Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
SEAL MEMBER AND GAS TURBINE
Document Type and Number:
WIPO Patent Application WO/2022/190689
Kind Code:
A1
Abstract:
Provided is a seal member which forms a combustion gas flow path of a gas turbine, wherein: the seal member includes a first main body part having therein a cooling path; the first main body part comprises a first end section which forms one end section in a circumferential direction, a second end section which forms the other end section on the opposite side in the circumferential direction, and an intermediate section formed between the first end section and the second end section; and the cooling path includes an intermediate section cooling path inclined at a first angle with respect to an axial direction, a first end section cooling path provided to the first end section and inclined at a second angle with respect to the axial direction, and a second end section cooling path provided to the second end section and inclined at a third angle with respect to the axial direction, the second angle and the third angle both being smaller than the first angle.

Inventors:
KINOSHITA TAIKI (JP)
SATO KENJI (JP)
TOKUYAMA KENTARO (JP)
TANIGUCHI KENTA (JP)
SAKAKI HIROYUKI (JP)
Application Number:
PCT/JP2022/002981
Publication Date:
September 15, 2022
Filing Date:
January 27, 2022
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
MITSUBISHI HEAVY IND LTD (JP)
MITSUBISHI POWER LTD (JP)
International Classes:
F02C7/28; F23R3/42
Foreign References:
JP2014009937A2014-01-20
US20120210720A12012-08-23
JP2006105076A2006-04-20
JP2016070081A2016-05-09
Attorney, Agent or Firm:
SSIP PATENT ATTORNEY CORPORATION (JP)
Download PDF: