WO2024060468A1

WO2024060468A1 - Facility using airflow for power assistance and auxiliary power generation (weak-pressure-adsorption-type fluid-driven power machine)

Info

Publication number: WO2024060468A1
Application number: PCT/CN2023/000047
Authority: WO
Inventors: 王子捷
Original assignee: 王子捷
Priority date: 2023-02-27
Filing date: 2023-03-26
Publication date: 2024-03-28

Abstract

According to the specific application of the law of conservation of energy, Bernoulli's principle has long told people that: when a fluid flows in a pipe, where the flow velocity is high, the pressure is low; and where the flow velocity is low, the pressure is high. According to Bernoulli's principle, when air flows in a pipe, where the flow velocity is high, the pressure is low; and where the flow velocity is low, the pressure is high. According to the principle of fluid continuity, when air flows in a pipe, where the pipe is narrow, the flow velocity is high; and where the pipe is wide, the flow velocity is low. In view of these two points, the following preliminary conclusion can be drawn: when air flows in a pipe, where the pipe is narrow, the flow velocity is high and the pressure is low; and on the contrary, where the pipe is wide, the flow velocity is low and the pressure is high. Drawing upon this conclusion, a preliminary explanation can be made for the reason for the lift on a wing (quoted from the principle of aircraft flight): during the flight of an aircraft, a fluid flows along a lower part of an aircraft wing in a direction opposite to the flight direction of the aircraft due to gravitational acceleration, creating the lift for the aircraft wing. The lift for an aircraft wing is a very huge amount of natural energy. Accordingly, the collection and reuse of a fluid that flows along the bottom of a moving object in a direction opposite to the motion direction of the moving object due to gravitational acceleration is generated. Therefore, a huge amount of natural energy similar to the lift for an aircraft wing can be produced, a power source for a moving object with a turbine rotating facility is formed, and a very practical driving power for a moving object with a turbine rotating facility is formed. During the flight of an aircraft, the wing overcomes a fluid flowing along the wing in a direction opposite to the flight direction of the aircraft, so as to form a weak-pressure adsorption space in the direction opposite to the flight direction of the aircraft; and this design pattern presents an excellent induction pattern for adsorbing a plurality of fluid driving surfaces in a moving object with a turbine rotating facility so as to form numerous turbine driving fluids. Therefore, it is feasible to design and put into practical application a new weak-pressure-adsorption-type fluid-driven power machine with a plurality of fluid driving surfaces, and it is also possible to specifically implement the design pattern on a facility using an airflow for power assistance and auxiliary power generation.

Description

Utilize air flow to assist and auxiliary power generation facilities (weak pressure adsorption fluid-driven power machinery)

Technical field

The present invention relates to a novel weak-pressure adsorption fluid-driven power machine with multiple fluid-driven surfaces, and in particular to a specific application in utilizing airflow assistance and auxiliary power generation facilities.

Background technique

The basis of human survival is to adapt to the natural environment in which human beings survive. As people living on the earth, we should realize that the earth's body and the atmosphere surrounding the earth's body, etc., are the fundamental factors that determine whether people can survive the creation and destruction of the natural environment. The eruptions of volcanoes in some areas of the earth's body, the discoveries of some people on the earth, and some ancient legends of the earth's people, etc., show that the earth's body is a living body, and that there have been some great changes in the earth's body, the earth's surface air pressure, sea levels, etc. ( See the attached page for the ancient underwater city). It shows that previous humans have existed in the earth's body, and it shows that the crystallization of some of the creations of previous humans has surpassed some of the creations of modern people (such as the mysterious metal 2 billion years ago in the attached page). Perhaps the population expansion and the serious shortage of resources per capita in the past forced people to exploit the earth's body in terrible ways, destroying the nearly stable coexistence between the earth's body plates. Perhaps in order to survive, people in the past had no choice but to develop some highly fissionable nuclear kinetic energy and high-energy-condensation products, and there were terrible nuclear wars. The terrible fission capabilities produced by the scrapping of nuclear waste and high-energy resources, as well as chemical pollution and nuclear war, have accelerated some fission around the earth's body's ozone layer and adapted to the natural environment in which humans previously lived. The ozone hole and thinning of the ozone layer discovered by people on the earth today. I wonder if the people who lived on the earth in the past were due to some huge changes in the ozone layer surrounding the earth's body, which affected the atmospheric pressure on the earth's surface and caused terrible fluctuations in sea level. , prompting the terrible drift of the earth's plates that have been mined and exploited by people, creating violent collisions between the earth's plates, causing the destruction of the natural environment that adapted to the survival of previous people, and prompting the natural destruction of previous people, thus creating ancient underwater cities and creating The mysterious metal 2 billion years ago created the Himalayas and more. With the stabilization of great changes in the earth's body and the atmosphere surrounding the earth's body, and with the regeneration of the natural environment that adapts to human survival, new human beings have emerged on the earth's body. If the people who lived before were naturally destroyed due to the huge changes in the ozone layer surrounding the earth's body, people on the earth now should be on the eve of the natural destruction of the people who lived before.

The ozone hole and the thinning of the ozone layer have warned that people should make full use of natural energy, try not to damage the ozone layer surrounding the earth's body, and maintain the natural environment suitable for people's survival while improving some of people's old living patterns. In May 2015, with the help of fluid-driven turbine manufacturing craftsmen in Tianjin, China, I used a turbine to carry a permanent magnet generator. When driving the turbine with one driving point at the same wind pressure, the turbine carried the permanent magnet generator to rotate slightly, using three When the driving points drive the turbine at the same time, the number of rotations of the permanent magnet generator carried by the turbine increases several times. The value created by the combined force of multiple driving points at the same wind pressure shows that some of my previous ideas can be implemented in practical applications. For this reason I recommend to people the specific application of a new type of weak-pressure adsorption fluid-driven power machinery with multiple fluid-driven surfaces in using air flow to assist and auxiliary power generation facilities.

Summary of the invention

According to the specific application of the law of conservation of energy, Bernoulli's theorem has long told people: when fluid flows in a pipe, wherever the flow rate is high, the pressure is small; where the flow rate is low, the pressure is high. According to Bernoulli's theorem, when air flows in a pipe, wherever the flow velocity is high, the pressure is small; wherever the flow velocity is low, the pressure is high. According to the fluid continuity theorem: when air flows in a pipe, wherever the pipe is thin, the flow velocity is high; where the pipe is thick, the flow velocity is small. Combining the above two points, we can draw the following preliminary conclusion: When air flows in a pipe, wherever the pipe is thin, the flow velocity is high and the pressure is low; conversely, wherever the pipe is thick, the flow velocity is small and the pressure is low. Large; with the help of this conclusion, we can preliminarily explain the reason for the lift force on the wing (quoted from the principle of aircraft flight); during the flight of the aircraft, the gravity acceleration fluid flows along the lower part of the aircraft wing in the opposite direction of the aircraft flight, forming the shape of the aircraft wing. Lifting force. The lifting force of an airplane wing is A very huge natural energy, resulting from the collection and reuse of gravity acceleration fluid flowing along the bottom of the moving object in the opposite direction of the moving object, can produce a huge natural energy similar to the lifting force of the aircraft wing, forming a turbine rotation facility for the moving object The power source forms a very practical driving force for moving objects carrying turbine rotation facilities. During the flight of the aircraft, the wings overcome the flow along the wings in the opposite direction of the aircraft flight to form a weak pressure adsorption space in the opposite direction of the aircraft flight. It is the pole of adsorbing moving objects carrying multiple fluid driving surfaces in the turbine rotating facility to form numerous turbine driven fluids. In the optimal induction mode, the design and practical application of a new weak-pressure adsorption fluid-driven power machine with multiple fluid-driven surfaces is feasible, and can be implemented in the use of air flow assistance and auxiliary power generation facilities.

The use of air flow assist and auxiliary power generation facilities is applied to air flow assist bicycles, electric assist bicycles using air flow to assist power generation, or electric motorcycles using air flow to assist power generation. It mainly involves: along the inside of the external air deflector (not shown in the figure) from top to bottom The lower part is divided into fluid pressure collecting cabin pressure gathering facilities, turbine driving facilities, and fluid negative pressure induction facilities, and generators (22), power transmission devices (23), batteries (24), drive motors (26), and electric energy control devices. (27), induced car body (28).

The fluid pressure collecting chamber pressure gathering facility mainly consists of: a fluid pressure collecting chamber (1) arranged around the periphery of the turbine driven fluid inflow device 13F or 13G around the turbine drive blades, and a fluid inflow fluid pressure collecting chamber (1) provided on both sides of the turbine driving facility. Port (2), the fluid flows into the fluid collecting bin flow guide cover (4), the fluid dust collector (5), the fluid flows into the flow guide cover (7), the fluid filter (6), the fluid flows into the fluid collecting bin inlet (3), the fluid flows into the interceptor cover (8), the fluid flows into the interceptor cover adjustment device (25) (not shown in the figure), and the external deflector cover (not shown in the figure).

The turbine drive facility mainly includes: turbine drive blades (9), turbine housing (10) (not shown in the figure), turbine shaft (11), turbine bracket (12), and a turbine drive fluid inflow device 13F is provided around the periphery of the turbine drive blades. There are multiple converging nozzles A, a mixing cylinder B, a turbine fluid driving nozzle C, a pressurizing tank and a depressurizing tank fluid separation plate D, and a pressurizing fluid diversion groove E. The fluid outlet of the converging nozzle A is connected to A fluid suction port is provided between the fluid inlet of the mixing cylinder B, and the fluid outflow port of the mixing cylinder B and the fluid inlet of the turbine fluid driving nozzle C are connected to each other; and a plurality of turbine driving fluid inflow devices 13G are provided around the periphery of the turbine driving blades. There is a constricted nozzle A, a turbine fluid driven nozzle C, a pressurizing tank and a pressure reducing tank fluid dividing plate D. The fluid outflow outlet of the constricted nozzle A and the fluid inlet of the turbine fluid driven nozzle C are connected to each other; a turbine fluid is provided Discharge port (14), turbine external drive fluid inlet (17), external drive fluid filter (18), external drive fluid guide cover (19), external drive fluid flows out of the constriction nozzle (20), and external drive fluid flows in The interceptor cover (21), the external driving fluid flows into the interceptor cover driving device (29), and the external deflector cover (not shown in the figure). There is a pressure reducing groove on the inside of the turbine drive blade and a pressure increasing groove on the outside. The turbine is fluid driven and adopts the fluid driving surface mode.

The fluid negative pressure inducing facilities include: turbine external drive fluid, gravity acceleration weak pressure adsorption fluid, fluid negative pressure guide cover (15), fluid negative pressure discharge port (16), and reverse flow along the outside of the external guide cover to the car body. direction of the fluid.

When an airflow-assisted bicycle, an electric power-assisted bicycle that utilizes airflow to assist power generation, or an electric motorcycle that utilizes airflow to assist power generation are traveling, and the vehicle body (28) is carrying an airflow-assisted or airflow-assisted power generation facility, the vehicle body (28) must Display) The fluid flows in the opposite direction to the vehicle body from the inside of the inflow port. The fluid flows through the rear part which is slightly lower than the front part. When the fluid flows into the inlet (3) of the fluid pressure tank, it forms a gravity acceleration fluid with extremely high pressure (quoted from the principle of aircraft flight). ), part of the gravity-accelerated fluid flows into the fluid collecting chamber inlet (3) and the fluid filter (6) and flows into the deflector cover (7). The gravity-accelerated fluid that flows into the deflector cover (7) passes through The fluid dust collecting net (5), the fluid flowing into the fluid collecting tank deflector (4), the fluid flowing into the fluid collecting tank shrinkage (2) flows into the fluid collecting tank (1), and the subsequent inflow of gravity acceleration fluid is very fast. A high-pressure collecting fluid is formed in the fluid collecting chamber (1). Part of the gravity-accelerated fluid flows into the fluid pressure chamber inlet (3) along the slope and outside the turbine fluid discharge port (14), and flows through the fluid negative pressure guide cover (15) and the fluid negative pressure outlet (16), flowing to the rear of the vehicle body; when the airflow assist and the airflow-assisted power generation facilities adopt the turbine-driven fluid inflow device 13F working mode around the periphery of the turbine-driven blades (as shown in Figure 4.13F), the fluid pressure accumulation Part of the high-pressure fluid collected in the chamber (1) is sprayed into the mixing cylinder B through the constricted nozzle A in the turbine-driven fluid inflow device 13F around the periphery of the turbine-driven blades, and the high-pressure fluid is sprayed into the fluid collecting chamber (1) in the mixing cylinder B. The turbine fluid driving surface is formed through the turbine fluid driving nozzle C and then the turbine driving blades (9) are driven. Since the turbine driving fluid adopts the fluid driving surface mode, when the turbine initially driving fluid ejected from the constricted nozzle A flows through the mixing cylinder B and the turbine fluid driving nozzle C to form the turbine fluid driving surface, the flow rate will slow down. Because the gap between the turbine fluid driving nozzle C and the driven turbine is very small, and the fluid injected by the constriction nozzle A through the mixing cylinder B is the gravitational acceleration fluid of the vehicle body that has been introduced by the fluid pressure chamber (1) and has been continuously pressurized. The pressure is extremely high, and the extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the continued pressure of the fluid required to slow down the flow rate when the turbine fluid drives the nozzle C to form the turbine fluid driving surface. The fluid driving surface composed of numerous turbine fluid driving nozzles C that continuously maintain pressure, induced by the guide angle of the turbine fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, drives the turbine driving blade (9), and is driven by the driven turbine. The blades (9) drive the turbine shaft (11) to rotate through numerous invisible levers formed by the turbine bracket (12) and the turbine shaft (11). Since the turbine driving mode is a fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point. As the turbine shaft (11) rotates, the turbine driving fluid that drives the turbine driving blades (9) partially drives the turbine driving fluid of the turbine driving blades (9) under the separation of the fluid dividing plate D between the pressure increasing tank and the pressure reducing tank. The fluid flows into the supercharging tank due to the centrifugal phenomenon caused by the rotation of the turbine. Part of the turbine-driven fluid flowing into the supercharging tank gradually increases the density and pressure of the supercharging fluid in the supercharging tank. At the same time, the decompression groove is caused to rotate along with the turbine shaft (11), and the density of the turbine driving fluid in the decompression groove is weakened. The density of the memory turbine driving fluid in the pressure reducing groove is weakened, which reduces the resistance ability of the memory fluid in the pressure reducing groove against the rotation of the turbine when the pressure reducing groove is transferred to the next turbine fluid driving surface. As the density and pressure of the pressurized fluid flowing into the pressurized tank gradually increase, part of the high-pressure fluid in the fluid pressure chamber (1) is sprayed into the mixing cylinder B through the reduced-nozzle A, because the fluid flow from the reduced-nozzle A There is a fluid inlet between the outlet and the fluid inlet of the mixing cylinder B, so when part of the high-pressure fluid in the fluid pressure chamber flows through the constricted nozzle A and is sprayed into the fluid inlet of the mixing cylinder B, the fluid inlet of the mixing cylinder B is The pressurized fluid in the peripheral part of the pressurizing tank is sucked into the mixing cylinder B through the fluid suction port. It is sucked into the pressurizing fluid in the inner part of the mixing cylinder B and the part of the high-pressure fluid in the pressure collecting chamber sprayed from the constricted nozzle A to form a high pressure. The mixed airflow is then sprayed out through the turbine fluid drive nozzle C, driving the turbine drive blades (9). The numerous invisible levers formed by the driven turbine drive blades (9) through the turbine bracket (12) and the turbine shaft (11) will cause the turbine shaft (11) to rotate easily. As the turbine rotates, part of the pressurized fluid flowing into the pressurized groove is discharged through the pressurized fluid guide groove E.

Along the inner side of the inlet of the external deflector (not shown in the figure) and the fluid into the fluid inlet of the pressure tank (3), part of the gravity-accelerated fluid flows toward the opposite direction of the vehicle body from the lower part of the diversion slope, and drives the fluid inlet through the outside of the turbine (17 ), the external drive fluid filter (18) flows into the external drive fluid guide cover (19), and the gravity acceleration fluid flowing into the external drive fluid guide cover 19 is ejected through the external drive fluid outflow constriction nozzle (20) to drive the turbine Blade(9). In order to enable the numerous turbine fluid driven nozzles C in the turbine drive facility to discharge the numerous turbine driven fluids generated when driving the turbine to rotate as quickly as possible, the endmost turbine fluid driven surfaces of the numerous turbine fluid driven nozzles C are connected to the turbine external driven fluid in a constriction type fluid drive. There is a vacuum arc between the surfaces, and the flow rate of the external driving fluid of the turbine is used. While the external driving fluid drives the turbine driving blades (9), the external driving fluid and the numerous fluids injected into the turbine driving fluid inflow device 13F around the periphery of the turbine driving blades A weak pressure zone is formed between the turbine drive fluid and the pressurized fluid discharged from the pressurized fluid diversion channel E in the pressurized tank. The weak pressure zone causes the vacuum arc to generate a vacuum phenomenon. The vacuum adsorption phenomenon of the vacuum arc causes the surrounding turbine drive The numerous turbine driving fluids injected into the turbine driving fluid inflow device 13F on the blade periphery and the boosting fluid partially flowing through the boosting fluid guide slot E and discharged from the boosting grooves are sucked into the vacuum arc and flow into the external driving fluid. turbine The driving fluid mixes with the external driving fluid to form an external driving fluid with a greatly increased flow rate. The external driving fluid with a greatly increased flow speed drives the turbine driving blades (9) and then flows to the turbine fluid discharge port (14). At the same time, the pressurized fluid diversion groove E and other facilities are also produced to promote the flow pattern in which part of the pressurized fluid in the pressurized tank is sucked out, so that the reverse resistance produced by the pressurized fluid in the pressurized tank to the rotating turbine is very small. , it also maintains the pressure of the pressurized fluid in the pressurized tank, restricts the random discharge of a large amount of pressurized fluid in the pressurized tank, and creates a more reasonable reuse of secondary energy.

Along the inner side of the inlet of the external deflector (not shown in the figure) and the fluid inlet of the fluid collecting tank (3), part of the gravity-accelerated fluid flows from the lower part of the deflector slope toward the opposite direction of the vehicle body, and flows through the turbine fluid discharge port (14) When the fluid flows from the outside to the inside of the negative pressure guide cover (15), the fluid density and flow rate due to gravity acceleration are extremely high, forming a weak pressure adsorption fluid on the outside of the turbine fluid outlet (14). The weak pressure adsorption fluid induces numerous turbine driven fluids to pass through the turbine fluid When the fluid flows into the negative pressure guide cover (15) from the discharge port (14), the weak pressure adsorption fluid causes the flow rate of the external driving fluid to further increase greatly. The weak pressure adsorption ability prompts the external driving fluid to absorb more of the numerous turbine driving fluids injected into the turbine driving fluid inflow device 13F around the periphery of the turbine driving blades and the pressurized fluid discharged from the pressurized fluid diversion groove E through part of the pressurized tank. It is sucked into the vacuum arc and flows into the external driving fluid, thereby further improving the fluid driving ability of the external driving fluid, and at the same time, more turbine driving fluid surrounding the periphery of the turbine driving blades flows into the numerous turbine driving fluids and booster grooves injected by the device 13F The pressurized fluid discharged through the pressurized fluid guide groove E in the middle part is induced by the external driving fluid to flow to the turbine fluid discharge port (14), and then flows along the external guide cover (not shown in the figure) into the inside of the port and the fluid The inflow fluid flows into the lower part of the guide slope of the pressure chamber inlet (3), flows through the turbine fluid discharge port (14) and flows to the inside of the negative pressure guide cover (15). Under the weak pressure adsorption fluid generated by the gravity acceleration fluid, many turbines The weak pressure adsorption fluid generated by the driving fluid and the gravity acceleration fluid flows to the fluid negative pressure discharge port (16).

The flow rate of the fluid flowing along the outside of the external air deflector (not shown in the figure) to the opposite direction of the vehicle body. With the running speed of the vehicle body, it flows through the outside of the fluid negative pressure discharge port (16) and flows in the opposite direction of the vehicle body. A very ideal fluid negative pressure adsorption space is formed outside the open fluid negative pressure outlet (16). The fluid negative pressure adsorption space absorbs the weak pressure generated by numerous turbine-driven fluids and gravity acceleration fluids inside the fluid negative pressure guide cover (15). The adsorbed fluid passes through the fluid negative pressure discharge port (16) and is sucked into the negative pressure adsorption space behind the vehicle body. Along the inner side of the external deflector (not shown in the figure) and the fluid flowing into the fluid manifold inlet (3), the gravity-accelerated fluid flows from the lower part of the deflection slope toward the opposite direction of the vehicle body movement, and flows through the turbine fluid discharge port (14) and the fluid When the negative pressure guide cover (15) and numerous turbine-driven fluids and weak-pressure adsorption fluids flow into the negative pressure adsorption space behind the vehicle body through the fluid negative pressure outlet (16), they fill the negative pressure adsorption space behind the vehicle body. Some fluid is required to reduce the force of the vehicle body retracting backward caused by the adsorption space behind the vehicle body running.

