the inner wall of the exhaust port of the 10 booster passage 12, so that the thrust of the 10 booster passage is increased to the thrust in the direction of 24 rotation, so that the pressurization of 26 is set. Wings fan wheel channel power 24 increases the rotational direction of thrust effect, so that the wings 26 disposed plenum fan wheel power both power operation of the wind function, to enhance efficiency of energy conservation.

As shown in the ninth figure, the 28-blade power ventilator uses a plurality of 13-plate-shaped passage walls and 22 cylindrical channel wall assemblies, and the upper cover member of the 28-blade electric ventilator is turned over by 90°. 10 supercharged passages, forming a fan-blade electric ventilator with a pressurized passage; as shown in the second figure, the air outside the plenum passage is 17 air originals without additional use of fuel, heat, and power. Some natural flow kinetic energy, relative flow kinetic energy, natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy and 10 increase The restriction of the cross-sectional area reduction in the pressure passage causes the natural air to flow into the maximum cross-sectional area A _in the inlet of the 10-pressure passage 14 , and the natural 18 forms a reversible adiabatic compression process of the air, so that the air is naturally compressed. Volume, increase absolute pressure, increase flow rate, flow to the exhaust port of the pressurized passage, and use the natural increase of the absolute pressure of the air to act on the inner wall of the 10 pressurized passage, thus making the original natural flow velocity and relative flow rate of the 17 air The natural 20 increase acts on the thrust of the inner wall of the 10 booster passage to increase the thrust of the 10 booster passage; and allows the natural flow into the 10 booster passage 14 without the need for additional fuel, heat, or power. The maximum cross-sectional area of the air inlet A _in , 18 forms the air of the air itself reversible adiabatic compression process, the natural outflow 10 the minimum cross-sectional area A _out排气 in the exhaust port 15 of the pressurized passage 15 allows the natural departure of the air 10 constraint in the cross-sectional area of the reduced pressure passage, so that the natural outflow of air within the minimum cross-sectional area a of the exhaust port 10 pressurizing passage 15 _out ⊥, natural air 19 itself is formed adiabatic expansion reversible, so that the natural air The expansion recovery volume, the return absolute pressure, and the recovery flow rate are discharged from the exhaust port of the pressurized passage, and the natural expansion of the air is used to recover the volume and expand outward to act on the inner wall of the 12 exhaust port, thereby making the original natural flow rate of the 17 air. The relative flow velocity kinetic energy natural 20 increase acts on the inner wall of the 10 plenum 12 exhaust port thrust, so that the 10 booster passage increases the thrust to the 24 rotation direction, so that 29 sets the boost channel Fan blade type power increases the effect of the thrust rotational direction 24, so that the blade-type fan 29 disposed plenum power of both power operation of the wind function and enhance efficiency of energy conservation.

As shown in the tenth figure, the 30 wind ventilator uses a set of 22 cylindrical channel wall members and 23 disc-shaped channel wall assemblies, and a plurality of 31 curved arc-shaped rotating blades of 30 wind ventilators, forming a plurality of inverted 90° 10 pressurized passages, forming 32 wind turbines with pressurized passages; as shown in the second figure, the natural air flow rate of the air outside the pressure passage is 17 air without additional use of fuel, heat, and power. Kinetic energy, relative flow kinetic energy, natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the 10 pressure channel The confinement of the cross-sectional area is reduced, so that the natural inflow of air into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 naturally forms a reversible adiabatic compression process of the air itself, so that the air thus naturally compresses the volume and increases the absolute Pressure, increase the flow rate, flow to the exhaust port of the pressurized passage, and use the natural increase of the absolute pressure of the air to act on the inner wall of the 10 pressurized passage, thus making the natural flow rate and relative flow velocity of the 17 air naturally The increase of 20 acts on the thrust of the inner wall of the 10 booster passage to increase the thrust of the 10 booster passage; and allows the natural inflow of 10 booster passages 14 without additional use of fuel, heat, and power. The maximum cross-sectional area of the mouth is A _in , 18 forms the air of the air itself reversible adiabatic compression process, the natural outflow 10 the minimum cross-sectional area A _out排气 in the exhaust port of the pressurized passage 15 allows the air to naturally escape 10 the pressurized passage The inner cross-sectional area is reduced by the constraint, so that the natural outflow 10 is the minimum cross-sectional area of the exhaust passage 15 in the exhaust port A _out ⊥ the air, the natural 19 forms the reversible adiabatic expansion process of the air itself, so that the air thus naturally expands and recovers Volume, return absolute pressure, return flow rate, flow out from the exhaust port of the pressurized passage, and use the natural expansion of the air to recover the volume and expand outward to act on the inner wall of the 12 exhaust port, thus making the natural flow rate of the 17 air, relative The natural 20 increase in flow kinetic energy acts on the thrust of the inner wall of the exhaust port of the 10 booster passage 12, so that the thrust of the 10 booster passage is increased in the direction of rotation of 24, so that the arc of the set pressure passage is curved. Rotary blade 24 to increase the thrust acting in the direction of rotation, the fan 32 is provided to boost the wind passage increased the thrust, torque, to enhance the operation efficiency, energy saving benefits.

