Method for producing turbine engine parts, and resulting blank and mould

US9844843B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9844843-B2
Application numberUS-201415106235-A
CountryUS
Kind codeB2
Filing dateDec 9, 2014
Priority dateDec 20, 2013
Publication dateDec 19, 2017
Grant dateDec 19, 2017

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  1. Title

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  2. Abstract

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  3. Assignees and inventors

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  4. Key dates

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  5. First independent claim

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  7. Citations and related patents

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Abstract

Official abstract text for this publication.

The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mold in order to produce a blank ( 3 ); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron with two generally trapezoidal opposing sides ( 30 a, 30 b ), and the parts are machined in the blank.

First claim

Opening claim text (preview).

The invention claimed is: 1. A method for producing multiple metal turbine engine parts, the method comprising: casting a metal alloy in a mould in order to produce a blank; and machining the blank in order to produce the parts, wherein the blank obtained by casting is a solid polyhedron with two trapezoidal opposing sides, and the parts are machined in the blank, wherein the blank having two lateral opposing sides being limited by two largest sides of the blank, each of the two largest sides being larger than each of said lateral opposing sides, wherein said parts are blades each having a longitudinal axis and, along such axis, a root at a first end, a heel at a second end, and a curved section vane which extends therebetween, wherein the blank is adapted to totally contain at least two such identical blades, positioned side by side, but at a distance from each other, and wherein the two largest sides of the blank are inscribed in an angle ranging from 2° to 10°, so that said blades can be machined in the blank and all have the same orientation, during the casting and machining steps. 2. The method according to claim 1 wherein, during the step a), the blank is so moulded that the two trapezoidal opposing sides are substantially parallel and each consist of only one substantially flat face. 3. The method according to claim 1 , wherein, upon moulding, the blank is so moulded that the heels of the blades are aligned along a plane parallel to a lateral face of the blank other than the two largest sides of the blank and other than the trapezoidal opposing sides. 4. The method according to claim 1 , wherein, prior to machining said parts, the blank is cut substantially along a plane: which passes between two volumes of the blank, each being adapted to totally contain at least one of said parts, and which cuts the two largest sides of the blank and the two lateral opposing sides. 5. A method for producing multiple metal turbine engine parts, the method comprising: casting a metal alloy in a mould in order to produce a blank; and machining the blank in order to produce the parts, wherein the blank obtained by casting is a solid polyhedron with two trapezoidal opposing sides, and the parts are machined in the blank, wherein said blank having two lateral opposing sides being limited by two largest sides of the blank, each of the two largest sides being larger than each of said lateral opposing sides, wherein said parts are blades each having a longitudinal axis and, along such axis, a root at a first end, a heel at a second end, and a section vane which extends therebetween, wherein the blank is adapted to totally contain at least two such identical blades, positioned side by side, but at a distance from each other, and wherein said blades are so machined in the blank that they all have the same orientation, and wherein, upon moulding, the blank is so moulded that the heels of the blades are aligned along a plane parallel to a lateral face of the blank other than the two largest sides of the blank and other than the trapezoidal opposing sides.

Assignees

Inventors

Classifications

  • B23P15/02Primary

    turbine or like blades from one piece · CPC title

  • Centrifugal casting; Casting by using centrifugal force · CPC title

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What does patent US9844843B2 cover?
The invention relates to a method for producing multiple metal turbine engine parts, comprising steps consisting in: a) casting a metal alloy in a mold in order to produce a blank ( 3 ); and b) machining the blank in order to produce the parts, characterized in that the blank obtained by casting is a solid polyhedron with two generally trapezoidal opposing sides ( 30 a, 30 b ), …
Who is the assignee on this patent?
Snecma
What technology area does this patent fall under?
Primary CPC classification B23P15/02. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Dec 19 2017 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 1 related publication on this page (citations in our corpus or others sharing the same primary CPC).