Air-assisted bicycles and air-assisted power generation electric power-assisted bicycles or air-assisted power generation electric motorcycles carrying air-assisted or air-assisted power generation facilities adopt the working mode of the turbine-driven fluid inflow device 13G surrounding the periphery of the turbine-driven blades (such as Figure 4.13G), the difference between them and the working mode of the turbine driving fluid inflow device 13F surrounding the periphery of the turbine driving blades is that the mixing cylinder B and the pressurized fluid guide groove E are eliminated. The fluid outflow port of the constricted nozzle A and the fluid inlet port of the turbine fluid drive nozzle C are connected to each other. When the vehicle body is running, airflow is used to assist or the power generation facility is operated using airflow, part of the high-pressure fluid collected in the fluid pressure chamber (1) is sprayed into the reduced nozzle A in the turbine-driven fluid inflow device 13G surrounding the periphery of the turbine-driven blades. Turbine drive nozzle C, because the turbine drive fluid adopts the fluid drive surface mode, the flow rate will slow down when the turbine initial drive fluid ejected from the constricted nozzle A flows into the turbine fluid drive nozzle C to form the turbine fluid drive surface. Since the gap between the turbine fluid driving nozzle C and the driven turbine is very small, the fluid outflow port of the reduced port nozzle A and the fluid inlet port of the turbine fluid driven nozzle C are connected to each other, and the fluid injected by the reduced port nozzle A is pressure-collected by the fluid. The pressure of the gravitational acceleration fluid introduced into the cabin (1) after the continued pressurization of the car body is extremely high. The extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the turbine fluid drive nozzle C. The continuous pressure of the fluid required to slow down the flow rate when forming the turbine fluid driving surface. The fluid driving surface composed of numerous turbine fluid driving nozzles C with constant pressure, induced by the flow direction angle of the fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, drives the turbine driving blades (9), and the numerous driven turbines The numerous invisible levers formed by the drive blades (9) via the turbine bracket (12) and the turbine shaft (11) will allow the turbine shaft (11) to rotate easily. As the turbine shaft (11) rotates, the turbine driving fluid that drives the turbine driving blades (9) partially drives the turbine driving fluid of the turbine driving blades (9) under the separation of the fluid dividing plate D between the pressure increasing tank and the pressure reducing tank. The fluid flows into the supercharging tank due to the centrifugal phenomenon caused by the rotation of the turbine. Part of the turbine driving fluid flowing into the supercharging tank and the turbine driving fluid ejected from the numerous turbine fluid driving nozzles C flow to the final fluid drive of the numerous turbine fluid driving nozzles C. A vacuum arc is provided between the external driving fluid surface of the turbine and the reduced fluid driving surface of the turbine. By utilizing the flow rate of the external driving fluid of the turbine, while the external driving fluid drives the turbine driving blades (9), the external driving fluid interacts with the surrounding turbine driving blades. A weak pressure zone is formed between the numerous turbine drive fluids injected into the peripheral turbine drive fluid inflow device 13G and part of the turbine drive fluid flowing into the booster tank. The weak pressure zone causes the vacuum arc to generate a vacuum phenomenon, and the vacuum arc adsorption phenomenon causes the surrounding The numerous turbine driving fluids injected into the turbine driving fluid inflow device 13G on the periphery of the turbine driving blades and part of the turbine driving fluid flowing into the booster tank are sucked into the vacuum arc and flow into the external driving fluid. The numerous turbine driving fluids and external driving fluids flowing into the external driving fluid The mixing creates an externally driven fluid with a greatly increased flow rate. The external driving fluid with a greatly increased flow speed drives the turbine driving blades (9) and then flows to the turbine fluid discharge port (14). At the same time, as the turbine shaft (11) rotates, the density of the turbine driving fluid in the decompression groove is weakened, which reduces the force generated by the fluid in the decompression groove against the rotation of the turbine when the decompression groove is transferred to the next turbine fluid driving surface. Blocking ability. Since the turbine driving mode is a fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point. Bicycles that use airflow to assist and electric power-assisted bicycles that use airflow to assist power generation or electric motorcycles that use airflow to assist power generation, when using the turbine-driven fluid inflow device 13G around the periphery of the turbine drive blades, there is no need to use the turbine-driven fluid inflow device 13F around the periphery of the turbine drive blades. Reuse of part of the turbine drive fluid in the boost tank during operating mode.

other:

A fluid pressure collecting bin (1), a fluid inflow into the fluid pressure collecting bin constriction (2), a fluid inflow into the fluid pressure collecting bin inlet (3), a fluid inflow into the fluid pressure collecting bin flow guide cover (4), a fluid dust collecting net (5), a fluid filter net (6), a fluid inflow into the flow guide cover (7), a fluid inflow into the intercepting cover (8), a turbine driving blade (9), a turbine housing (10), a turbine shaft (11), a turbine bracket (12), a turbine driving fluid inflow device 13F surrounding the outer periphery of the turbine driving blade is provided with a plurality of constriction nozzles A, a mixing gas cylinder B, a turbine fluid driving nozzle C, a boosting groove and a decompression groove fluid partition plate D, a boosting fluid flow guide groove E, a turbine fluid discharge port (14), a fluid negative pressure flow guide cover (15), a fluid negative pressure discharge port (16), a turbine An external driving fluid inlet (17), an external driving fluid filter (18), an external driving fluid flow guide cover (19), an external driving fluid outflow constriction nozzle (20), an external driving fluid inflow interception cover (21), a pressure reducing groove provided on the inner side of the turbine driving blade and a pressurizing groove provided on the outer side, a generator (22), a power transmission device (23), a battery (24), a fluid inflow interception cover adjustment device (25), a driving motor (26), an electric energy control device (27), an induction vehicle body (28), an external driving fluid inflow interception cover driving device (29), and a turbine driving fluid inflow device 13G surrounding the outer periphery of the turbine driving blade, which is provided with a plurality of constriction nozzles A, a turbine fluid driving nozzle C, a pressurizing groove and a pressure reducing groove fluid partition plate D, etc.

Purpose of the present invention:

Through a new type of weak-pressure adsorption fluid-driven power machine with multiple fluid-driven surfaces, air-assisted bicycles and air-assisted electric power-assisted bicycles or air-assisted electric motorcycles can be carried by air-assisted or air-assisted bicycles. The reuse of secondary energy displayed in power generation facilities improves people's cognitive ability to adapt to nature and rationally utilize nature, alleviate some of the confusion caused by the lack of per capita energy and resources to people's survival, and reduce man-made damage to the ozone layer surrounding the earth's body. , maintain the natural environment suitable for people's survival.

Picture description:

FIG1 is a schematic diagram of a cross-sectional application of an airflow-assisted bicycle.

Figure 2 is a schematic cross-sectional application diagram of an electric power-assisted bicycle using airflow to assist in power generation.

Figure 3 is a schematic cross-sectional application diagram of an electric motorcycle using airflow to assist power generation.

Figure 4 is a schematic diagram of the application of turbine drive fluid inflow devices 13F and 13G around the periphery of the turbine drive blades.

Specific implementation:

Example 1 Using airflow to assist a bicycle

Utilizing air flow to assist the bicycle eliminates the generator (22), battery (24), driving motor (26), and electric energy control device (27). As shown in Figure 1, when the airflow assisting bicycle is running and the airflow assisting device is carried along the vehicle body (28), the fluid flows in the opposite direction of the movement of the vehicle body along the inside of the inlet of the external air deflector (not shown in the figure). When the fluid flows into the inclined plane of the inlet (3) of the fluid pressure tank through the rear part which is slightly lower than the front part, a gravity acceleration fluid with extremely high pressure is formed (derived from the principle of aircraft flight), and part of the gravity acceleration fluid flows into the fluid pressure tank flow through the fluid. The fluid flowing into the inlet (3) and the fluid filter (6) flows into the guide cover (7). The gravity acceleration fluid flowing into the guide cover (7) passes through the fluid dust collection screen (5) and flows into the fluid pressure chamber. The fluid flows into the flow guide cover (4) and the fluid pressure collecting chamber shrinkage (2) and flows into the fluid pressure collecting chamber (1). The subsequent inflow of gravity acceleration fluid quickly forms a high-pressure collecting fluid in the fluid pressure collecting chamber (1). . Part of the fluid accelerated by gravity flows along the slope of the inlet (3) of the fluid pressure chamber and outside the turbine fluid discharge port (14), flows through the fluid negative pressure guide cover (15) and the fluid negative pressure discharge port (16), and flows in the direction The vehicle body runs behind the vehicle; when the airflow assist and airflow-assisted power generation facilities adopt the 13F working mode of the turbine-driven fluid inflow device surrounding the periphery of the turbine-driven blades (as shown in Figure 4.13F), part of the high-pressure fluid collected by the fluid pressure collecting chamber (1), The turbine driven fluid inflow device 13F around the periphery of the turbine driven blades is sprayed into the mixing cylinder B through the constriction nozzle A. The high-pressure fluid sprayed into the fluid pressure chamber (1) in the mixing cylinder B forms the turbine fluid driving surface through the turbine fluid driving nozzle C. The rear drive turbine drives the blades (9). Since the turbine driving fluid adopts the fluid driving surface mode, when the turbine initially driving fluid ejected from the constricted nozzle A flows through the mixing cylinder B and the turbine fluid driving nozzle C to form the turbine fluid driving surface, the flow rate will slow down. Because the gap between the turbine fluid driving nozzle C and the driven turbine is very small, and the fluid injected by the constriction nozzle A through the mixing cylinder B is the gravitational acceleration fluid of the vehicle body that has been introduced by the fluid pressure chamber (1) and has been continuously pressurized. The pressure is extremely high, and the extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the continued pressure of the fluid required to slow down the flow rate when the turbine fluid drives the nozzle C to form the turbine fluid driving surface. The fluid driving surface composed of numerous turbine fluid driving nozzles C that continuously maintain pressure, induced by the guide angle of the turbine fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, drives the turbine driving blade (9), and is driven by the driven turbine. The blades (9) drive the turbine shaft (11) to rotate through numerous invisible levers formed by the turbine bracket (12) and the turbine shaft (11). Since the turbine driving mode is a fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point. As the turbine shaft (11) rotates, the turbine driving fluid that drives the turbine driving blades (9) partially drives the turbine driving fluid of the turbine driving blades (9) under the separation of the fluid dividing plate D between the pressure increasing tank and the pressure reducing tank. The fluid flows into the supercharging tank due to the centrifugal phenomenon caused by the rotation of the turbine. Part of the turbine-driven fluid flowing into the supercharging tank gradually increases the density and pressure of the supercharging fluid in the supercharging tank. At the same time, the decompression groove is caused to rotate along with the turbine shaft (11), and the density of the turbine driving fluid in the decompression groove is weakened. The density of the memory turbine driving fluid in the pressure reducing groove is weakened, which reduces the resistance ability of the memory fluid in the pressure reducing groove to the turbine rotation when the pressure reducing groove is transferred to the next turbine fluid driving surface. As the density and pressure of the pressurized fluid flowing into the pressurized tank gradually increase, part of the high-pressure fluid in the fluid pressure chamber (1) is sprayed into the mixing cylinder B through the constricted nozzle A, because the fluid flow from the converging nozzle A There is a fluid inlet between the outlet and the fluid inlet of the mixing cylinder B, so when part of the high-pressure fluid in the fluid pressure chamber flows through the constricted nozzle A and is sprayed into the fluid inlet of the mixing cylinder B, the fluid inlet of the mixing cylinder B is The pressurized fluid in the peripheral part of the pressurizing tank is sucked into the mixing cylinder B through the fluid suction port. It is sucked into the pressurizing fluid in the inner part of the mixing cylinder B and the part of the high-pressure fluid in the pressure collecting chamber sprayed from the constricted nozzle A to form a high pressure. The mixed airflow is then sprayed out through the turbine fluid drive nozzle C, driving the turbine drive blades (9). The numerous invisible levers formed by the driven numerous turbine drive blades (9) through the turbine bracket (12) and the turbine shaft (11) will cause the turbine shaft (11) to rotate easily. As the turbine rotates, part of the pressurized fluid flowing into the pressurized groove is discharged through the pressurized fluid guide groove E.

