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Rotating pulse detonation engine, power generation system comprising the same, and methods of manufacturing and using the same

The pulse detonation is converted into rotating thrust by the rotating pulse detonation engine, combined with the turbine unit, which solves the problems of low efficiency and high pollution of traditional engines, and achieves high-efficiency, low-pollution rotating torque propulsion, which is suitable for a variety of fuels and application scenarios. .

Inactive Publication Date: 2018-06-08
李伟德
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  • Abstract
  • Description
  • Claims
  • Application Information

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Problems solved by technology

however, the fuel and oxidizer must be stored within the rocket case, and the weight of the fuel and oxidizer requires more fuel and oxidizer (eg, to move the fuel and oxidizer) and reduces the efficiency of the engine

Method used

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  • Rotating pulse detonation engine, power generation system comprising the same, and methods of manufacturing and using the same
  • Rotating pulse detonation engine, power generation system comprising the same, and methods of manufacturing and using the same
  • Rotating pulse detonation engine, power generation system comprising the same, and methods of manufacturing and using the same

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Embodiment Construction

[0039] Reference will now be made in detail to various embodiments of the invention, examples of which are illustrated in the accompanying drawings. While the invention will be described in conjunction with the following examples, it will be understood that these descriptions are not intended to limit the invention to these examples. On the contrary, the invention is intended to cover alternatives, modifications and equivalents, which may be included within the spirit and scope of the invention. Moreover, in the following detailed description, numerous specific details are set forth in order to provide a thorough understanding of the invention. It will be apparent, however, to one skilled in the art that the present invention may be practiced without these specific details. In other instances, well-known methods, procedures, components, and materials have not been described in detail so as not to unnecessarily obscure relevant aspects of the present invention.

[0040] There...

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PUM

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Abstract

An engine, a power generation system, and methods of manufacturing and using the same are disclosed. The engine includes a detonation / combustion chamber configured to detonate a fuel and rotate arounda central rotary shaft extending from the chamber, a fuel supply inlet configured to provide the fuel to the chamber, an air supply channel configured to supply air to the chamber, at least two rotating arms extending radially from the chamber and configured to exhaust gases from detonating the fuel in the chamber and provide a rotational thrust and / or force, and a mechanical work unit configuredto receive at least part of the rotational thrust and / or force. Each of the rotating arms has an exhaust nozzle at a distal end thereof, the exhaust nozzle being at or having an angle configured to provide the rotational thrust and / or force.

Description

[0001] Cross References to Related Applications [0002] This application claims U.S. Provisional Patent Application Nos. 62 / 172,560, filed June 8, 2015, 62 / 285,174, filed October 21, 2015, and 15 / 046,965, filed February 18, 2016 US Patent Application No. , each of which is incorporated herein by reference as if fully set forth herein. technical field [0003] The field to which the invention generally relates is that of detonation and / or combustion engines. More specifically, embodiments of the present invention relate to a novel rotary pulse detonation and / or combustion engine, power generation system including the same, and methods of manufacture and use thereof. Background technique [0004] The traditional combustion of coal and oil is still used as the main source of energy to generate electricity and drive automobiles and modern jets. However, these technologies lead to air pollution and global warming. [0005] In a conventional jet engine, air is compressed and ...

Claims

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Application Information

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Patent Type & Authority Applications(China)
IPC IPC(8): F01B21/04F02K7/02
CPCF01D1/32F02C5/04F02C5/12Y02T50/60F02K1/78F02K7/06F02K9/64
Inventor 李伟德
Owner 李伟德
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