IP Library Granted Patent US 10,408,277
Granted Patent B2
US 10,408,277 · App. 15/535,396 · Granted Sep 10, 2019

Twist-breakable mechanical fuse and cooling unit of a turbine engine fitted with such a fuse

Inventors: Mathieu Cladiere (Pau, FR); Armand Bueno (Assat, FR); Olivier Pierre Descubes (Nay, FR); Stephane Vergez (Aast, FR)
Assignee: SAFRAN HELICOPTER ENGINES
F16D9/06F01D21/00F01D25/12F04D29/263F05D2260/20F05D2260/311
View Patent ↗
Loading inventors, assignments & file history…
Monitor This Case
Get email alerts when status or documents change.
Order Certified Copies
Most orders are placed with the USPTO same day — all within 24 business hours.
Order via The Patent Place →
Pre-filled with this patent's details
Quick Facts
Patent No.
US 10,408,277
App. No.
15/535,396
Granted
Sep 10, 2019
Kind
B2
Abstract

The invention relates to a mechanical fuse intended to be rigidly mounted between a drive unit ( 8, 9 ), and a receiver unit ( 10 ), each rotating about the same axis ( 7 ) of rotation, said fuse comprising a body ( 13 ) extending in a longitudinal direction parallel to said axis ( 7 ) of rotation, once the fuse is mounted between said drive unit ( 8, 9 ) and receiver unit ( 10 ). The invention is characterized in that said body ( 13 ) comprises a plurality of longitudinal bars ( 14 ), each bar ( 14 ) being deformable by bending, such as to form a twist-breakable mechanical fuse.

Claims (11)

1. A mechanical fuse intended to be mounted securely in a turbine engine between a driving mechanical member, referred to as a driving member, and a driven mechanical member, referred to as a receiving member, each rotating about the same axis of rotation, said fuse comprising a body extending in a longitudinal direction parallel to said axis of rotation, once the fuse is mounted between said driving and receiving members,

wherein said body comprises a plurality of longitudinal bars, each bar being suitable for being deformed by bending, under the action of a torsional moment applied to all the bars, so as to form a breakable mechanical fuse.

2. The fuse according to claim 1 , wherein it comprises means for the reversible coupling of the fuse to said driving member, which means are arranged at a longitudinal end of said body, referred to as the distal end.

3. The mechanical fuse according to claim 2 , wherein said distal end of said body has a conical portion or a cylindrical portion, which portion is adapted to a conical portion or a cylindrical portion of said driving member.

4. The fuse according to claim 1 , wherein it comprises means for the reversible coupling of the fuse to said receiving member, which means are arranged at a longitudinal end of said body, referred to as the proximal end.

5. The mechanical fuse according to claim 4 , wherein said proximal end of said body comprises an attachment plate suitable for being attached to said receiving member.

6. The mechanical fuse according to claim 1 , wherein said body is hollow.

7. The mechanical fuse according to claim 3 , wherein it comprises means for the reversible coupling of the fuse to said receiving member, which means are arranged at a longitudinal end of said body, referred to as the proximal, wherein said body is hollow, wherein it comprises a strut suitable for being received in said hollow body through said proximal end and for being able to place said conical portion of the distal end in abutment on said conjugate conical portion of said driving member.

8. The fuse according to claim 7 , wherein said strut has a shoulder that makes it possible to limit the axial movement of said receiving member in the event of mechanical breakage of the fuse.

9. The fuse according to claim 1 , wherein said body is cylindrical and in that it comprises three bars distributed uniformly around said body.

10. A cooling unit of a turbine engine comprising a driving shaft and an impeller mounted in cantilever on said shaft, wherein it comprises a mechanical fuse according to claim 1 that is arranged between said driving shaft and said impeller.

Assignments (2)
CHANGE OF NAME Recorded Jul 3, 2017
From: TURBOMECA
To: SAFRAN HELICOPTER ENGINES
Reel/Frame 043084/0351 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded Jun 19, 2017
From: CLADIERE, MATHIEU PIERRE; BUENO, ARMAND; DESCUBES, OLIVIER PIERRE; VERGEZ, STEPHANE ERIC
To: TURBOMECA
Reel/Frame 042752/0018 →
Priority Claims (1)
FR 14 62399 · Dec 15, 2014 · national
Continuity (1)
Related Publication 20170343052A1 · Nov 30, 2017