Along the inner side of the inlet of the external deflector (not shown in the figure) and the fluid into the fluid inlet of the pressure tank (3), part of the gravity-accelerated fluid flows toward the opposite direction of the vehicle body from the lower part of the diversion slope, and drives the fluid inlet through the outside of the turbine (17 ), the external drive fluid filter (18) flows into the external drive fluid guide cover (19), and the gravity acceleration fluid flowing into the external drive fluid guide cover 19 is ejected through the external drive fluid outflow constriction nozzle (20) to drive the turbine Blade(9). In order to enable the numerous turbine fluid driven nozzles C in the turbine drive facility to discharge the numerous turbine driven fluids generated when driving the turbine to rotate as quickly as possible, the endmost turbine fluid driven surfaces of the numerous turbine fluid driven nozzles C are connected to the turbine external driven fluid in a constriction type fluid drive. There is a vacuum arc between the surfaces, and the flow rate of the external driving fluid of the turbine is used. While the external driving fluid drives the turbine driving blades (9), the external driving fluid and the numerous fluids injected into the turbine driving fluid inflow device 13F around the periphery of the turbine driving blades A weak pressure zone is formed between the turbine drive fluid and the pressurized fluid discharged from the pressurized fluid diversion channel E in the pressurized tank. The weak pressure zone causes the vacuum arc to generate a vacuum phenomenon. The vacuum adsorption phenomenon of the vacuum arc causes the surrounding turbine drive The numerous turbine driving fluids injected into the turbine driving fluid inflow device 13F on the blade periphery and the boosting fluid partially flowing through the boosting fluid guide slot E and discharged from the boosting grooves are sucked into the vacuum arc and flow into the external driving fluid. The turbine driving fluid mixes with the external driving fluid to form an external driving fluid with a greatly increased flow rate. The external driving fluid with a greatly increased flow speed drives the turbine driving blades (9) and then flows to the turbine fluid discharge port (14). At the same time, the pressurized fluid diversion groove E and other facilities are also produced to promote the flow pattern in which part of the pressurized fluid in the pressurized tank is sucked out, so that the reverse resistance produced by the pressurized fluid in the pressurized tank to the rotating turbine is very small. , it also maintains the pressure of the pressurized fluid in the pressurized tank, restricts the random discharge of a large amount of pressurized fluid in the pressurized tank, and creates a more reasonable reuse of secondary energy.

The flow rate of the fluid flowing along the outside of the external air deflector (not shown in the figure) to the opposite direction of the vehicle body. With the running speed of the vehicle body, it flows through the outside of the fluid negative pressure discharge port (16) and flows in the opposite direction of the vehicle body. A very ideal fluid negative pressure adsorption space is formed outside the open fluid negative pressure outlet (16). The fluid negative pressure adsorption space absorbs the weak pressure generated by numerous turbine-driven fluids and gravity acceleration fluids inside the fluid negative pressure guide cover (15). The adsorbed fluid passes through the fluid negative pressure discharge port (16) and is sucked into the negative pressure adsorption space behind the vehicle body. Along the inner side of the external deflector (not shown in the figure) and the fluid flows into the fluid manifold inlet (3) and under the deflection slope, part of the gravity acceleration fluid flows in the opposite direction to the movement of the vehicle body, and flows through the turbine fluid discharge port (14) and the fluid When the negative pressure guide cover (15) and numerous turbine-driven fluids and weak-pressure adsorption fluids flow into the negative pressure adsorption space behind the vehicle body through the fluid negative pressure outlet (16), they fill the negative pressure adsorption space behind the vehicle body. Some fluid is required to reduce the force of the vehicle body retracting backward caused by the adsorption space behind the vehicle body running.

When the airflow assisting device is working and the airflow assisting device is working, the turbine shaft (11) that rotates easily in the turbine drive device is transmitted by the assisting transmission device (23) to drive the bicycle driving wheel or drive shaft, forming an airflow-assisting device. Auxiliary power for power-assisted bicycles. When the auxiliary power of a moving bicycle needs to be reduced, use the fluid inflow interceptor cover adjustment device (25) to partially open the fluid inflow interceptor cover (8) and close part of the fluid inflow inlet (3) of the fluid inflow pressure chamber to reduce the inflow. The partial gravity in the fluid pressure collecting chamber (1) accelerates the inflow of the fluid, reduces the pressure of the after-pressure fluid flowing into the fluid pressure collecting chamber (1), and reduces some effects of the air flow assist facility.

When the moving bicycle does not need to use the airflow assist facility to work or the airflow assist facility fails, the fluid flows into the interceptor cover adjustment device (25) and the external driving fluid flows into the interceptor cover driving device (29) to flow the fluid into the interceptor cover (8) And the turbine external drive fluid inflow cut-off cover (21) is opened, the turbine drive fluid inflow port of the air flow assist facility is closed, and the work of the air flow assist facility is stopped.

Example 2 Electric power-assisted bicycle using airflow to assist power generation

The electric power-assisted bicycle that utilizes airflow to assist in power generation eliminates the power-assisted conduction device (23). As shown in Figure 2, when the electric power-assisted bicycle that utilizes airflow to assist in power generation is traveling, the airflow-assisted power generation facility is carried along the body (28) when working. The fluid flows in the opposite direction to the vehicle body from the inside of the inlet of the cover (not shown in the figure). The fluid flows through the rear part which is slightly lower than the front part. When the fluid flows into the slope of the inlet (3) of the fluid pressure chamber, a gravity-accelerated fluid with extremely high pressure is formed ( (Taken from the principle of aircraft flight), part of the gravity acceleration fluid flows into the fluid manifold inlet (3), the fluid filter (6), the fluid flows into the deflector (7), and the inflow fluid flows into the deflector (7) The fluid accelerated by gravity flows into the fluid pressure tank (1) through the fluid dust collection net (5), the fluid inflow into the fluid pressure tank deflector (4), and the fluid inflow into the fluid pressure tank (1). The subsequent inflow of gravity The accelerating fluid quickly forms a high-pressure accumulating fluid in the fluid accumulating chamber (1). Part of the fluid accelerated by gravity flows along the slope of the inlet (3) of the fluid pressure chamber and outside the turbine fluid discharge port (14), flows through the fluid negative pressure guide cover (15) and the fluid negative pressure discharge port (16), and flows in the direction The vehicle body runs behind the vehicle; when the airflow assist and airflow-assisted power generation facilities adopt the 13F working mode of the turbine-driven fluid inflow device surrounding the periphery of the turbine-driven blades (as shown in Figure 4.13F), part of the high-pressure fluid collected by the fluid pressure collecting chamber (1), The turbine driven fluid inflow device 13F around the periphery of the turbine driven blades is sprayed into the mixing cylinder B through the constriction nozzle A. The high-pressure fluid sprayed into the fluid pressure chamber (1) in the mixing cylinder B forms the turbine fluid driving surface through the turbine fluid driving nozzle C. The rear drive turbine drives the blades (9). Since the turbine driving fluid adopts the fluid driving surface mode, when the turbine initially driving fluid ejected from the constricted nozzle A flows through the mixing cylinder B and the turbine fluid driving nozzle C to form the turbine fluid driving surface, the flow rate will slow down. Because the gap between the turbine fluid driving nozzle C and the driven turbine is very small, and the fluid injected by the constriction nozzle A through the mixing cylinder B is the gravitational acceleration fluid of the vehicle body that has been introduced by the fluid pressure chamber (1) and has been continuously pressurized. The pressure is extremely high, and the extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the continued pressure of the fluid required to slow down the flow rate when the turbine fluid drives the nozzle C to form the turbine fluid driving surface. The fluid driving surface composed of numerous turbine fluid driving nozzles C that continuously maintain pressure, induced by the guide angle of the turbine fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, drives the turbine driving blade (9), and is driven by the driven turbine. The blades (9) drive the turbine shaft (11) to rotate through numerous invisible levers formed by the turbine bracket (12) and the turbine shaft (11). Since the turbine driving mode is a fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point. As the turbine shaft (11) rotates, the turbine driving fluid that drives the turbine driving blades (9) partially drives the turbine driving fluid of the turbine driving blades (9) under the separation of the fluid dividing plate D between the pressure increasing tank and the pressure reducing tank. The fluid flows into the supercharging tank due to the centrifugal phenomenon caused by the rotation of the turbine. Part of the turbine-driven fluid flowing into the supercharging tank gradually increases the density and pressure of the supercharging fluid in the supercharging tank. At the same time, the decompression groove is caused to rotate along with the turbine shaft (11), and the density of the turbine driving fluid in the decompression groove is weakened. The density of the memory turbine driving fluid in the pressure reducing groove is weakened, which reduces the resistance ability of the memory fluid in the pressure reducing groove against the rotation of the turbine when the pressure reducing groove is transferred to the next turbine fluid driving surface. As the density and pressure of the pressurized fluid flowing into the pressurized tank gradually increase, part of the high-pressure fluid in the fluid pressure chamber (1) is sprayed into the mixing cylinder B through the constricted nozzle A, because the constricted nozzle There is a fluid suction port between the fluid outlet of nozzle A and the fluid inlet of mixing cylinder B. Therefore, when part of the high-pressure fluid in the fluid pressure collecting chamber flows through the constricted nozzle A and is sprayed into the fluid inlet of mixing cylinder B, the mixture will The pressurized fluid in the pressurizing groove around the fluid inlet of cylinder B is sucked into the mixing cylinder B through the fluid suction port, and is sucked into the fluid collecting chamber where the pressurized fluid in the pressurizing groove in the inner part of the mixing cylinder B and the constricted nozzle A are sprayed Part of the high-pressure fluid forms a high-pressure mixed airflow and is ejected through the turbine fluid drive nozzle C to drive the turbine drive blades (9). The numerous invisible levers formed by the driven turbine drive blades (9) through the turbine bracket (12) and the turbine shaft (11) will cause the turbine shaft (11) to rotate easily. As the turbine rotates, part of the pressurized fluid flowing into the pressurized groove is discharged through the pressurized fluid guide groove E.