As shown in the eleventh figure, the 33 wall-mounted electric ventilator uses a plurality of 13-plate channel walls and 34 cylindrical components of a 33-hung electric ventilator to form a plurality of 10 plenums that are turned over 90°. Forming a wall-mounted electric ventilator with a pressurized passageway; as shown in the second figure, the air outside the plenum passage is kinetic energy at the natural flow rate of 17 air without additional use of fuel, heat, and power. The relative flow velocity kinetic energy naturally flows into the maximum cross-sectional area A _in of the inlet port of the 10 boosting passage 14 , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the cross-sectional area of the 10 pressurized passage. The reduced constraint causes the natural inflow of air into the maximum cross-sectional area A _in of the inlet port of the 10 booster passage 14, and the natural 18 forms a reversible adiabatic compression process of the air itself, so that the air thus has a natural compression volume, an increase in absolute pressure, Increase the flow rate, flow to the exhaust port of the booster passage, and use the natural increase of the absolute pressure of the air to act on the inner wall of the 10 pressurization passage. Therefore, the natural flow rate and the relative flow velocity of the 17 air are naturally increased by 20 10 thrust of the inner wall of the pressurized passage to increase the thrust of the 10 booster passage; and let the natural inflow into the maximum cross-sectional area of the intake port of the 10 booster passage 14 without additional use of fuel, heat, and power. In A _in , 18 forms the air of the air's own reversible adiabatic compression process, and the natural outflow 10 is the minimum cross-sectional area A _out排气 in the exhaust port of the booster passage 15 to allow the natural escape of the air. The cross-sectional area in the pressurized passage is reduced. The constraint is such that the natural outflow 10 is the smallest cross-sectional area in the exhaust port 15 of the exhaust passage A _out of the air, the natural 19 forms a reversible adiabatic expansion process of the air itself, so that the air thus naturally expands the volume, restores the absolute pressure The return flow rate is flowed out from the exhaust port of the pressurized passage, and the natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the 12 exhaust port, so that the original natural flow velocity and relative flow velocity of the 17 air are natural. Increasing the thrust acting on the inner wall of the exhaust port of the 10 booster passage 12, so that the thrust passage of the 10 booster passage is increased in the direction of rotation of 24, so that the wall-mounted electric ventilator with the boost passage is increased by 25 The high-force thrust to the direction of rotation of 24 makes the wall-mounted electric ventilator with 25 booster passages have the functions of electric power and wind operation to enhance the energy-saving benefits.

As shown in Fig. 12, a 36-horizontal-axis wind turbine is constructed by providing a plurality of 13-plate-shaped passage walls and a plurality of 37-rotating blades of 36 horizontal-axis wind turbines to form a plurality of 10-pressure passages, forming 38 to set a pressurized passage. The horizontal axis wind turbine; as shown in the third figure, the air outside the pressure passage is kinetic energy, the relative flow velocity kinetic energy, and the natural inflow of the air outside the pressure passage without additional use of fuel, heat, and power. 10 The maximum cross-sectional area of the intake port of the booster passage 14 is within A _in , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the constraint of the cross-sectional area reduction within 10 the pressurized passage, making the natural The air flowing into the maximum cross-sectional area A _in of the inlet of the 10 pressure passage 14 naturally forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and presses the pressure passage. The exhaust port flows, and the natural absolute increase of the air acts on the inner wall of the 10 pressurized passage, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase by 20 0 Thrust of the inner wall of the pressurized passage to increase the thrust of the 10 booster passage; and allow the natural maximum flow into the inlet of the 10 booster passage 14 without additional use of fuel, heat, or power. In A _in , 18 forms the air of the air's own reversible adiabatic compression process, and the natural outflow 10 is the minimum cross-sectional area A _out排气 in the exhaust port of the booster passage 15 to allow the natural escape of the air. The cross-sectional area in the pressurized passage is reduced. The constraint is such that the natural outflow 10 is the smallest cross-sectional area in the exhaust port 15 of the exhaust passage A _out of the air, the natural 19 forms a reversible adiabatic expansion process of the air itself, so that the air thus naturally expands the volume, restores the absolute pressure The return flow rate is flowed out from the exhaust port of the pressurized passage, and the natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the 12 exhaust port, so that the original natural flow velocity and relative flow velocity of the 17 air are natural. Increasing the thrust acting on the inner wall of the exhaust port of the 10 booster passage 12, so that the thrust passage of the 10 booster passage is increased in the direction of rotation of 24, so that the 37-turn rotary vane of the pressurized passage is increased to 24 Thrust and torsion in the direction of rotation, so that the horizontal axis wind turbine with 38 pressure passages can improve the efficiency of operation and save energy.

As shown in the thirteenth, 39 vertical-axis wind turbines, using a plurality of 13-plate channel walls and 22 cylindrical channel wall assemblies and 39 vertical-axis wind turbines, a plurality of 37 rotating blades constitute a multi-turn 90° 10 supercharged passages, forming 40 horizontal axis wind turbines with pressurized passages; as shown in the second figure, the air outside the pressurized passages is 17 air without additional use of fuel, heat, and power. Natural flow velocity kinetic energy, relative flow kinetic energy, natural inflow into the maximum cross-sectional area A _in the inlet of the 10 booster passage 14 , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and 10 supercharging The restriction of the cross-sectional area in the channel is reduced, so that the natural inflow of air into the maximum cross-sectional area A _in the inlet of the 10-pressure passage 14 naturally forms a reversible adiabatic compression process of the air, so that the air thus has a natural compression volume. Increase the absolute pressure, increase the flow rate, flow to the exhaust port of the pressurized passage, and use the natural increase of the absolute pressure of the air to act on the inner wall of the 10 pressurized passage, thus making the original natural flow rate and phase of the 17 air The natural 20 increase in flow kinetic energy acts on the thrust of the inner wall of the 10 booster passage to increase the thrust of the 10 booster passage; and allows the natural inflow 10 to be boosted without the need for additional fuel, heat, and power. The maximum cross-sectional area A _{in the} inlet of the passage 14 is 18, and the air forming the reversible adiabatic compression process of the air itself, the natural outflow 10, the minimum cross-sectional area A _out排气 in the exhaust port of the pressurized passage 15 allows the air to naturally detach 10 The cross-sectional area in the pressurized passage is reduced by the constraint, so that the natural outflow 10 is the minimum cross-sectional area in the exhaust port of the pressurized passage 15 A _out of the air, the natural 19 forms a reversible adiabatic expansion process of the air itself, so that the air The natural expansion recovery volume, the return absolute pressure, and the recovery flow rate are discharged from the exhaust port of the pressurized passage, and the natural expansion of the air is used to recover the volume and expand outward to act on the inner wall of the 12 exhaust port, thus making the 17 air original. The natural flow rate and the relative flow velocity kinetic energy naturally increase by 20 to the thrust of the inner wall of the exhaust port of the 10 booster passage 12, so that the 10 booster passage increases the thrust to the direction of 24 rotation, so that the setting is increased. Rotary blade 37 to the passage 24 increases the rotational direction of action of the thrust, torque, so that horizontal axis wind turbine provided with a pressurizing channel 40 increase efficiency of operation, energy saving benefits.

