Title:
ロケットエンジン部材並びにロケットエンジン部材の製造方法
Document Type and Number:
Japanese Patent JP4014208
Kind Code:
B2
Abstract:
Method and arrangement for providing a liquid fuel rocket engine member having a load bearing wall structure ( 11,14 ) including a plurality of cooling channels ( 11 ) for handling a coolant flow. Each cooling channel ( 11 ) is provided with a flow guiding surface ( 15 ) extending at an angle to the cooling channel axis, for providing the axial coolant flow with an added flow component in the radial direction.
Inventors:
Hegunder, Yang
Application Number:
JP2002556494A
Publication Date:
November 28, 2007
Filing Date:
January 09, 2002
Export Citation:
Assignee:
Volvo Aero Corporation
International Classes:
F02K9/64; F02K99/00; B21D53/84; B23P15/00; F02K1/00; F02K9/97; F28F1/40; F28F13/12
Domestic Patent References:
| JP6330816A | ||||
| JP10274002A | ||||
| JP6010766A | ||||
| JP7243351A |
Attorney, Agent or Firm:
Kazuo Shigenobu
Hideo Shimizu
Yuichi Takagi
Hideo Shimizu
Yuichi Takagi