The flow rate of the fluid flowing along the outside of the external air deflector (not shown in the figure) to the opposite direction of the vehicle body. With the running speed of the vehicle body, it flows through the outside of the fluid negative pressure discharge port (16) and flows in the opposite direction of the vehicle body. A very ideal fluid negative pressure adsorption space is formed outside the open fluid negative pressure outlet (16), and the fluid negative pressure adsorption space guides the fluid negative pressure. The weak-pressure adsorption fluid generated by numerous turbine-driven fluids and gravity-accelerated fluids inside the cover (15) passes through the fluid negative pressure outlet (16) and is sucked into the negative-pressure adsorption space behind the running vehicle body. Along the inner side of the external deflector (not shown in the figure) and the fluid flows into the fluid manifold inlet (3) and under the deflection slope, part of the gravity acceleration fluid flows in the opposite direction to the movement of the vehicle body, and flows through the turbine fluid discharge port (14) and the fluid When the negative pressure guide cover (15) and numerous turbine-driven fluids and weak-pressure adsorption fluids flow into the negative pressure adsorption space behind the vehicle body through the fluid negative pressure outlet (16), they fill the negative pressure adsorption space behind the vehicle body. Some fluid is required to reduce the force of the vehicle body retracting backward caused by the adsorption space behind the vehicle body running.

The drive motor (26) is driven manually or by the electric energy of the battery (24). When the electric power-assisted bicycle is traveling and the air flow is used to assist the power generation facility in operation, the turbine shaft (11) that rotates easily in the turbine drive facility drives the generator. (22) Generate electrical energy. Under the control of the electric energy control device (27), the electric energy generated by the generator (22) is combined with the electric energy of the battery (24) to drive the drive motor (26), forming a new supply of electric energy for the drive motor of the electric power-assisted bicycle that uses airflow to assist in power generation. model. As the running speed of the vehicle body increases, and as the power generation energy generated by the air flow-assisted power generation facility increases, when the driving capacity of the drive motor (26) reaches the speed required for the vehicle body operation, the artificial driving force is cancelled. When the amount of electricity generated by the generator (22) reaches the electric energy required to drive the motor (26) and other tasks, the electric energy control device (27) will automatically stop the electric energy output of the battery (24). When the electric energy generated by the generator (22) exceeds the electric energy required to drive the motor (26) and other tasks, the excess generated electric energy generated by the generator (22) charges the battery (24) through the electric energy regulating device (27). When the driving motor (26) stops working, the main function of the electric energy generated by the generator (22) is to charge the battery (24) through the electric energy regulating device (27).

When the generator fails or the airflow-assisted power generation facility fails, and the airflow-assisted power generation facility needs to stop working, the fluid flows into the interceptor cover adjustment device (25) and the external drive fluid flows into the interceptor cover driving device (29) to flow the fluid into the interceptor cover. (8) and the external drive fluid inflow interceptor cover (21) are opened to close the turbine drive fluid inflow inlet of the air flow-assisted power generation facility, and stop the operation of the air flow-assisted power generation facility.

Example 3 Using airflow to assist in power generation for electric motorcycles

The electric motorcycle that utilizes airflow to assist power generation eliminates the power-assisted conduction device (23). As shown in Figure 3, when the electric motorcycle that utilizes airflow to assist power generation is traveling, the airflow-assisted power generation facility is carried along the body (28) when working. The fluid flows in the opposite direction to the vehicle body from the inside of the inlet of the cover (not shown in the figure). The fluid flows through the rear part which is slightly lower than the front part. When the fluid flows into the slope of the inlet (3) of the fluid pressure chamber, a gravity-accelerated fluid with extremely high pressure is formed ( (Taken from the principle of aircraft flight), part of the gravity acceleration fluid flows into the fluid manifold inlet (3), the fluid filter (6), the fluid flows into the deflector (7), and the inflow fluid flows into the deflector (7) The fluid accelerated by gravity flows into the fluid pressure tank (1) through the fluid dust collection net (5), the fluid inflow into the fluid pressure tank deflector (4), and the fluid inflow into the fluid pressure tank (1). The subsequent inflow of gravity The accelerating fluid quickly forms a high-pressure accumulating fluid in the fluid accumulating chamber (1). Part of the fluid accelerated by gravity flows along the slope of the inlet (3) of the fluid pressure chamber and outside the turbine fluid discharge port (14), flows through the fluid negative pressure guide cover (15) and the fluid negative pressure discharge port (16), and flows in the direction The vehicle body runs behind the vehicle; when the airflow assist and airflow-assisted power generation facilities adopt the 13F working mode of the turbine-driven fluid inflow device surrounding the periphery of the turbine-driven blades (as shown in Figure 4.13F), part of the high-pressure fluid collected by the fluid pressure collecting chamber (1), The turbine driven fluid inflow device 13F around the periphery of the turbine driven blades is sprayed into the mixing cylinder B through the constriction nozzle A. The high-pressure fluid sprayed into the fluid pressure chamber (1) in the mixing cylinder B forms the turbine fluid driving surface through the turbine fluid driving nozzle C. The rear drive turbine drives the blades (9). Since the turbine driving fluid adopts the fluid driving surface mode, when the turbine initially driving fluid ejected from the constricted nozzle A flows through the mixing cylinder B and the turbine fluid driving nozzle C to form the turbine fluid driving surface, the flow rate will slow down. Because the gap between the turbine fluid driving nozzle C and the driven turbine is very small, and the fluid injected by the constriction nozzle A through the mixing cylinder B is the gravitational acceleration fluid of the vehicle body that has been introduced by the fluid pressure chamber (1) and has been continuously pressurized. The pressure is extremely high, and the extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the continued pressure of the fluid required to slow down the flow rate when the turbine fluid drives the nozzle C to form the turbine fluid driving surface. The fluid driving surface composed of numerous turbine fluid driving nozzles C that continuously maintain pressure, induced by the guide angle of the turbine fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, drives the turbine driving blade (9), and is driven by the driven turbine. The blades (9) drive the turbine shaft (11) to rotate through numerous invisible levers formed by the turbine bracket (12) and the turbine shaft (11). Since the turbine drive mode is Fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point. As the turbine shaft (11) rotates, the turbine driving fluid that drives the turbine driving blades (9) partially drives the turbine driving fluid of the turbine driving blades (9) under the separation of the fluid dividing plate D between the pressure increasing tank and the pressure reducing tank. The fluid flows into the supercharging tank due to the centrifugal phenomenon caused by the rotation of the turbine. Part of the turbine-driven fluid flowing into the supercharging tank gradually increases the density and pressure of the supercharging fluid in the supercharging tank. At the same time, the decompression groove is caused to rotate along with the turbine shaft (11), and the density of the turbine driving fluid in the decompression groove is weakened. The density of the memory turbine driving fluid in the pressure reducing groove is weakened, which reduces the resistance ability of the memory fluid in the pressure reducing groove against the rotation of the turbine when the pressure reducing groove is transferred to the next turbine fluid driving surface. As the density and pressure of the pressurized fluid flowing into the pressurized tank gradually increase, part of the high-pressure fluid in the fluid pressure chamber (1) is sprayed into the mixing cylinder B through the reduced-nozzle A, because the fluid flow from the reduced-nozzle A There is a fluid inlet between the outlet and the fluid inlet of the mixing cylinder B, so when part of the high-pressure fluid in the fluid pressure chamber flows through the constricted nozzle A and is sprayed into the fluid inlet of the mixing cylinder B, the fluid inlet of the mixing cylinder B is The pressurized fluid in the peripheral part of the pressurizing tank is sucked into the mixing cylinder B through the fluid suction port. It is sucked into the pressurizing fluid in the inner part of the mixing cylinder B and the part of the high-pressure fluid in the pressure collecting chamber sprayed from the constricted nozzle A to form a high pressure. The mixed airflow is then sprayed out through the turbine fluid drive nozzle C, driving the turbine drive blades (9). The numerous invisible levers formed by the driven turbine drive blades (9) through the turbine bracket (12) and the turbine shaft (11) will cause the turbine shaft (11) to rotate easily. As the turbine rotates, part of the pressurized fluid flowing into the pressurized groove is discharged through the pressurized fluid guide groove E.

