Title:
FACILITY USING AIRFLOW FOR POWER ASSISTANCE AND AUXILIARY POWER GENERATION (WEAK-PRESSURE-ADSORPTION-TYPE FLUID-DRIVEN POWER MACHINE)
Document Type and Number:
WIPO Patent Application WO/2024/060468
Kind Code:
A1
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.
Inventors:
WANG ZIJIE (CN)
Application Number:
PCT/CN2023/000047
Publication Date:
March 28, 2024
Filing Date:
March 26, 2023
Export Citation:
Assignee:
WANG ZIJIE (CN)
International Classes:
F03D9/32
Foreign References:
| US20180156192A1 | 2018-06-07 | |||
| CN105480100A | 2016-04-13 | |||
| CN106438208A | 2017-02-22 | |||
| CN107215426A | 2017-09-29 | |||
| CN201428509Y | 2010-03-24 | |||
| CN206766264U | 2017-12-19 |
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