As shown in Figure 14, the ship 41 uses a plurality of 13-plate-shaped passage walls, and the structure of the left and right side hulls of the 41 ships constitutes 10 pressurized passages on the left and right sides, forming a ship with 42 pressurized passages; In the three maps, the air outside the pressure passage is kinetic energy and relative flow kinetic energy of the original air flow rate of 17 air without additional use of fuel, heat and power, and naturally flows into the inlet of the 10 pressure passage 14 The maximum cross-sectional area A _in is constrained by the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural inflow 10 is pressurized. The air with the largest cross-sectional area A _in , the natural 18 forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, flows to the exhaust port of the pressurized passage, and utilizes the air naturally. The increase of the absolute pressure acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate increase by 20 to the thrust of the inner wall of the 10 pressure passage, so that 10 is supercharged. Road increased thrust; the case and without additional fuel, energy, power, so that naturally flows into the plenum 10 of the intake port 14 the maximum cross-sectional area A _in, 18 forming the air itself reversible adiabatic compression process air , the natural outflow 10 pressure passage 15 the minimum cross-sectional area in the exhaust port A _out ⊥, let the air naturally detach from the 10 cross-sectional area of the pressurized passage to reduce the constraint, so that the natural outflow 10 pressurized passage 15 exhaust The inner air with the smallest cross-sectional area A _out ,, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and flows out of the exhaust port of the pressurized passage. The natural expansion and recovery volume of the air expands outwardly on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase 20 on the inner wall of the exhaust port of the 10 pressure passage 12 Thrust, so that the 10 booster passage increases the upward thrust, so that the ship with 42 booster passages increases the lift force to improve the efficiency of the ship on the water and save energy. .

As shown in the fifteenth figure, the 43 hovercraft uses a plurality of 13-plate-shaped passage walls, and the hull structure on the left and right sides of the 43 hovercraft constitutes a 10-pressure passage on the left and right sides, forming a hovercraft with a pressurized passage; In the three maps, the air outside the pressure passage is kinetic energy and relative flow kinetic energy of the original air flow rate of 17 air without additional use of fuel, heat and power, and naturally flows into the inlet of the 10 pressure passage 14 The maximum cross-sectional area A _in is constrained by the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural inflow 10 is pressurized. The air with the largest cross-sectional area A _in , the natural 18 forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, flows to the exhaust port of the pressurized passage, and utilizes the air naturally. The increase of the absolute pressure acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase by 20 on the inner wall of the 10 pressure passage, so that 1 0 The booster channel increases the thrust; and allows the natural inflow into the maximum cross-sectional area A _in the inlet of the 10 booster passage 14 without the need for additional fuel, heat, and power, 18 forming a reversible adiabatic compression of the air itself. The process of the air, the natural outflow 10 of the pressurized passage 15 the minimum cross-sectional area within the exhaust port A _out ⊥, allowing the air to naturally detach from the 10 cross-sectional area of the pressurized passage to reduce the constraint, so that the natural outflow 10 pressurized passage 15 The air with the smallest cross-sectional area A _{out in the} exhaust port, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and the exhaust port of the pressurized passage Outflow, using the natural expansion of the air to recover the volume and expand outward to act on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase 20 to the exhaust port of the 10 booster passage 12 The thrust of the inner wall is such that the 10 booster passage increases the upward thrust, so that the hovercraft with the boost passage is increased by 44 to improve the efficiency and economy of running on the water or on land. The benefits of energy.

As shown in the sixteenth figure, the 45 kite uses a 13-plate-shaped passage wall and a structure below the 45 kite to form a 10-pressure passage to form 46 a kite with a pressurized passage; as shown in the fifth figure, no additional fuel is needed. In the case of heat energy and power, let the air outside the pressure passage be kinetic energy and relative flow velocity of the original natural flow velocity of 17 air, and naturally flow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 to 17 The original natural flow velocity of the air, the pushing pressure of the relative flow velocity kinetic energy, and the restriction of the cross-sectional area reduction in the 10 pressure passages allow the natural inflow of air into the maximum cross-sectional area A _in of the intake port of the 10 pressure passage 14 Natural 18 forms the reversible adiabatic compression process of the air, so that the air naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage. The natural pressure is increased by the absolute pressure of the air. The inner wall of the channel, so that the natural flow rate of the 17 air, the natural kinetic energy of the relative flow velocity is increased by 20, which acts on the inner wall of the 10 pressure passage to increase the thrust of the 10 pressure passage; In the case where the fuel used, heat, power, so that naturally flows into the plenum 10 within intake port 14 the maximum cross-sectional area A _in, 18 to form an air own air reversible adiabatic compression process, the natural outflow plenum 10 15 The minimum cross-sectional area A _out内 in the exhaust port allows the air to naturally escape from the constraint of reducing the cross-sectional area in the 10 pressurized passage, so that the natural outflow 10 is the smallest cross-sectional area in the exhaust port of the boost passage 15 A _out ⊥ The air, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and recovers the volume outward by the natural expansion of the air. The expansion acts on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy are naturally increased by 20 to the thrust of the inner wall of the exhaust port of the 10 pressure passage 12, so that the 10 pressure passage is provided. Increase the upward thrust to increase the climb and lift force of the kite with the booster passage to increase the climbing efficiency and the lifting efficiency in the air.