Along the inner side of the inlet of the external deflector (not shown in the figure) and the fluid inlet of the fluid collecting tank (3), part of the gravity-accelerated fluid flows from the lower part of the deflector slope toward the opposite direction of the vehicle body, and flows through the turbine fluid discharge port (14) When the fluid flows from the outside to the inside of the negative pressure guide cover (15), the fluid density and flow rate due to gravity acceleration are extremely high, forming a weak pressure adsorption fluid on the outside of the turbine fluid outlet (14). The weak pressure adsorption fluid induces numerous turbine driven fluids to pass through the turbine fluid When the fluid flows into the negative pressure guide cover (15) from the discharge port (14), the weak pressure adsorption fluid causes the flow rate of the external driving fluid to further increase greatly. The weak pressure adsorption ability prompts the external driving fluid to absorb more of the numerous turbine driving fluids injected into the turbine driving fluid inflow device 13F around the periphery of the turbine driving blades and the pressurized fluid discharged from the pressurized fluid diversion groove E through part of the pressurized tank. It is sucked into the vacuum arc and flows into the external driving fluid, thereby further improving the fluid driving ability of the external driving fluid, and at the same time, more turbine driving fluid surrounding the periphery of the turbine driving blades flows into the numerous turbine driving fluids and booster grooves injected by the device 13F The middle part of the pressurized fluid discharged through the pressurized fluid guide groove E is induced by the external driving fluid to flow to the turbine fluid discharge port (14), and then flows along the external guide cover (in the figure). (not shown) inside the inlet and the fluid flows into the lower part of the guide slope of the fluid manifold inlet (3), flows through the turbine fluid outlet (14) and flows to the inside of the negative pressure guide cover (15). Under the adsorption of pressure adsorption fluid, the weak pressure adsorption fluid generated by numerous turbine driven fluids and gravity acceleration fluid flows to the fluid negative pressure discharge port (16).

The electric energy of the battery (24) drives the drive motor (26) and uses airflow to assist in generating electricity. When the electric motorcycle is running and the airflow assists the power generation facility in working, the turbine shaft (11) that rotates easily in the turbine drive facility drives the generator (22) to generate electricity. electrical energy. The electric energy generated by the generator (22) is transmitted to the driving motor (26) through the electric energy regulating device (27), forming auxiliary electric energy for the electric motorcycle that uses airflow to assist in power generation. When the electric energy generated by airflow-assisted power generation can meet the required operating electric energy for driving the motor (26) and the like, the electric energy control device (27) will automatically stop the electric energy output of the battery (24). When the electric energy generated by air flow-assisted power generation exceeds the electric energy required for driving the motor (26) and other tasks, the excess electric energy charges the battery (24) through the electric energy regulating device (27). When the driving motor (26) stops working and does not require electric energy, the main function of the electric energy generated by the generator (22) is to charge the battery (24) through the electric energy regulating device (27).

Air-assisted bicycles and air-assisted power generation electric power-assisted bicycles or air-assisted power generation electric motorcycles carrying air-assisted or air-assisted power generation facilities adopt the working mode of the turbine-driven fluid inflow device 13G surrounding the periphery of the turbine-driven blades (such as Figure 4.13G), the difference between them and the working mode of the turbine driving fluid inflow device 13F surrounding the periphery of the turbine driving blades is that the mixing cylinder B and the pressurized fluid guide groove E are eliminated. The fluid outflow port of the constricted nozzle A and the fluid inlet port of the turbine fluid drive nozzle C are connected to each other. When the vehicle body is running, airflow is used to assist or the power generation facility is operated using airflow, part of the high-pressure fluid collected in the fluid pressure chamber (1) is sprayed into the reduced nozzle A in the turbine-driven fluid inflow device 13G surrounding the periphery of the turbine-driven blades. Turbine drive nozzle C, because the turbine drive fluid adopts the fluid drive surface mode, the flow rate will slow down when the turbine initial drive fluid ejected from the constricted nozzle A flows into the turbine fluid drive nozzle C to form the turbine fluid drive surface. Since the gap between the turbine fluid driving nozzle C and the driven turbine is very small, the fluid outflow port of the reduced port nozzle A and the fluid inlet port of the turbine fluid driven nozzle C are connected to each other, and the fluid injected by the reduced port nozzle A is pressure-collected by the fluid. The pressure of the gravitational acceleration fluid introduced into the cabin (1) after continued pressurization is extremely high, and the extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the turbine fluid drive nozzle C to form the turbine fluid drive surface. The continued pressure of the fluid required for the flow slowdown phenomenon. The fluid driving surface composed of numerous turbine fluid driving nozzles C with constant pressure, induced by the flow direction angle of the fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, drives the turbine driving blades (9), and the numerous driven turbines The numerous invisible levers formed by the drive blades (9) via the turbine bracket (12) and the turbine shaft (11) will allow the turbine shaft (11) to rotate easily. As the turbine shaft (11) rotates, The turbine driving fluid that drives the turbine driving blades (9) partially drives the turbine driving fluid that drives the turbine driving blades (9) under the divergence of the fluid dividing plate D between the pressure increasing tank and the pressure reducing tank. The centrifugal phenomenon occurs as the turbine rotates. Part of the turbine driving fluid flowing into the supercharging groove and the turbine driving fluid ejected from the numerous turbine fluid driving nozzles C flow to the most terminal fluid driving surface of the numerous turbine fluid driving nozzles C and the turbine external driving fluid constriction type fluid The vacuum arc provided between the driving surfaces utilizes the flow velocity of the external driving fluid of the turbine. While the external driving fluid drives the turbine driving blades (9), the external driving fluid and the peripheral turbine driving fluid surrounding the turbine driving blades are injected into the device 13G. A weak pressure zone is formed between numerous turbine driving fluids and part of the turbine driving fluid flowing into the supercharging tank. The weak pressure zone causes the vacuum arc to generate a vacuum phenomenon. The vacuum adsorption phenomenon of the vacuum arc causes the turbine driving fluid surrounding the periphery of the turbine driving blades to flow into the device 13G. The numerous turbine driving fluids injected and part of the turbine driving fluid flowing into the supercharging tank are sucked into the vacuum arc and flow into the external driving fluid. The numerous turbine driving fluids flowing into the external driving fluid mix with the external driving fluid to form an external driving fluid with a greatly increased flow rate. The external driving fluid with a greatly increased flow speed drives the turbine driving blades (9) and then flows to the turbine fluid discharge port (14). At the same time, as the turbine shaft (11) rotates, the density of the turbine driving fluid in the decompression groove is weakened, which reduces the force generated by the fluid in the decompression groove against the rotation of the turbine when the decompression groove is transferred to the next turbine fluid driving surface. Blocking ability. Since the turbine driving mode is a fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point. Bicycles that use airflow to assist and electric power-assisted bicycles that use airflow to assist power generation or electric motorcycles that use airflow to assist power generation, when using the turbine-driven fluid inflow device 13G around the periphery of the turbine drive blades, there is no need to use the turbine-driven fluid inflow device 13F around the periphery of the turbine drive blades. Reuse of part of the turbine drive fluid in the boost tank during operating mode.

Claims

According to the specific application of the law of conservation of energy, Bernoulli's theorem has long told people: when fluid flows in a pipe, wherever the flow rate is high, the pressure is small; where the flow rate is small, the pressure is high; according to Bernoulli's theorem , when air flows in a pipe, wherever the flow rate is high, the pressure is small; wherever the flow rate is small, the pressure is high; according to the fluid continuity theorem: when air flows in a pipe, wherever the pipe is thin, the flow rate is large ; Where the pipe is thick, the flow rate is small; combining the above two points, we can draw the following preliminary conclusion: When air flows in the pipe, wherever the pipe is thin, the flow rate is large and the pressure is small; conversely, wherever the pipe is Where it is thicker, the flow speed is smaller and the pressure is larger. With the help of this conclusion, we can preliminarily explain the reason for the lift force on the wing. During the flight of the airplane, the gravity acceleration fluid flows along the lower part of the wing of the airplane in the opposite direction of the flight of the airplane, forming an airplane. The lifting force of the wing; the lifting force of the aircraft wing is a very huge natural energy, which generates the collection and reuse of gravity acceleration fluid flowing along the bottom of the moving object in the opposite direction of the moving object, which can produce a lift similar to that of the aircraft wing. The huge natural energy of force forms a power source for moving objects carrying turbine rotating facilities, forming a very practical driving force for moving objects carrying turbine rotating facilities; during the flight of an aircraft, the wings overcome the flow along the wings of the fluid in the opposite direction of the aircraft flight. The design pattern of forming a weak-pressure adsorption space in the opposite direction of aircraft flight is an excellent induction pattern for adsorbing moving objects carrying multiple fluid-driven surfaces in turbine rotating facilities to form numerous turbine-driven fluids. A new type of weak-pressure adsorption space with multiple fluid-driven surfaces The design and practical application of adsorption fluid-driven power machinery is feasible and can be implemented in the use of air flow assistance and auxiliary power generation facilities;

The use of air flow assist and auxiliary power generation facilities is applied in the use of air flow to assist bicycles, the use of air flow to assist in power generation, electric power assist bicycles, or the use of air flow to assist in power generation of electric motorcycles. It mainly involves: from top to bottom along the inside of the external deflector, it is divided into fluid pressure collection Cabin pressure gathering facilities, turbine drive facilities, and fluid negative pressure induction facilities, as well as generators, power transmission devices, batteries, drive motors, electric energy control devices, and induction vehicle bodies;

The fluid pressure collecting facility is mainly composed of: a fluid pressure collecting chamber arranged around the periphery of the turbine drive blades of the turbine driven fluid inflow device 13F or 13G. The fluid arranged on both sides of the turbine driving facility flows into the fluid pressure collecting chamber constriction. Fluid inflow guide cover, fluid dust collection screen, fluid inflow guide cover, fluid filter screen, fluid inflow into the fluid pressure bin inlet, fluid inflow interceptor cover, fluid inflow interceptor cover adjustment device, and external flow guide cover composition;

The turbine drive facility mainly includes: turbine drive blades, turbine casing, turbine shaft, turbine bracket. The turbine drive fluid inflow device 13F is provided with multiple constriction nozzles A, mixing cylinder B, turbine fluid drive nozzle C, surrounding the periphery of the turbine drive blades. The fluid dividing plate D between the pressure increasing tank and the pressure reducing tank is provided with a pressurizing fluid diversion groove E. A fluid suction port is provided between the fluid outflow port of the constricted nozzle A and the fluid inlet of the mixing cylinder B. The mixing cylinder B The fluid outflow port is interconnected with the fluid inlet of the turbine fluid drive nozzle C; and the turbine drive fluid inflow device 13G is provided with a plurality of constriction nozzles A, turbine fluid drive nozzles C, boosting grooves and pressure reducing devices around the periphery of the turbine drive blades. The groove fluid dividing plate D, the fluid outlet of the constriction nozzle A and the fluid inlet of the turbine fluid drive nozzle C are connected to each other; a turbine fluid outlet, a turbine external drive fluid inlet, an external drive fluid filter, and an external drive are provided. Fluid guide cover, the external drive fluid flows out of the constriction nozzle, the external drive fluid flows into the interceptor cover, the external drive fluid flows into the interceptor cover driving device, and the external guide cover; there is a decompression groove on the inside of the turbine drive blade and a pressure increase groove on the outside ; Turbine fluid drive, using fluid drive surface mode;

