Rotary knocking gas turbine
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Applications(China)
- Current Assignee / Owner
- XIAN THERMAL POWER RES INST CO LTD
- Publication Date
- 2014-11-19
- Estimated Expiration
- Not applicable · inactive patent
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Abstract
Description
【Technical field】
[0001] The invention relates to a gas turbine, in particular to a rotating detonation gas turbine for ships and industries. 【Background technique】
[0002] Combustion is an indispensable key link in the release of fuel energy in gas turbines. There are many forms of combustion. According to the characteristics and methods of flame self-propagation, it can be divided into two types: slow combustion and detonation combustion. Slow-flame combustion is the acceleration of the reaction caused by the temperature rise of the unburned mixture through heat conduction (or the transfer of free atoms and free radicals to the unburned mixture due to thermal diffusion and thermal radiation to produce a chain reaction), thereby making the flame The leading edge continues to advance into the unburned mixture, and the flame surface of the slow-burning combustion is usually called a slow-burning wave. Due to the limitation of the temperature transfer mode of the slow-burning...