Login| Sign Up| Help| Contact|

Patent Searching and Data


Title:
タービンディスク及びタービンディスクの製造方法
Document Type and Number:
Japanese Patent JP6877964
Kind Code:
B2
Abstract:
A turbine disc 202 having a radius and a circumference is provided. The turbine disc includes a central aperture 402 and a plurality of cooling channels 316, 414 circumferentially spaced about the central aperture such that the cooling channels are in flow communication with the central aperture. Each of the cooling channels has a radially inner end 424, a radially outer end 426, and a lengthwise axis 422 that is curved between the radially inner end and the radially outer end.

More Like This:
WO/2013/143872A SYSTEM FOR INDUCTIVE HEATING OF TURBINE ROTOR DISKS
JP2006097585MOUNTING STRUCTURE FOR AIR SEPARATOR AND GAS TURBINE PROVIDED WITH THE SAME
Inventors:
Sudaka Niri
Sachet Barrel Quentin Eldorido
Robert Cormack Young
Marius Planeschi
Application Number:
JP2016225698A
Publication Date:
May 26, 2021
Filing Date:
November 21, 2016
Export Citation:
Click for automatic bibliography generation   Help
Assignee:
GENERAL ELECTRIC COMPANY
International Classes:
F01D5/08
Domestic Patent References:
JP2009203926A
JP9013902A
JP2013139808A
Foreign References:
US4203705
US20120171029
Attorney, Agent or Firm:
Hirokazu Ogura
Toshihisa Kurokawa
Takuto Tanaka



 
Previous Patent: 画像形成装置、画像形成装置の制御方法、およびプログラム

Next Patent: 液体供給ユニットの製造方法