The fluid negative pressure induction facilities include: turbine external driving fluid, gravity acceleration weak pressure adsorption fluid, fluid negative pressure deflector, fluid negative pressure discharge port, and fluid flowing along the outer side of the external deflector in the opposite direction of the vehicle body;

Bicycles that use airflow to assist and electric power-assisted bicycles that use airflow to assist power generation or electric motorcycles that use airflow to assist power generation are running. When the vehicle body is carrying airflow assistance or using airflow to assist power generation facilities, the flow flows toward the vehicle body along the inside of the inlet of the external air deflector. The fluid flows in the opposite direction, and the rear part is slightly lower than the front part. When the fluid flows into the inlet inlet slope of the fluid pressure chamber, a gravity-accelerated fluid with extremely high pressure is formed. Part of the gravity-accelerated fluid flows into the inlet of the fluid pressure chamber through the fluid, and the fluid passes through The fluid flowing into the filter screen flows into the deflector, and the gravity acceleration fluid flowing into the deflector passes through the fluid dust collection net, the fluid flows into the fluid collecting chamber deflector, and the fluid flows into the fluid collecting chamber shrinkage and flows into the fluid collecting chamber. The subsequent inflow of gravity-accelerated fluid quickly forms a high-pressure concentrated fluid in the fluid pressure chamber; part of the gravity-accelerated fluid flows along the inlet slope of the fluid pressure chamber and outside the turbine fluid outlet, and flows through the fluid negative pressure diversion cover and the fluid negative pressure outlet, flowing to the rear of the vehicle body; using airflow to assist and using airflow to assist power generation facilities, the turbine-driven fluid inflow device surrounding the periphery of the turbine-driven blades is used. In the 13F working mode, part of the high-pressure fluid collected in the fluid pressure chamber, The turbine driven fluid inflow device 13F around the periphery of the turbine drive blade is sprayed into the mixing cylinder B through the constriction nozzle A. The high-pressure fluid sprayed into the fluid pressure chamber in the mixing cylinder B forms a turbine fluid driving surface through the turbine fluid driving nozzle C and then drives the turbine. Drive blades; since the turbine driving fluid adopts the fluid driving surface mode, when the turbine initially driving fluid ejected from the constricted nozzle A flows through the mixing cylinder B and the turbine fluid driving nozzle C to form the turbine fluid driving surface, the flow rate will slow down. ; Because the gap between the turbine fluid driving nozzle C and the driven turbine is very small, and the fluid injected by the constriction nozzle A through the mixing cylinder B is the pressure of the fluid caused by the continuous pressure of the vehicle body running gravity acceleration introduced by the fluid pressure chamber. The extremely high flow rate of the fluid produced by the extremely high pressure fluid will quickly complete the continuous pressure of the fluid required for the flow rate to slow down when the turbine fluid drive nozzle C forms the turbine fluid driving surface; numerous turbine fluid drives that continue to maintain pressure The fluid driving surface formed by the nozzle C, induced by the diversion angle of the turbine fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine and drives the turbine driving blades. The driven turbine driving blades pass through numerous invisible structures formed by the turbine bracket and the turbine shaft. The lever drives the turbine shaft to rotate; since the turbine drive mode is a fluid drive surface, the turbine fluid driving force generated by the numerous turbine fluid drive surfaces created by the numerous turbine fluid drive nozzles C should be much higher than the turbine fluid generated by the traditional fluid drive point. Driving force; as the turbine shaft rotates, the turbine drive fluid that drives the turbine drive blades partially drives the turbine drive fluid that drives the turbine drive blades as the turbine rotates due to the divergence of the fluid separation plate D between the pressure increasing tank and the pressure reducing tank. The centrifugal phenomenon generated flows into the supercharging tank, and part of the turbine driving fluid flowing into the supercharging tank causes the density and pressure of the supercharging fluid in the supercharging tank to gradually increase; at the same time, the decompression tank rotates with the rotation of the turbine shaft, and the pressure in the decompression tank increases. The density of the memory turbine driving fluid is weakened; the density of the memory turbine driving fluid in the pressure reducing groove is weakened, which reduces the resistance ability of the memory fluid in the pressure reducing groove against the rotation of the turbine when the pressure reducing groove is transferred to the next turbine fluid driving surface; as The density and pressure of the pressurized fluid flowing into the pressurizing tank gradually increase. When part of the high-pressure fluid in the fluid pressure chamber is sprayed into the mixing cylinder B through the constricted nozzle A, the fluid outlet of the converging nozzle A is in contact with the mixing cylinder B. There is a fluid suction port between the fluid inflow ports, so when part of the high-pressure fluid in the fluid pressure chamber flows through the constricted nozzle A and is sprayed into the fluid inlet of the mixing cylinder B, the peripheral part of the fluid inlet of the mixing cylinder B is pressurized into the tank. The internal pressurized fluid is sucked into the mixing cylinder B through the fluid suction port, and is sucked into the pressurizing tank in the inner part of the mixing cylinder B. The pressurized fluid and the fluid sprayed from the constricted nozzle A form a high-pressure mixed airflow in the pressure collecting chamber and then pass through the turbine. The fluid drives the nozzle C to eject, driving the turbine drive blades; the many driven turbine drive blades pass through the many invisible levers formed by the turbine bracket and the turbine shaft, causing the turbine shaft to rotate easily; as the turbine rotates, the part flowing into the supercharging groove The pressurized fluid is discharged through the pressurized fluid diversion groove E;

Part of the gravity-accelerated fluid flows along the inner side of the inlet of the external shroud and the inlet of the fluid into the pressure tank and under the diversion slope toward the opposite direction of the vehicle body. It flows into the external drive fluid guide through the turbine external drive fluid inlet and the external drive fluid filter. Flow cover, the gravitational acceleration fluid flowing into the external drive fluid guide cover is ejected through the external drive fluid outflow constriction nozzle, driving the turbine drive blade; in order to promote the numerous turbine fluid drive nozzles C in the turbine drive facility to generate numerous fluids when driving the turbine to rotate. The turbine drive fluid can be discharged as quickly as possible. There is a vacuum arc between the turbine fluid drive surface at the end of the turbine fluid drive nozzles C and the turbine external drive fluid constriction fluid drive surface. The flow rate of the turbine external drive fluid is used to drive the turbine externally. While the fluid drives the turbine drive blades, the external drive fluid and the numerous turbine drive fluids injected into the turbine drive fluid inflow device 13F around the periphery of the turbine drive blades and the pressurized fluid partially flowing through the pressurized fluid guide groove E in the pressurized grooves are discharged. A weak pressure zone is formed between them. The weak pressure zone causes the vacuum arc to produce a vacuum phenomenon. The vacuum adsorption of the vacuum arc This phenomenon causes numerous turbine drive fluids injected into the turbine drive fluid inflow device 13F around the periphery of the turbine drive blades and the pressurized fluid discharged from the pressurized fluid diversion channel E partially flowing through the pressurized fluid guide grooves to be sucked into the vacuum arc and flow into the external drive fluid. The numerous turbine driving fluids of the external driving fluid mix with the external driving fluid to form an external driving fluid with a huge flow rate; the external driving fluid with a huge flow rate drives the turbine drive blades and then flows to the turbine fluid discharge port; at the same time, a pressurized fluid guide groove E is produced and other facilities to promote the flow pattern in which part of the pressurized fluid in the pressurized tank is sucked out, so that the reverse resistance produced by the pressurized fluid in the pressurized tank on the rotating turbine is very small, and the pressurization in the supercharged tank is maintained. The pressure of the fluid restricts the random discharge of a large amount of pressurized fluid in the pressurized tank, creating more reasonable secondary energy reuse;

When the fluid flows along the inner side of the external deflector inlet and the lower part of the deflection slope of the fluid manifold inlet, it flows in the opposite direction to the vehicle body. When it flows through the outside of the turbine fluid discharge port and flows to the inside of the fluid negative pressure deflector, due to The fluid density and flow rate accelerated by gravity are extremely high, forming a weak pressure adsorption fluid outside the turbine fluid discharge port. The weak pressure adsorption fluid induces numerous turbine driven fluids to flow into the fluid negative pressure guide cover through the turbine fluid discharge port. At the same time, the weak pressure adsorption fluid increases the flow rate. The greatly increased flow rate of the external driving fluid will further increase significantly. The further increased flow rate of the external driving fluid generates a huge increase in the weak pressure adsorption capacity, prompting the external driving fluid to absorb more surrounding turbine drive blades and the turbine drive fluid flows into the device 13F The numerous turbine drive fluids injected and the pressurized fluid discharged from the pressurized fluid diversion channel E in the pressurized tank are sucked into the vacuum arc and flow into the external drive fluid, thus further improving the fluid drive capability of the external drive fluid. At the same time, Prompting more turbine drive fluid around the periphery of the turbine drive blades, the numerous turbine drive fluids injected into the device 13F and the pressurized fluid partially flowing through the pressurized fluid guide groove E in the pressurized grooves flow to the turbine under the induction of the external drive fluid. After the fluid is discharged, it flows along the inside of the inlet of the external guide cover and the lower part of the guide slope of the inlet of the fluid collecting tank. It flows through the outside of the turbine fluid discharge port and flows to the inside of the negative pressure guide cover. The weak acceleration of the fluid caused by gravity is Under the adsorption of pressure adsorption fluid, the weak pressure adsorption fluid generated by numerous turbine driven fluids and gravity acceleration fluid flows to the fluid negative pressure discharge port;

The fluid flowing along the outside of the external air deflector in the opposite direction of the vehicle body will flow along the outside of the negative pressure outlet of the vehicle as the vehicle body moves in the opposite direction. When the fluid flows in the opposite direction of the vehicle body, the flow rate of the fluid will be outside the open fluid negative pressure outlet. A very ideal fluid negative pressure adsorption space is formed. In the fluid negative pressure adsorption space, the weak pressure adsorption fluid generated by numerous turbine-driven fluids and gravity acceleration fluids inside the fluid negative pressure guide cover is sucked into the rear of the vehicle body through the fluid negative pressure outlet. Negative pressure adsorption space; along the inner side of the external deflector and the lower part of the deflection slope where the fluid flows into the fluid header inlet, the gravity-accelerated fluid flows in the opposite direction to the movement of the vehicle body, flows through the turbine fluid outlet and the fluid negative pressure deflector, and When many turbine-driven fluids and weak-pressure adsorption fluids flow into the negative pressure adsorption space behind the vehicle body through the fluid negative pressure outlet, they fill some of the fluid required for the negative pressure adsorption space behind the vehicle body and reduce the risk of damage caused by the adsorption space behind the vehicle body. The force of the car body retracting backward;