As shown in the seventeenth figure, the 47 parachute uses a plurality of 13-plate-shaped passage walls, and the structure of the 49 parachute constitutes a 10-pressure passage to form a parachute with 48 a pressurized passage; as shown in the first figure, no additional In the case of using fuel, heat, and power, let the air outside the pressure passage be kinetic energy and relative flow velocity of the original natural flow velocity of 17 air, and naturally flow into the maximum cross-sectional area A _in of the intake port of the 10 pressure passage 14 . With the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the constraint of the cross-sectional area reduction in the 10 pressure passage, the natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 The air, the natural 18 forms the reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage, using the natural increase of the absolute pressure of the air to act on the 10 The inner wall of the pressurized passage, so that the natural flow rate of the 17 air, the natural kinetic energy of the relative flow velocity is increased by 20, which acts on the inner wall of the 10 pressure passage to increase the thrust of the 10 pressure passage. And the case without additional fuel, energy, power, so that naturally flows into the plenum 10 of the intake port 14 the maximum cross-sectional area A _in, 18 to form an air own air reversible adiabatic compression process, the natural outflow 10 The minimum cross-sectional area A _out内 in the exhaust port of the booster passage 15 allows the air to naturally escape from the constraint of reducing the cross-sectional area in the 10 booster passage, so that the natural outflow 10 is the smallest cut in the exhaust port of the boost passage 15 The air of the area A _out , the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and utilizes the natural expansion of the air. The outward expansion of the recovery volume acts on the inner wall of the 12 exhaust port, so that the natural natural flow velocity of the 17 air and the natural kinetic energy of the relative flow velocity are increased by 20 to the thrust of the inner wall of the exhaust port of the 10 pressurized passage 12, so that 10 The booster passage increases the upward thrust, so that the parachute with 48 booster passages increases the climb and lift force to improve the climbing efficiency and the lifting efficiency in the air.

For example, in the eighteenth and nineteenth, the 50 rockets are provided with a plurality of 13-plate-shaped passage walls, and the 50-frame 52 structure constitutes a 10-pressure passage to form a rocket with a pressurized passage; 51, as shown in the third figure. In the case of no need to use additional fuel, heat, power, let the air outside the pressurized passage have the natural flow velocity of 17 air, the relative flow kinetic energy, and the maximum cross-sectional area of the inlet of the 10 pressurized passage 14 naturally flowing into the air. In A _in , the natural flow rate of 17 air, the pushing pressure of the kinetic energy of the relative flow velocity, and the reduction of the cross-sectional area in the 10 pressure passages make the natural inflow into the maximum of the intake port of the 10 pressure passage 14 The air _{in the} area A _in , the natural 18 forms the reversible adiabatic compression process of the air itself, so that the natural compression volume of the air, the increase of the absolute pressure, the increase of the flow rate, the flow to the exhaust port of the pressurized passage, the natural increase of the air is absolutely The pressure acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate increase by 20, which acts on the inner wall of the 10 pressure passage to increase the thrust of the 10 pressure passage. And without the need to additionally use fuel, heat, power, let the natural flow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 18, forming the air of the air itself reversible adiabatic compression process, natural Outflow 10 The minimum cross-sectional area A _out内 in the exhaust port of the booster passage 15 allows the air to naturally escape from the constraint of reducing the cross-sectional area in the 10 booster passage, so that the natural outflow 10 is the smallest in the exhaust port of the boost passage 15 The air with a cross-sectional area A _out ,, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and utilizes the natural air. The expansion recovery volume is outwardly expanded to act on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase by 20 to the thrust of the inner wall of the exhaust port of the 10 pressure passage 12, Increase the pressure of the 10 booster passage to the upper direction, so that the rocket with the booster passage is set to increase the climb and lift force to enhance the climb and lift efficiency of the flight in the air to enhance the flight. Voyage, energy conservation benefits.

As shown in the twenty-fifth figure, the 53-drop aircraft uses a plurality of 13-plate channel walls to form a 10-pressure passage with the 52 structure of the 53-drop aircraft to form 54 a drop-off aircraft with a pressurized passage. As shown in the third figure, in the case of no need to use additional fuel, heat, power, let the air outside the pressurized passage with the natural flow velocity of 17 air, the relative flow kinetic energy, the natural flow into the 10 pressure passage 14 into The maximum cross-sectional area of the air port A _in , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural inflow 10 pressure passage 14 The air in the maximum cross-sectional area of the air inlet A _in the natural air 18 forms a reversible adiabatic compression process of the air, so that the air naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage. Using the natural increase of the absolute pressure of the air on the inner wall of the 10 pressure passage, the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate are increased by 20 to the thrust of the inner wall of the 10 pressure passage, so that 10 The pressurized passage increases the thrust; and allows the natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 without the need for additional fuel, heat, and power, 18 forming a reversible adiabatic compression process of the air itself. The air, the natural outflow 10 pressure passage 15 the smallest cross-sectional area within the exhaust port A _out ⊥, let the air naturally detach from the 10 cross-sectional area within the pressurized passage to reduce the constraint, so that the natural outflow 10 boost channel 15 rows The air with the smallest cross-sectional area A _out in the air port, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and flows out of the exhaust port of the pressurized passage. The natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the 12 exhaust port. Therefore, the natural flow rate of the 17 air and the relative flow velocity kinetic energy are naturally increased by 20 in the exhaust port of the 10 pressure passage 12 The thrust of the wall, so that the 10 booster passages increase the upward thrust, so that the 54 drop-type aircraft with the booster passage increases the climb and lift to enhance the airborne flight. Climb, buoyant efficiency, to enhance the flight range, energy-saving benefits.

