IP Library Granted Patent US 8,919,723
Granted Patent B2
US 8,919,723 · App. 13/561,667 · Granted Dec 30, 2014

Turbojet engine fan duct suspension using connecting rods with elastomer bushing

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Quick Facts
Patent No.
US 8,919,723
App. No.
13/561,667
Granted
Dec 30, 2014
Kind
B2
Abstract

Device for adjusting the length of a connecting rod and consisting of a bushing positioned inside an eye of the said connecting rod, the said bushing comprising at least one element in which there is made a bore to act as a support for a pivot pin intended to pass through the eye, characterized in that the said element is a cylinder made of a metallic material covered by a cylinder made of an elastomeric material so as to form with the metallic cylinder a cylinder homothetic with the previous one, the generatrices of the said cylinders being oriented in a direction that is inclined with respect to the longest length of the said connecting rod.

Claims (20)

1. A device for adjusting the length of a connecting rod comprising:

a bushing positioned inside an eye of the connecting rod, the bushing comprising

first and second metallic cylinders facing each other and being symmetric to each other with respect to a first plane passing through an axis of the connecting rod, the first and second metallic cylinders each including a bore, each bore having an axis oriented perpendicular to the axis of the connecting rod, the axes of the bores being aligned with each other; and

first and second elastomeric cylinders homothetic with and surrounding the first and second metallic cylinders, respectively,

wherein generatrices of the metallic and elastomeric cylinders are oriented in a direction that is inclined with respect to the axis of the connecting rod, and

wherein a space is provided between internal faces of the first and second metallic cylinders facing each other, the space presenting a disc shape with parallel faces.

2. The device according to claim 1 , wherein the first and second metallic cylinders are symmetric to each other about a second plane, orthogonal to the first plane, so that the first and second metallic cylinders are geometrically identical.

3. A connecting rod comprising:

an eye at an end thereof; and

a bushing positioned inside the eye, the bushing comprising:

first and second metallic cylinders facing each other and being symmetric to each other with respect to a first plane passing through an axis of the connecting rod, the first and second metallic cylinders each including a bore, each bore having an axis oriented perpendicular to the axis of the connecting rod, the axes of the bores being aligned with each other; and

first and second elastomeric cylinders homothetic with and surrounding the first and second metallic cylinders, respectively,

wherein generatrices of the metallic and elastomeric cylinders are oriented in a direction that is inclined with respect to the axis of the connecting rod, and

wherein a space is provided between internal faces of the first and second metallic cylinders facing each other, the space presenting a disc shape with parallel faces.

4. The connecting rod according to claim 1 , wherein the eye presents, in cross section on the first plane that passes through the axis of the connecting rod and a direction of the pivot pin, a herringbone shape.

5. The connecting rod according to claim 3 , wherein the eye presents, in cross section on a plane orthogonal to the direction of the generatrices of the cylinders, a shape of a circle.

6. The connecting rod according to claim 3 further comprising a pivot pin passing through the eye,

wherein the pivot pin comprises at least one end stop which limits movement of the bushing in a direction transverse to a direction parallel to the axis of the connecting rod.

7. The connecting rod according to claim 6 , wherein the pivot pin further comprises a clamping ring able to push the bushing towards the end stop.

8. The connecting rod according to claim 7 , wherein the eye presents, in cross section on the plane passing through the axis of the connecting rod and through the pivot pin, a herringbone shape with a vertex oriented in a direction of a shank of the connecting rod.

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 Jul 30, 2012
From: BELLABAL, FRANCOIS ROBERT; RIVIERE, THOMAS GERARD DANIEL
To: SNECMA
Reel/Frame 028676/0220 →