Title:
ターボ機械冷却システム
Document Type and Number:
Japanese Patent JP7187176
Kind Code:
B2
Abstract:
The present disclosure is directed to a cooling system for a turbomachine. The cooling system includes a turbomachine component defining a turbomachine component cavity. The cooling system also includes an insert positioned within the turbomachine component cavity for cooling the turbomachine component. The insert includes an insert body and a spring body. The spring body includes a first portion fixedly coupled to the insert body, a second portion in sliding engagement with the turbomachine component, and a third portion in sliding engagement with the insert body.
Inventors:
Sandip Datta
Scott Francis Johnson
Joseph Anthony Weber
Scott Francis Johnson
Joseph Anthony Weber
Application Number:
JP2018093513A
Publication Date:
December 12, 2022
Filing Date:
May 15, 2018
Export Citation:
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F01D9/02; F01D5/18
Domestic Patent References:
| JP1244103A | ||||
| JP2010216471A | ||||
| JP57083606A |
Foreign References:
| US20100068034 | ||||
| US8777569 |
Attorney, Agent or Firm:
Hiroshi Ogura
Takuto Tanaka
Takuto Tanaka
Previous Patent: Nucleic acid detection method for pathogenic microorganisms
Next Patent: Pockets in rotor blades for turbomachinery
Next Patent: Pockets in rotor blades for turbomachinery