Figure 21, 55 unpowered glider, using a set of 13 plate-shaped channel wall, with 55 unpowered glider body structure and wing constitutes 10 pressure channel, forming 56 unpowered to set the boost channel The glider; as shown in the third figure, the air outside the pressure passage is kinetic energy and relative flow kinetic energy of the original air flow rate of 17 air without additional use of fuel, heat energy and power, and naturally flows into the 10 pressure passage 14 The maximum cross-sectional area of the air inlet is within A _in , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural inflow 10 pressure passage 14 The maximum cross-sectional area of the air inlet A _in the air, the natural 18 forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage. The natural increase of the absolute pressure of the air acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase 20 on the inner wall of the 10 pressure passage. Thrust, so that increased thrust plenum 10; and the lower without additional fuel, thermal, dynamic situation, so that the natural flow into plenum 10 of the intake port 14 the maximum cross-sectional area A _in, 18 to form an air itself The reversible adiabatic compression process of the air, the natural outflow 10 of the pressurized passage 15 in the exhaust port of the minimum cross-sectional area A _out ⊥, allowing the air to naturally escape the 10 cross-sectional area of the pressurized passage to reduce the constraint, so that the natural outflow 10 The minimum cross-sectional area of the exhaust passage 15 in the exhaust port A _out ⊥ the air, the natural 19 forms a reversible adiabatic expansion process of the air itself, so that the air thus naturally expands the volume, restores the absolute pressure, restores the flow rate, and is pressurized by the passage The exhaust port flows out, and the natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the 12 exhaust port. Therefore, the natural flow rate of the 17 air and the relative flow velocity kinetic energy are naturally increased by 20 to the 10 pressure passage 12 The thrust of the inner wall of the exhaust port is such that the 10 booster passage increases the upward thrust, so that the unpowered glider with the boost passage is increased by 56, and the lift and lift are increased to enhance The climb and lift efficiency of flying in the air to enhance the flight of the flight.

As shown in Figure 22, the 57 aircraft uses a plurality of 13-plate-shaped passage walls, and the fuselage structure of the 57 aircraft and the wing constitutes a 10-pressure passage to form an aircraft with a pressurized passage; In the case of no need to use additional fuel, heat, and power, let the air outside the pressurized passage be kinetic energy at the natural flow rate of 17 air, the relative flow kinetic energy, and the natural flow into the 10 intake passage. Within the area A _in , the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passages make the natural inflow of the 10 intake passages 14 the largest. The air _{in the} cross-sectional area A _in , the natural 18 forms a reversible adiabatic compression process of the air itself, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, flows to the exhaust port of the pressurized passage, and naturally increases the air utilization. The absolute pressure acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate increase by 20 to the thrust of the inner wall of the 10 pressure passage, so that the 10 pressure increase channel is increased. Thrust; and in the case where the fuel without additional thermal energy, power, so that naturally flows into the plenum 10 within intake port 14 the maximum cross-sectional area A _in, 18 forming the air itself reversible adiabatic compression process, the air, natural The outflow 10 is the minimum cross-sectional area A _out内 in the exhaust port of the booster passage 15 to allow the air to naturally escape the constraint of the cross-sectional area reduction within the 10 booster passage, so that the natural outflow 10 is in the exhaust port of the boost passage 15 The air with the smallest cross-sectional area A _out ,, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and flows out of the exhaust port of the pressurized passage, utilizing the air naturally. The expansion and recovery volume expands outwardly on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow velocity increase the thrust of the inner wall of the exhaust port of the 10 pressure passage 12, In order to increase the upward pressure of the 10 booster passages, so that the aircraft with the boost passages can increase the climb force and the lift force to improve the climb, lift efficiency and flight in the air. The voyage and energy saving benefits.

For example, in the twenty-third figure, the 57 aircraft uses a plurality of 13-plate-shaped passage walls to form a 10-pressure passage with the wings on the left and right sides of the 57 aircraft to form an aircraft with a pressurized passageway; as shown in the third figure, In the case of no need to use additional fuel, heat, power, let the air outside the pressurized passage have the natural flow velocity of 17 air, the relative flow kinetic energy, and the maximum cross-sectional area of the inlet of the 10 pressurized passage 14 naturally flowing into the air. In A _in , the natural flow rate of 17 air, the pushing pressure of the kinetic energy of the relative flow velocity, and the reduction of the cross-sectional area in the 10 pressure passages make the natural inflow into the maximum of the intake port of the 10 pressure passage 14 The air _{in the} area A _in , the natural 18 forms the reversible adiabatic compression process of the air itself, so that the natural compression volume of the air, the increase of the absolute pressure, the increase of the flow rate, the flow to the exhaust port of the pressurized passage, the natural increase of the air is absolutely The pressure acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate increase by 20 to the thrust of the inner wall of the 10 pressure passage, so that the 10 pressure passage is increased. ; And in the case where the fuel without additional thermal energy, power, so that naturally the maximum sectional area 14 flows into the plenum 10 of the intake port A _in, 18 forming the air itself reversible adiabatic compression process air, natural Outflow 10 The minimum cross-sectional area A _out内 in the exhaust port of the booster passage 15 allows the air to naturally escape from the constraint of reducing the cross-sectional area in the 10 booster passage, so that the natural outflow 10 is the smallest in the exhaust port of the boost passage 15 The air with a cross-sectional area A _out ,, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and utilizes the natural air. The expansion recovery volume is outwardly expanded to act on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase by 20 to the thrust of the inner wall of the exhaust port of the 10 pressure passage 12, Increase the 10 booster passage to increase the upward thrust, so that the aircraft with the boost passage can increase the climb and lift force to enhance the climb, lift efficiency and flight of the air. Cheng, the benefits of energy conservation.

