IP Library Granted Patent US 8,827,734
Granted Patent B2
US 8,827,734 · App. 13/505,987 · Granted Sep 9, 2014

Turbo machine electrical connection element

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Quick Facts
Patent No.
US 8,827,734
App. No.
13/505,987
Granted
Sep 9, 2014
Kind
B2
Abstract

An electrical connection element for a turbine engine, including conductors connected to a connector by a tubular coupling surrounding one end of the conductors, and an insert providing protection against wear of the conductors being mounted in the tubular coupling. The insert includes a substantially tubular central body containing the conductors and provided over at least a fraction of its length with a series of spacers bearing against an inside surface of the tubular coupling of the connection element so as to hold the central body at a distance from the inside surface.

Claims (22)

1. An electrical connection element for a turbine engine, the element comprising:

electrical conductors connected to a connector by a tubular coupling surrounding an end of the conductors; and

an insert for providing protection against wear of the conductors, the insert being disposed in the tubular coupling around the conductors, the insert comprising a substantially tubular central body containing the conductors and provided over at least a fraction of the length with a series of spacers extending substantially radially outwards and bearing against an inside surface of the tubular coupling of the connection element so as to hold the central body at a distance from the inside surface, with no fastening of the series of spacers to the inside surface of the tubular coupling.

2. The electrical connection element according to claim 1 , wherein the insert is elastically deformable, or is bendable.

3. An electrical connection element for a turbine engine, the element comprising:

electrical conductors connected to a connector by a tubular coupling surrounding an end of the conductors; and

an insert for providing protection against wear of the conductors, the insert being disposed in the tubular coupling around the conductors, the insert including a substantially tubular central body containing the conductors and provided over at least a fraction of the length with a series of spacers extending substantially radially outwards and bearing against an inside surface of the tubular coupling of the connection element so as to hold the central body at a distance from the inside surface, the spacers comprising parallel disks that are spaced apart from one another along the central body.

4. The electrical connection element according to claim 3 , wherein the disks are connected together by longitudinal bridges of material that are elastically deformable and that form the central body.

5. The electrical connection element according to claim 3 , wherein the insert further includes a tubular end connected to one end of the central body and having an outside diameter that is substantially equal to the inside diameter of the tubular coupling of the connection element, the tubular end defining a storage chamber for storing extra lengths of the conductors of the connection element.

6. The electrical connection element according to claim 5 , wherein the end of the insert remote from the tubular end is substantially frustoconical in shape.

7. The electrical connection element according to claim 1 , wherein the insert is made as a single piece of plastics material, or of polytetrafluoroethylene.

8. An electrical connection element for a turbine engine, the element comprising:

electrical conductors connected to a connector by a tubular coupling surrounding an end of the conductors; and

an insert for providing protection against wear of the conductors, the insert being disposed in the tubular coupling around the conductors, the insert having a length and including a substantially tubular central body containing the conductors and provided over at least a fraction of the length with a series of spacers extending substantially radially outwards and bearing against an inside surface of the tubular coupling of the connection element so as to hold the central body at a distance from the inside surface, the insert including a longitudinal slot extending over all of the length so as to enable the insert to be mounted on the conductors of the connection element.

9. The electrical connection element according to claim 1 , wherein the insert is releasably mounted in the tubular coupling which is straight or forms a bend.

10. An airplane engine, comprising at least one electrical connection element according to claim 1 .

11. An electrical connection element for a turbine engine, the element comprising:

a connector;

electrical conductors;

a tubular coupling surrounding an end of the conductors and connecting the conductors to the connector; and

an insert for providing protection against wear of the conductors, the insert being disposed in the tubular coupling around the conductors, the insert comprising a substantially tubular central body containing the conductors, the substantially tubular central body having a length and being provided over at least a fraction of the length with a series of spacers extending substantially radially outwards from the substantially tubular central body, the series of spacers bearing against an inside surface of the tubular coupling, so as to hold the substantially tubular central body at a distance from the inside surface, the insert being freely disposed in the tubular coupling so as to be adapted to be inserted into and removed from the tubular coupling by sliding therealong.

12. An airplane engine, comprising at least one electrical connection element according to claim 11 .

Assignments (3)
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 →
ASSIGNMENT OF ASSIGNOR'S INTEREST Recorded May 8, 2012
From: AUDIC, YVON; DETERRE, GEOFFRAY; LABRANCHE, JULIEN; PRINZIVALLE, NICOLAS
To: SNECMA
Reel/Frame 028170/0329 →