The patent badge is an abbreviated version of the USPTO patent document. The patent badge does contain a link to the full patent document.

The patent badge is an abbreviated version of the USPTO patent document. The patent badge covers the following: Patent number, Date patent was issued, Date patent was filed, Title of the patent, Applicant, Inventor, Assignee, Attorney firm, Primary examiner, Assistant examiner, CPCs, and Abstract. The patent badge does contain a link to the full patent document (in Adobe Acrobat format, aka pdf). To download or print any patent click here.

Date of Patent:
May. 25, 2021

Filed:

Jun. 18, 2019
Applicant:

Zhejiang University, Hangzhou, CN;

Inventors:

Gang Xiao, Hangzhou, CN;

Kaixiang Xing, Hangzhou, CN;

Tianfeng Yang, Hangzhou, CN;

Mingjiang Ni, Hangzhou, CN;

Zhongyang Luo, Hangzhou, CN;

Kefa Cen, Hangzhou, CN;

Assignee:

ZHEJIANG UNIVERSITY, Hangzhou, CN;

Attorneys:
Primary Examiner:
Assistant Examiner:
Int. Cl.
CPC ...
F01D 5/28 (2006.01); F01D 5/18 (2006.01); F03G 6/06 (2006.01); F02C 1/05 (2006.01); F01K 25/10 (2006.01);
U.S. Cl.
CPC ...
F01D 5/288 (2013.01); F01D 5/18 (2013.01); F01D 5/186 (2013.01); F01D 5/28 (2013.01); F02C 1/05 (2013.01); F03G 6/064 (2013.01); F01K 25/103 (2013.01); F05D 2260/202 (2013.01); F05D 2260/221 (2013.01); F05D 2300/611 (2013.01);
Abstract

A turbine for solar thermal power generation and a Brayton cycle are disclosed. The turbine includes a blade which has a cooling working medium inlet and a cooling working medium jet orifice. The blade is provided as a cavity with hollow interior; the cooling working medium inlet is located inside the blade; the cooling working medium jet orifice is provided on the blade surface on which is provided a spectral conversion coating; the spectral conversion coating converts heat on the blade surface into conversion characteristic band radiation which is radiation energy adjacent to cooling working medium characteristic band radiation of a cooling working medium. The turbine adopts a characteristic spectral coating and a jet cooling to enhance the cooling effect for a turbine blade and to improve the system efficiency of the Brayton cycle.


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