IP Library Granted Patent US 6,905,312
Granted Patent B2
US 6,905,312 · App. 10/226,208 · Granted Jun 14, 2005

Method of manufacturing an integral rotor blade disk and corresponding disk

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Quick Facts
Patent No.
US 6,905,312
App. No.
10/226,208
Granted
Jun 14, 2005
Kind
B2
Abstract

A method of manufacturing a blisk comprises the steps of cutting a disk to a rough shape comprising a hub with a plurality of blade blanks projecting radially therefrom, machining each blade blank by tangential milling using a tool with a rotation spindle perpendicular to the radial direction to make repeated radial passes, the tool being turned through a facet angle with respect to the disk between each pass. Each blade blank is thus milled to a blade having faceted surfaces. Preferably, the width of each facet is smaller that 5 mm, and adjacent facets subtend angles smaller than 5°, or even more preferably smaller than 3°.

Claims (42)

1. A method of manufacturing a blisk comprising a hub and a plurality of blades integrally projecting substantially radially therefrom, which method comprises the steps of:

cutting a disk to a rough state to form blade blanks therein;

milling each of said blade blanks by tangential milling using a tool, said milling step comprising the steps of:

a) making a substantially radial pass with respect to said disk with said tool;

b) turning said tool through a facet angle with respect to said disk in a plane tangential to said disk; and

repeating steps a) and b) until a blade has been milled from said blade blank, wherein the substantially radial passes are made over an entire surface of said blade blanks.

2. A method of manufacturing a blisk comprising a hub and a plurality of blades integrally projecting substantially radially therefrom, which method comprises the steps of:

cutting a disk to a rough state to form blade blanks therein;

milling each of said blade blanks by tangential milling using a tool, said milling step comprising the steps of:

a) making a substantially radial pass with respect to said disk with said tool;

b) turning said tool through a facet angle with respect to said disk in a plane tangential to said disk; and

repeating steps a) and b) until a blade has been milled from said blade blank,

wherein said tool has a conical central part, a rounded end part and a rounded part for connection to a rotation spindle, the rounded part for connection tapers toward said rotation spindle, said central part tapering toward said end part and connecting to said end part and to said rounded part for connection without forming a ridge.

3. A method of manufacturing a blisk comprising a hub and a plurality of blades integrally projecting substantially radially therefrom, which method comprises the steps of:

cutting a disk to a rough state to form blade blanks therein;

milling each of said blade blanks by tangential milling using a tool, said milling step comprising the steps of:

a) making a substantially radial pass with respect to said disk with said tool;

b) turning said tool through a facet angle with respect to said disk in a plane tangential to said disk; and

repeating steps a) and b) until a blade has been milled from said blade blank,

wherein said step of cutting the disk to a rough sate includes the formation of an outer holding annulus connecting said blade blanks, each said substantially radial pass running from said hub to said annulus, and wherein said method further comprises a step of parting said annulus from the blades after said blades have been milled.

4. A method of manufacturing a blisk according to claim 3 , wherein said annulus is parted from said blades by wire electrical discharge machining.

5. A method of manufacturing a blisk comprising a hub and a plurality of blades integrally projecting substantially radially therefrom, which method comprises the steps of:

cutting a disk to a rough state to form blade blanks therein;

milling each of said blade blanks by tangential milling using a tool, said milling step comprising the steps of:

a) making a substantially radial pass with respect to said disk with said tool;

b) turning said tool through a facet angle with respect to said disk in a plane tangential to said disk; and

repeating steps a) and b) until a blade has been milled from said blade blank,

wherein said tool is inclined in a substantially radial plane at least at one of the ends of said passes.

6. A method of manufacturing a blisk according to claim 1 , wherein said tool comprises a part-finishing tool, the method further comprising a step of replacing said part-finishing tool with a finishing tool, whereby the blade blanks are each milled completely twice.

7. A method of manufacturing a blisk comprising a hub and a plurality of blades integrally projecting substantially radially therefrom, which method comprises the steps of:

cutting a disk to a rough state to form blade blanks therein;

milling each of said blade blanks by tangential milling using a tool, said milling step comprising the steps of:

a) making a substantially radial pass with respect to said disk with said tool;

b) turning said tool through a facet angle with respect to said disk in plane tangential to said disk; and

repeating steps a) and b) until a blade has been milled from said blade blank,

wherein said tool comprises a part-finishing tool, the method further comprising a step of replacing said part-finishing tool with a finishing tool, whereby the blade blanks are each milled completely twice, and

wherein each said tool has a conical central part, a rounded end part and a rounded part for connection to a rotation spindle, the rounded part for connection tapers toward said rotation spindle, said central part tapering toward said end part and connecting to said end part and to said rounded part for connection, wherein said part-finishing tool has a taller central part than said finishing tool.

8. A blisk which comprises blades having faces formed of substantially radial longilinear facets, wherein said facets extend over an entire surface of said blades.

9. A blisk according to claim 8 , wherein said facets are separated by concave connecting portions at least on a side of each blade which corresponds to a pressure face.

10. A blisk according to claim 8 , wherein adjacent facets subtend angles smaller than 5°.

11. A blisk according to claim 9 , wherein adjacent facets subtend angles smaller than 3°.

12. A blisk according to claim 9 , wherein said facets have widths at most equal to 5 mm.

Assignments (4)
CORRECTIVE ASSIGNMENT TO CORRECT THE COVER SHEET TO REMOVE APPLICATION NOS. 10250419, 10786507, 10786409, 12416418, 12531115, 12996294, 12094637 12416422 PREVIOUSLY RECORDED ON REEL 046479 FRAME 0807. ASSIGNOR(S) HEREBY CONFIRMS THE CHANGE OF NAME. Recorded Aug 24, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046939/0336 →
CHANGE OF NAME Recorded May 23, 2018
From: SNECMA
To: SAFRAN AIRCRAFT ENGINES
Reel/Frame 046479/0807 →
CHANGE OF NAME Recorded Feb 20, 2008
From: SNECMA MOTEURS
To: SNECMA
Reel/Frame 020609/0569 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Mar 25, 2005
From: BOURGY, JOEL; DAVID, JEAN-PIERRE ANDRE DENIS; DERRIEN, STEPHANE JEAN-DANIEL MAURICE; MALEVILLE, THIERRY JEAN
To: SNECMA-MOTEURS
Reel/Frame 016396/0024 →