For example, in the twenty-fourth and twenty-fifth drawings, the 59-propeller uses a plurality of 13-plate-shaped passage walls, and the propeller blades of the 61-propeller form a 10-pressure passage to form a propeller for setting a pressurized passage; In the three maps, the air outside the pressure passage is kinetic energy and relative flow kinetic energy of the original air flow rate of 17 air without additional use of fuel, heat and power, and naturally flows into the inlet of the 10 pressure passage 14 The maximum cross-sectional area A _in is constrained by the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural inflow 10 is pressurized. The air with the largest cross-sectional area A _in , the natural 18 forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, flows to the exhaust port of the pressurized passage, and utilizes the air naturally. The increase of the absolute pressure acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate increase by 20 to the thrust of the inner wall of the 10 pressure passage, so that 10 is supercharged. Road increased thrust; the case and without additional fuel, energy, power, so that naturally flows into the plenum 10 of the intake port 14 the maximum cross-sectional area A _in, 18 forming the air itself reversible adiabatic compression process air , the natural outflow 10 pressure passage 15 the minimum cross-sectional area in the exhaust port A _out ⊥, let the air naturally detach from the 10 cross-sectional area of the pressurized passage to reduce the constraint, so that the natural outflow 10 pressurized passage 15 exhaust The inner air with the smallest cross-sectional area A _out ,, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and flows out of the exhaust port of the pressurized passage. The natural expansion and recovery volume of the air expands outwardly on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase 20 on the inner wall of the exhaust port of the 10 pressure passage 12 The thrust is such that the 10 booster passage increases the thrust forward or upward so that the propeller that sets the boost passage 60 increases the propulsive force to improve the efficiency of the rotary propulsion.

As shown in the twenty-sixth, 62 helicopters, using a plurality of 13-plate channel walls, and the fuselage structure on the left and right sides of the 62 helicopter constitute 10 left and right side pressurized passages, forming 63 helicopters with pressurized passages; As shown in the third figure, the air outside the pressure passage is kinetic energy with a natural flow rate of 17 air, the relative flow velocity kinetic energy, and the natural flow into the 10 pressure passage 14 intake air without additional use of fuel, heat, and power. The maximum cross-sectional area of the mouth is within A _in , with the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passage, so that the natural flow into the 10 pressure passage 14 The maximum cross-sectional area of the air port A _in the air, the natural 18 forms a reversible adiabatic compression process of the air itself, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage, utilizing The natural increase of the absolute pressure of the air acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow rate increase the thrust of the inner wall of the 10 pressure passage. So that increased thrust plenum 10; and the lower without additional fuel, thermal, dynamic situation, so that the natural flow into plenum 10 of the intake port 14 the maximum cross-sectional area A _in, 18 forming the air itself reversible adiabatic The air in the compression process, the natural outflow 10, the minimum cross-sectional area A _out内 in the exhaust port of the booster passage 15 allows the air to naturally escape the constraint of the cross-sectional area reduction within the 10 booster passage, so that the natural outflow 10 pressurization passage 15 The minimum cross-sectional area in the exhaust port A _out ⊥ The air, the natural 19 forms the reversible adiabatic expansion process of the air itself, so that the air naturally expands to recover the volume, restores the absolute pressure, restores the flow rate, and exhausts from the pressurized passage. The mouth flows out, and the natural expansion of the air is used to expand the volume and expand outward to act on the inner wall of the 12 exhaust port. Therefore, the natural flow rate of the 17 air and the relative flow velocity kinetic energy are naturally increased by 20 to the exhaust port of the 10 booster passage 12 The thrust of the inner wall is such that the 10 booster passage increases the upward thrust, so that the helicopter with the boost passage is set to increase the climb, lift, flight range, and energy saving. benefit.

As shown in the twenty-seventh figure, the 64 truck uses a plurality of 13-plate-shaped passage walls, and the body structure of the top of the 64 truck constitutes a 10-pressure passage that is turned upside down by 180°, and is provided with a plurality of 13-plate shapes. The passage wall and the body structure on the left and right sides of the 64 truck constitute 10 supercharged passages on the left and right sides of the inverted 180° upside down, forming 65 trucks with pressurized passages; as shown in the second and third figures, no additional fuel is needed. In the case of heat energy and power, let the air outside the pressure passage be kinetic energy and relative flow velocity of the original natural flow velocity of 17 air, and naturally flow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 to 17 The original natural flow velocity of the air, the pushing pressure of the relative flow velocity kinetic energy, and the restriction of the cross-sectional area reduction in the 10 pressure passages allow the natural inflow of air into the maximum cross-sectional area A _in of the intake port of the 10 pressure passage 14 Natural 18 forms the reversible adiabatic compression process of the air, so that the air naturally compresses the volume, increases the absolute pressure, increases the flow rate, flows to the exhaust port of the pressurized passage, and uses the natural increase of the absolute pressure of the air. It is used for the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow velocity increase the thrust of the inner wall of the 10 pressure passage to increase the thrust of the 10 pressure passage; Without the need to additionally use fuel, heat, and power, let the natural flow into the maximum cross-sectional area Ain of the inlet 10 of the pressurized passage 14 18 to form the air of the air itself reversible adiabatic compression process, the natural outflow 10 boost a minimum sectional area in the passage 15 vent _out ⊥, so that the air from the natural constraints cross-sectional area of the reduced pressure intensification passage 10, so that the minimum cross-sectional area of the plenum 10 natural outflow exhaust port a _out 15 The sly air, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and recovers the volume by the natural expansion of the air. The external expansion acts on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow velocity increase the thrust of the inner wall of the exhaust port of the 10 pressure passage 12, Plenum 10 so increased downward thrust effect, so that the truck 65 is provided plenum downward pressing force increases, the efficiency of operation in order to enhance stability in the air, affixed efficiency.

