IP Library Granted Patent US 7,143,877
Granted Patent B2
US 7,143,877 · App. 10/513,796 · Granted Dec 5, 2006

Fusible link comprising damper and backstop

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Quick Facts
Patent No.
US 7,143,877
App. No.
10/513,796
Granted
Dec 5, 2006
Kind
B2
Abstract

A link including a rod with a connection member at each end with an axis passing through both connection members. The rod includes a fusible zone as a narrow section lying between a first rod portion connected to a first connection member and a second rod portion connected to a second connection member. The fusible zone breaks when tensile force to which the link is subjected is greater than a predetermined value. The two rod portions are inseparable in event of the fusible zone breaking by a cylinder coaxial about the axis and secured to the first rod portion, and having an end wall through which the second rod portion passes. The second rod portion includes a collar that can slide into the cylinder if the fusible zone breaks. The inside wall of the cylinder includes teeth configured to be broken by the collar if the fusible zone breaks.

Claims (24)

1. A link comprising:

a rod having a connection member at each end with an axis going through both connection members, wherein said rod includes a fusible zone in a form of a narrow section lying between a first rod portion connected to a first of the connection members and a second rod portion connected to a second of the connection members, said fusible zone configured to break when tensile force to which said link is subjected is greater than a predetermined value;

a body coaxial about said axis and secured at one end to the first rod portion, said body presenting at its other end an end wall having an orifice through which the second rod portion is capable of sliding, said body defining a cavity in which the fusible zone is housed, together with a collar formed around the second rod portion configured to slide into said cavity in an event of the fusible zone breaking;

a plurality of teeth formed on an inside wall of the body, said teeth being configured to be broken by the collar following breaking of the fusible zone; and

means for preventing return movement of the second rod portion after the fusible zone has broken,

wherein said plurality of teeth, while being broken by said collar, absorb a shock in the event of the fusible zone breaking, and

wherein said plurality of teeth are formed on the inside wall of the body in an annular chamber defined by the collar and by the end wall of the cylinder body.

2. A link according to claim 1 , wherein said body is configured so that the two rod portions are inseparable after the fusible zone breaks.

3. A link according to claim 2 , wherein said teeth are spread over one or more spirals.

4. A link according to claim 1 , wherein said means for preventing return movement comprises at least a first tooth different from said plurality of teeth and formed on the inside wall of the cylinder body and facing a helical groove made in a periphery of the collar, co-operation between said first tooth and said groove immediately after the fusible zone has broken causing at least one of the rod portions to become twisted, said first tooth forming an anti-return abutment after the collar has moved past it as a consequence of said rod portion turning in an opposite direction by elastic effect.

5. A link according to claim 1 , wherein said teeth are spread over one or more spirals.

6. A link according to claim 4 , wherein said teeth are spread over one or more spirals.

7. A link according to claim 1 , wherein said body and said cavity are cylindrical.

8. A link comprising:

a rod having a connection member at each end with an axis going through both connection members, wherein said rod includes a fusible zone in a form of a narrow section lying between a first rod portion connected to a first of the connection members and a second rod portion connected to a second of the connection members, said fusible zone configured to break when tensile force to which said link is subjected is greater than a predetermined value;

a body coaxial about said axis and secured at one end to the first rod portion, said body presenting at its other end an end wall having an orifice through which the second rod portion is capable of sliding, said body defining a cavity in which the fusible zone is housed, together with a collar formed around the second rod portion configured to slide into said cavity in an event of the fusible zone breaking;

a plurality of teeth formed on an inside wall of the body, said teeth being configured to be broken by the collar following breaking of the fusible zone,

wherein said collar defines a groove.

9. A link according to claim 8 , further comprising a first tooth, different from said plurality of teeth, formed on the inside wall of the body and configured to engage said groove after the fusible zone breaks.

10. A link according to claim 9 , wherein said groove is helical.

11. A link according to claim 9 , wherein said groove traverses said collar so that said first tooth enters said groove at one side of said collar and exits said collar at another side of said collar as said collar slides into said cavity after the fusible zone breaks.

12. A link according to claim 11 , wherein said first tooth abuts against said collar after said first tooth exits said collar.

13. A link according to claim 12 , further comprising a second tooth, different from said plurality of teeth, formed on the inside wall of the body and configured to engage said groove after said first tooth exits said collar.

14. A link according to claim 9 , wherein said first tooth is located relative to said plurality of teeth so that said first tooth engages said groove of said collar before said collar breaks said plurality of teeth following breaking of the fusible zone.

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 Dec 1, 2004
From: DUSSERRE-TELMON, GUY; ETOILE, GERARD
To: SNECMA MOTEURS
Reel/Frame 016032/0430 →