When airflow-assisted bicycles and airflow-assisted power generation electric power-assisted bicycles or airflow-assisted power generation electric motorcycles carry airflow-assisted or airflow-assisted power generation facilities, when the working mode of the turbine-driven fluid inflow device 13G is adopted around the periphery of the turbine-driven blades, they The difference from the working mode of the turbine driven fluid inflow device 13F surrounding the periphery of the turbine driven blades is that the mixing cylinder B and the pressurized fluid guide groove E are eliminated; the fluid flow between the fluid outlet of the constricted nozzle A and the turbine fluid driven nozzle C is eliminated. The inlets are connected to each other; when the vehicle body is running and the air flow is used to assist or the air flow is used to assist the operation of the power generation facility, part of the high-pressure fluid collected in the fluid pressure chamber is sprayed through the reduced nozzle A in the turbine drive fluid inflow device 13G around the periphery of the turbine drive blades. Entering the turbine drive nozzle C, since the turbine drive fluid adopts the fluid drive surface mode, the turbine initially driven fluid ejected from the constricted nozzle A flows into the turbine fluid drive nozzle C to form the turbine fluid drive surface, and the flow rate slows down; due to The gap between the turbine fluid driving nozzle C and the driven turbine is very small, because the fluid outlet of the constricted nozzle A and the fluid inlet of the turbine fluid driven nozzle C are connected to each other, and the fluid injected by the converging nozzle A is from the fluid pressure chamber. The pressure of the gravity acceleration fluid introduced by the vehicle body after the continued pressure is extremely high, and the extremely high flow rate of the fluid generated by the extremely high pressure fluid will quickly complete the turbine fluid drive nozzle C to form the turbine fluid drive surface. The continuous pressure of the fluid required for the current flow slowdown phenomenon; the fluid driving surface composed of numerous turbine fluid driving nozzles C that continue to maintain pressure, is induced by the diversion angle of the fluid driving surface, overcomes the torque in the opposite direction generated by the driven turbine, and drives the turbine Driving blades, the numerous invisible levers formed by the turbine bracket and the turbine shaft will cause the turbine shaft to rotate easily; as the turbine shaft rotates, the turbine driving fluid that drives the turbine driving blades passes between the booster tank and the reducer. Under the diversion of the pressure groove fluid partition plate D, part of the turbine drive fluid that drives the turbine drive blades flows into the supercharger tank due to the centrifugal phenomenon caused by the rotation of the turbine. Part of the turbine drive fluid that flows into the supercharger tank mixes with the numerous turbine fluid drive nozzles C. The jetted turbine drive fluid flows to the vacuum arc provided between the final fluid drive surface of the numerous turbine fluid drive nozzles C and the turbine external drive fluid constriction fluid drive surface. The flow rate of the turbine external drive fluid is used to drive the turbine externally. While the fluid drives the turbine drive blades, a weak pressure zone is formed between the external drive fluid and the numerous turbine drive fluids injected into the turbine drive fluid inflow device 13G around the periphery of the turbine drive blades and part of the turbine drive fluid flowing into the booster tank. The vacuum arc causes the vacuum arc to generate a vacuum phenomenon. The vacuum adsorption phenomenon of the vacuum arc causes numerous turbine drive fluids injected into the turbine drive fluid inflow device 13G around the periphery of the turbine drive blades and part of the turbine drive fluid flowing into the booster tank to be sucked into the vacuum arc and flow outside. The driving fluid, the numerous turbine driving fluids flowing into the external driving fluid, mixes with the external driving fluid to form an external driving fluid with a huge increase in flow speed; the external driving fluid with a huge flow speed drives the turbine drive blades and then flows to the turbine fluid outlet; at the same time, it also generates energy as the turbine As the shaft rotates, the density of the turbine driving fluid in the decompression groove is weakened, which reduces the resistance ability of the fluid in the decompression groove against the rotation of the turbine when the decompression groove moves to the next turbine fluid driving surface; because the turbine drive mode is Fluid driving surface, the turbine fluid driving force generated by the numerous turbine fluid driving surfaces created by the numerous turbine fluid driving nozzles C should be much higher than the turbine fluid driving force generated by the traditional fluid driving point; using air flow to assist the bicycle and using air flow to assist Electric power-assisted bicycles that generate electricity or electric motorcycles that use airflow to assist power generation, when using the peripheral turbine-driven fluid inflow device 13G that surrounds the turbine drive blades, lack the part in the booster tank when using the peripheral turbine-driven fluid inflow device 13F that surrounds the turbine drive blades. Reuse of turbine drive fluids;

other:

Fluid collecting silo, fluid flows into the fluid collecting silo shrinkage, fluid flows into the fluid collecting silo inlet, fluid flows into the fluid collecting silo guide cover, fluid dust collection screen, fluid filter screen, fluid flows into the guide cover, fluid flows in Cutting cover, turbine drive blade, turbine casing, turbine shaft, turbine bracket, surrounding the periphery of the turbine drive blade, the turbine drive fluid inflow device 13F is provided with a plurality of constriction nozzles A, mixing cylinders B, turbine fluid drive nozzles C, and boosting grooves The fluid separation plate D of the pressure reducing tank is provided with a pressurized fluid guide slot E, which is provided with a turbine fluid discharge port, a fluid negative pressure guide cover, a fluid negative pressure discharge port, a turbine external driving fluid inlet, and an external driving fluid Filter, externally driven fluid guide cover, externally driven fluid flows out of the constriction nozzle, externally driven fluid flows into the interceptor cover, there is a decompression groove on the inside of the turbine drive blade and a booster groove on the outside, generator, power transmission device, battery, The fluid flows into the interceptor cover adjustment device, the drive motor, the electric energy control device, the induction vehicle body, the external drive fluid flows into the interceptor cover drive device, and the turbine drive fluid inflow device 13G is provided with multiple constriction nozzles A and turbine fluid around the periphery of the turbine drive blades. Drive the nozzle C, the fluid separation plate D between the pressure increasing tank and the pressure reducing tank.
According to claim 1: the use of air flow to assist the bicycle eliminates the need for generators, batteries, drive motors, and electric energy control devices; when the air flow assist bicycle is traveling and the air flow assist facility is working, the turbine shaft in the turbine drive facility that rotates easily is assisted by The conduction of the transmission device drives the bicycle drive wheel or drive shaft to form auxiliary power that uses airflow to assist the bicycle; when the moving bicycle needs to reduce the auxiliary power, the fluid flows into the interceptor cover adjustment device to open a part of the fluid into the interceptor cover and close the fluid Part of the fluid inflow port that flows into the fluid pressure collecting tank reduces the inflow of part of the gravity acceleration fluid flowing into the fluid pressure collecting tank, reduces the pressure of the continued pressure fluid flowing into the fluid pressure collecting tank, and reduces some of the effects of the air flow assist facility;

When the moving bicycle does not need to use the airflow assist facility to work or the airflow assist facility fails, the fluid flows into the interceptor cover adjustment device and the external drive fluid flows into the interceptor cover driving device to open the fluid flow into the interceptor cover and the turbine external drive fluid into the interceptor cover. , close the turbine-driven fluid inlet of the air-assisted facility and stop using air-assisted equipment. Facility work.
According to claim 1: the electric power-assisted bicycle that utilizes airflow to assist in power generation eliminates the power-assisted conduction device; the electric power-assisted bicycle is driven manually or by the electric energy of the battery and uses airflow to assist in power generation. When the electric power-assisted bicycle is traveling and uses airflow to assist the power generation facility in operation, the turbine The easily rotating turbine shaft in the drive facility drives the generator to generate electrical energy; under the control of the electrical energy control device, the electrical energy generated by the generator is combined with the electrical energy of the battery to drive the drive motor, forming a new drive motor that uses airflow to assist in power generation and electric power-assisted bicycles. supply mode; as the running speed of the car body increases, and as the power generation energy generated by the airflow-assisted power generation facility increases, when the driving capacity of the drive motor reaches the speed required for the car body operation, the artificial driving force is cancelled; when the generator generates When the power generation reaches the power required to drive the motor, etc., the power control device will automatically stop the battery's power output; when the power generated by the generator exceeds the power required to drive the motor, the excess power generated by the generator will be The regulating device charges the battery; when the driving motor stops working, the main job of the electric energy generated by the generator is to charge the battery through the electric energy regulating device;

When the generator fails or the airflow-assisted power generation facility fails, and the work of the airflow-assisted power generation facility needs to be stopped, the fluid flows into the interceptor cover adjustment device and the external drive fluid flows into the interceptor cover driving device, and the fluid flows into the interceptor cover and the external drive fluid flows into the interceptor. When the cover is opened, the turbine-driven fluid inlet of the airflow-assisted power generation facility is closed, and the operation of the airflow-assisted power generation facility is stopped.
According to claim 1: the electric motorcycle that uses airflow to assist power generation eliminates the power-assisted conduction device; the electric energy of the battery drives the motor to drive the electric motorcycle that uses airflow to assist power generation. When the airflow assists power generation facility is working, the turbine drive facility can easily operate. The rotating turbine shaft drives the generator to generate electric energy; the electric energy generated by the generator is transmitted to the driving motor through the electric energy control device, forming auxiliary electric energy for the electric motorcycle that uses air flow to assist in power generation; when the electric energy generated by air flow to assist in power generation can meet the driving requirements When the electric energy required for the operation of the motor, etc. is exceeded, the electric energy control device will automatically stop the electric energy output of the battery; when the electric energy generated by the air flow-assisted power generation exceeds the electric energy required for the driving of the motor, etc., the excess electric energy is charged to the battery through the electric energy control device; when the drive When the motor stops working and does not require electric energy, the main job of the electric energy generated by the generator is to charge the battery through the electric energy regulating device;

When the generator fails or the airflow-assisted power generation facility fails, and the work of the airflow-assisted power generation facility needs to be stopped, the fluid flows into the interceptor cover adjustment device and the external drive fluid flows into the interceptor cover driving device, and the fluid flows into the interceptor cover and the external drive fluid flows into the interceptor. When the cover is opened, the turbine-driven fluid inlet of the airflow-assisted power generation facility is closed, and the operation of the airflow-assisted power generation facility is stopped.