As shown in the twenty-eighth figure, the 66 bus uses a plurality of 13-plate-shaped passage walls, and the body structure of the top of the 66 bus constitutes a 10-pressure boosting passage that is turned upside down by 180°, and is provided with a plurality of 13-plate shapes. The passage wall, and the body structure on the left and right sides of the 66 bus constitute a 180-degree up and downside left and right side 10 pressurized passage to form a bus with a pressurized passage; as shown in the second and third figures, without additional fuel, In the case of heat energy and power, let the air outside the pressure passage be kinetic energy and relative flow velocity of the original natural flow velocity of 17 air, and naturally flow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 to 17 air. The original natural flow rate, the dynamic pressure of the relative flow kinetic energy, and the reduction of the cross-sectional area in the 10 pressure passages allow the natural flow of air into the maximum cross-sectional area A _in of the intake port of the 10 pressure passage 14 . The natural 18 forms a reversible adiabatic compression process of the air, so that the air naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage, using the natural absolute increase of the absolute pressure of the air. On the inner wall of the 10 pressure passage, the natural flow rate of the 17 air and the natural kinetic energy of the relative flow velocity are increased by 20 to the thrust of the inner wall of the 10 pressure passage, so that the 10 pressure passage increases the thrust; In the case of additional use of fuel, heat, and power, let the natural flow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 18, forming the air of the air itself reversible adiabatic compression process, the natural outflow 10 pressurization a minimum sectional area in the passage 15 vent _out ⊥, so that the air from the natural constraints cross-sectional area of the reduced pressure intensification passage 10, so that the minimum cross-sectional area of the plenum 10 natural outflow exhaust port a _out 15 The sly air, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and recovers the volume by the natural expansion of the air. The external expansion acts on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow velocity increase the thrust of the inner wall of the exhaust port of the 10 pressure passage 12 to The 10 booster passage is increased to the downward thrust, so that the bus with the boost passage is increased by 67 to increase the downward pressure of the bus to improve the stability and the efficiency of the operation.

As shown in the twenty-ninth figure, the 68 wagon uses a plurality of 13-plate-shaped passage walls, and the body structure of the top of the 68 wagon constitutes a 10-pressure boosting passage that is turned upside down by 180°, and a plurality of 13-plates are used. The channel wall of the channel, with the door components on the left and right sides of the 68 wagon, constitutes a left and right side 10 pressurized passage that is turned upside down by 180° to form a wagon with a pressurized passage; as shown in the second and third figures, no additional In the case of using fuel, heat, and power, let the air outside the pressure passage be kinetic energy and relative flow velocity of the original natural flow velocity of 17 air, and naturally flow into the maximum cross-sectional area A _in of the intake port of the 10 pressure passage 14 . With the natural flow rate of 17 air, the dynamic pressure of the relative flow kinetic energy, and the constraint of the cross-sectional area reduction in the 10 pressure passage, the natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 The air, the natural 18 forms the reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, flows to the exhaust port of the pressurized passage, and uses the natural increase of the air absolutely. The force acts on the inner wall of the 10 pressure passage, so that the natural flow rate of the 17 air and the natural kinetic energy of the relative flow velocity increase the thrust of the inner wall of the 10 pressure passage to increase the thrust of the 10 pressure passage; In the case of no need to additionally use fuel, heat, power, let the natural flow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 18, the air that forms the reversible adiabatic compression process of the air itself, the natural outflow 10 The minimum cross-sectional area A _out内 in the exhaust port of the pressurized passage 15 allows the air to naturally escape from the constraint of reducing the cross-sectional area in the 10-pressure passage, so that the natural outflow 10 is the smallest cross-sectional area in the exhaust port of the boost passage 15 A _out of the air, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and recovers with the natural expansion of the air. The outward expansion of the volume acts on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase by 20 on the inner wall of the exhaust port of the 10 pressure passage 12 Force, so that the 10 booster passage increases the downward thrust, so that the wagon with the boost passage is set to increase the downward push pressure to improve the stable efficiency and the grounding efficiency of the operation.

As shown in the thirtieth figure, the 70 sedan uses a plurality of 13-plate-shaped passage walls, and the body structure of the top of the 70 sedan constitutes a 10-increment channel that is turned upside down by 180°, and uses a plurality of 13-plate-shaped passages. The wall, with the door components on the left and right sides of the 70 sedan, constitutes a 180° upside down left and right side 10 pressurized passage to form a sedan with a pressurized passage; as shown in the second and third figures, no additional fuel, heat, In the case of power, let the air outside the pressure passage be kinetic energy and relative flow velocity of the original natural flow velocity of 17 air, and naturally flow into the maximum cross-sectional area A _in the inlet of the 10 pressure passage 14 to 17 air. The natural flow rate, the relative flow velocity of the kinetic energy of the dynamic pressure and the reduction of the cross-sectional area within the 10 plenum channel, so that the natural flow into the 10 plenum 14 inlet air inlet the maximum cross-sectional area A _in the air, natural 18 forms a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage, utilizing the natural increase of the absolute pressure of the air to act on the 10 The inner wall of the pressurized passage, so that the natural flow rate of the 17 air, the natural kinetic energy of the relative flow velocity is increased by 20, and the thrust of the inner wall of the 10 pressurized passage is increased, so that the 10 booster passage increases the thrust; In the case of using fuel, heat, and power, the natural inflow into the maximum cross-sectional area A _in the inlet of the 10 pressurized passage 14 18 forms the air of the air itself reversibly adiabatic compression process, and naturally flows out 10 the pressurized passage 15 The minimum cross-sectional area A _out内 in the exhaust port allows the air to naturally escape from the constraint of reducing the cross-sectional area in the 10 pressurized passage, so that the natural outflow 10 is the smallest cross-sectional area in the exhaust port of the pressurized passage 15 A _out Air, the natural 19 forms a reversible adiabatic expansion process of the air, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, flows out of the exhaust port of the pressurized passage, and expands outward by the natural expansion of the air. Acting on the inner wall of the 12 exhaust port, so that the natural flow rate of the 17 air and the relative flow velocity kinetic energy naturally increase by 20 to the thrust of the inner wall of the exhaust port of the 10 booster passage 12, so that 10 Increased pressure passage downward thrust effect, so that the plenum 71 disposed cars downward pressing force increases, the efficiency of operation in order to enhance stability, efficiency affixed.

