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Title:
METHOD FOR PRODUCING COMPONENTS OF A GAS TURBINE
Document Type and Number:
WIPO Patent Application WO2005009654
Kind Code:
A3
Abstract:
The invention relates to a method for producing components of a gas turbine, in particular, an aircraft engine, by powder metallurgy injection moulding. In said injection moulding method, a metal powder is first mixed with a binding agent to form an homogeneous product, whereby at least one moulded body is then produced by injection moulding from said homogeneous product and whereby the or each moulded body is subjected to a binding agent removal process. The or each moulded body is then compacted by sintering to form at least one component with the desired geometric properties. According to said invention, the or each moulded body is placed in a powder product during sintering.

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JP2005526178A method for producing a sintered member from a sinterable material
Inventors:
KRANZEDER JOSEF (DE)
KRAUS MAX (DE)
MUELLER CLAUS (DE)
STEINHARDT ERICH (DE)
Application Number:
PCT/DE2004/001468
Publication Date:
June 16, 2005
Filing Date:
July 08, 2004
Export Citation:
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Assignee:
MTU AERO ENGINES GMBH (DE)
KRANZEDER JOSEF (DE)
KRAUS MAX (DE)
MUELLER CLAUS (DE)
STEINHARDT ERICH (DE)
International Classes:
B22F3/10; B22F3/22; (IPC1-7): B22F3/22; B22F3/10
Foreign References:
DE3527367A11987-02-12
US4783297A1988-11-08
DE3608095A11986-10-16
EP0633440A11995-01-11
Other References:
PATENT ABSTRACTS OF JAPAN vol. 1998, no. 01 30 January 1998 (1998-01-30)
PATENT ABSTRACTS OF JAPAN vol. 1996, no. 05 31 May 1996 (1996-05-31)
PATENT ABSTRACTS OF JAPAN vol. 1996, no. 08 30 August 1996 (1996-08-30)
PATENT ABSTRACTS OF JAPAN vol. 011, no. 025 (M - 556) 23 January 1987 (1987-01-23)
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