Method for manufacturing a part by metal injection molding

Patent metadata

Field	Value
Publication number	US-9950370-B2
Application number	US-201213720577-A
Country	US
Kind code	B2
Filing date	Dec 19, 2012
Priority date	Dec 20, 2011
Publication date	Apr 24, 2018
Grant date	Apr 24, 2018

Abstract

A method for manufacturing a part includes metal injection molding of metal powder mixed with a binder to produce individual components of the part as separately molded green compact sections which are then debindered to form brown compact sections. At least one of the brown compact sections is subjected to a pre-sintering process to undergo a first shrinkage. The pre-sintered brown compact section and a further brown compact section are joined together to form a multi-part brown compact which is subsequently subjected to a main sintering process, where the pre-sintered brown compact section undergoes less shrinkage than the further brown compact section to draw together and firmly connect the pre-sintered brown compact section and the further brown compact section.

First claim

The invention claimed is:

1. A method for manufacturing a part, comprising:
producing individual components of the part as separately molded green compact sections by metal injection molding of metal powder mixed with a binder, and then removing the binder from the green compact sections to form first, second and third debindered brown compact sections with the third brown compact section shaped to act as a connecting part to connect together the first and second brown compact sections;
subjecting one chosen from the third brown compact section, and the first and second brown compact sections to a pre-sintering process in which the one chosen from the third brown compact section, and the first and second brown compact sections undergoes a first shrinkage;
connecting to one another the first and second brown compact sections with the third brown compact section as the connecting part to form a multi-part brown compact, the other of the third brown compact section, and the first and second brown compact sections being non-pre-sintered when connected to the pre-sintered one chosen from the third brown compact section, and the first and second brown compact sections;
subsequently subjecting the multi-part brown compact to a main sintering process whereby the connected first, second and third brown compact sections undergo shrinkage, with the one pre-sintered one chosen from the third brown compact section, and the first and second brown compact sections undergoing a second shrinkage less than a shrinkage of the other of the third brown compact section, and the first and second brown compact sections to draw together and firmly connect to one another the first, second and third brown compact sections, thereby providing pressure on contact surfaces to be joined of the first, second and third brown compact sections;
connecting the first, second and third brown compact sections to one another before the main sintering process by positively engaging connecting elements provided on joining surfaces of the first, second and third brown compact sections, wherein the connecting elements of the first, second and third brown compact sections include:
a first one of a projection or a recess on the third brown compact section and a matching and complementary shape on the first brown compact section; and
a second one of a projection or a recess on the third brown compact section and a matching and complementary shape on the second brown compact section;
providing the one chosen from the third brown compact section, and the first and second brown compact sections to be pre-sintered with dimensions such that, before being subjected to the pre-sintering process, the one chosen from the third brown compact section, and the first and second brown compact sections cannot be connected to the other of the third brown compact section, and the first and second brown compact sections, and during the pre-sintering process the one chosen from the third brown compact section, and the first and second brown compact sections shrinks sufficiently to permit connection to the other of the third brown compact section, and the first and second brown compact sections;
wherein the third brown compact section which is the connecting part draws the first and second brown compact sections against one another making contact during the main sintering process.

2. The method in accordance with claim 1 , wherein the projection tapers towards the contact surfaces between the first and second brown compact sections and has at least one chosen from a dovetail and a club shape, and wherein the recess has a matching and complementary shape.

3. The method in accordance with claim 2 , and further comprising providing the projection with a convex curvature and the recess with a concave curvature.

4. The method in accordance with claim 1 , and further comprising providing the third brown compact section which is the connecting part with two projections acting as connecting elements.

5. The method in accordance with claim 1 , and further comprising providing that the part has a rotationally symmetrical design where one of the first and second brown compact sections is an inner brown compact section and the other of the first and second brown compact sections is an outer brown compact section enclosing the inner brown compact section, and the third brown compact section is the pre-sintered piece and via the main sintering process the outer brown compact section is drawn together with the inner brown compact section by the third brown compact section.

6. The method in accordance with claim 1 , wherein the first, second and third brown compact sections consist of a same material and have substantially identical shrinkage properties.

7. The method in accordance with claim 1 , wherein the pre-sintered one chosen from the third brown compact section, and the first and second brown compact sections undergoes a volume shrinkage of at least 2% during pre-sintering.

Assignees

• Rolls Royce Deutschland Ltd & Co Kg

Inventors

• Roth-Fagaraseanu Dan
• Schruefer Lukas

Classifications

• B22F5/009

  of turbine components other than turbine blades (of turbine blades B22F5/04) · CPC title

• B22F7/062

  involving the connection or repairing of preformed parts · CPC title

• B22F7/06

  of composite workpieces or articles from parts, e.g. to form tipped tools {(B22F7/002 takes precedence)} · CPC title

• B22F2005/005

  Article surface comprising protrusions · CPC title

• B22F7/02 Primary

  of composite layers {(B22F7/002 takes precedence)} · CPC title