In summary, the above embodiments of the present invention are not intended to be merely or only the embodiments. The main purpose of the above embodiments of the present invention is to express a pressurized passage for increasing the thrust of vehicles and implements operating in the air. And methods and effects are easy for those who are familiar with such skills. The additions, modifications, and alterations of the above-described embodiments are intended to be included in the scope of the present invention without departing from the spirit and scope of the invention.

10‧‧‧Train channel

11‧‧‧air inlet

12‧‧‧Exhaust port

13‧‧‧ plate-shaped channel wall

Claims (8)

A pressurized passage and method for increasing the thrust of a vehicle and an instrument operating in the air, comprising: at least one pressurized passage; the pressurized passage having a plate-shaped passage wall having an intake inclined upwardly The mouth has an exhaust port inclined obliquely to the rear, and has a polygonal and circular arc-shaped channel structure, and has a structure in which a cross-sectional area in the passage is reduced from the air inlet to the exhaust port; the intake of the pressurized passage The maximum cross-sectional area of the port A _in > the minimum cross-sectional area _{in the} exhaust port A _out ⊥; the maximum cross-sectional area of the inlet of the pressurized passage A _in > the maximum cross-sectional area of the exhaust port A _out ; The maximum cross-sectional area of the exhaust port A _out ≧ the minimum cross-sectional area A _out内_in the exhaust port; the ratio of the maximum cross-sectional area A _{in of the} intake port of the boosting passage to the minimum cross-sectional area A _out排气_in the exhaust port 1<A _in /A _out ⊥≦27.435; using at least one pressurized passage, disposed on the vehicle, the components, structure or structure of the vehicle operating in the air, so that the original flow velocity kinetic energy of the air outside the pressurized passage can be Smooth inflow and outflow into the pressurized passage; no additional need The case with the fuel, heat, power, so that outside air plenum at a flow rate of the kinetic energy of the original natural flows of the air intake plenum maximum sectional area A _in, the flow rate of air to the kinetic energy of the original dynamic pressure The pushing and the restriction of the cross-sectional area reduction in the pressurized passage naturally form a reversible adiabatic compression process of the air, so that the air thus naturally compresses the volume, increases the absolute pressure, increases the flow rate, and flows to the exhaust port of the pressurized passage. The natural pressure of the air is applied to the inner wall of the pressurized passage, so that the original kinetic energy of the air naturally increases the thrust acting on the inner wall of the pressurized passage, so as to connect the components and structures of the pressurized passage. Or the structure increases the thrust to increase the thrust of the vehicles and implements operating in the air; and allows the natural inflow into the pressurized passage to form a self-reversible adiabatic compression process without additional use of fuel, heat, or power. air, the minimum cross-sectional area a in the natural outflow vent _out plenum cross-sectional area of the plenum ⊥ departing from the reduced constraints, natural shape The air itself reversibly adiabatic expansion process, so that the natural expansion of the air thus recovers the volume, restores the absolute pressure, restores the flow rate, and flows out from the exhaust port of the pressurized passage; and uses the natural expansion of the air to recover the volume and expand outward to act on the pressurized passage. The inner wall of the gas port, so that the original kinetic energy of the air naturally increases the thrust acting on the inner wall of the exhaust port of the pressurized passage, so as to increase the thrust of the component, structure or structure in which the pressurized passage is provided, so that The vehicles and implements operating in the air increase the thrust; so that the vehicles and implements operating in the air can be improved in the efficiency of operation in the air and save energy. As described in claim 1, the pressurized passage and method for increasing the thrust of the vehicle and the machine operating in the air, wherein the vehicle and the machine operating in the air refer to the operation, movement and rotation in the air. Vehicles, implements, or vehicles that use natural kinetic energy of air, relative kinetic energy, airborne motion, motion, and rotation. As described in the first paragraph of the patent application, a pressurized passage and method for increasing the thrust of a vehicle and an instrument operating in the air, wherein the vehicle includes: a vehicle, a ship, and an aircraft. As described in the first paragraph of the patent application, a pressurized passage and method for increasing the thrust of a vehicle and an implement operating in the air, wherein the implement includes: a machine, an appliance, and an appliance. As described in the first paragraph of the patent application, a pressurized passage and method for increasing the thrust of a vehicle and an instrument operating in the air, wherein the increased thrust includes: an increase in the direction of rotation The thrust, the increase of the thrust to the top, the thrust to the lower side, the thrust to the left, the thrust to the right, the thrust to the front, and the thrust to the rear. As described in the first paragraph of the patent application, a pressurized passage and method for increasing the thrust of a vehicle and an instrument operating in the air, wherein the pressurized passage includes: a pressurized passage formed by a plate-shaped passage wall, The pressure-increasing passage formed by the plate-shaped passage wall and the components of the vehicle and the machine that are operated in the air, the plate-shaped passage wall and the carrier and the structure of the machine in the air constitute a pressurized passage and a plate. The shaped passage wall forms a pressurized passage together with the carrier and the structure of the implement that operate in the air. As described in claim 1, the pressurized passage and method for increasing the thrust of the vehicle and the machine operating in the air, wherein the ratio of <1 _in /A _out ⊥≦27.435, the ratio of 27.435 is determined by the relationship [( γ+1)/2] ^γ/(γ-1) /sin(4°) calculated that the relationship γ is the gas adiabatic index, and the air in the natural atmosphere is γ≒1.40 at 20 °C. The sin(4°) ≒ 0.069 is substituted into the relational formula to obtain [(γ+1)/2] ^γ/(γ-1) /sin(4°)≒1.893/0.069≒27.435, the relation [[γ+ 1)/2] ^γ/(γ-1) /sin(4°) can also be written as [2/(γ+1)] ^-γ/(γ-1) /sin(4°). As described in claim 1, the pressurized passage and method for increasing the thrust of the vehicle and the machine operating in the air, wherein the original kinetic energy of the air includes: the original natural kinetic energy of the air, the air The original relative flow kinetic energy.