IP Library Granted Patent US 9,581,047
Granted Patent B2
US 9,581,047 · App. 14/779,931 · Granted Feb 28, 2017

Ball joint device for suspending a turbine engine on a pylon or suspending equipment on the body of the turbine engine

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 9,581,047
App. No.
14/779,931
Granted
Feb 28, 2017
Kind
B2
Abstract

Ball joint device for suspending a turbine engine from a pylon or suspending equipment on the body of the turbine engine, comprising a connecting rod, one end of which bears a ball and which is inserted between the two lugs of a clevis, the ball having a boring for the passage of a spindle having an axial boring for mounting a screw for clamping and axial locking the ball, the ball being axially locked by clamping between a bushing and a ring which carries removable means for axially retaining the ring with respect to the clevis during an operation of dismantling the device.

Claims (14)

1. Ball joint device for suspending a turbine engine from a pylon or suspending equipment on the body of a turbine engine, comprising a first element, one end of which bears a ball and which is inserted between two lugs of a second element, the ball having a boring for the passage of a spindle, the ends of which pass through bushings mounted so as to be clamped in openings of the lugs, the device further comprising a screw or a nut co-operating with the spindle in order to ensure clamping and axial locking of the ball joint, wherein the ball joint is mounted so as to be clamped between a first of the aforementioned bushings and a first end of a ring, cylindrical in shape, the ring being mounted around a part of the spindle and engaged in a second of the aforementioned bushings, the second bushing comprising a rim axially supported on an external lateral face of the lug in which the second bushing is mounted and having a free end extending beyond an internal face of the lug, this ring passing through the second bushing and being urged axially towards and against the ball joint by clamping of the screw or of the nut, the ring having, at the first end thereof, removable means for axial retention of the ring with respect to the second element during an operation of dismantling of the device.

2. Device according to claim 1 , wherein the removable axial retention means comprise a circlip which is removably mounted on the first end of the ring and is capable of being supported on the second of the aforementioned bushings in the event that the screw or the nut is unscrewed.

3. Device according to claim 2 , wherein the circlip comprises a split ring which is accommodated in an external annular groove of the first end of the ring.

4. Device according to claim 1 , wherein the spindle comprises an axial boring for mounting the screw, the head of which is intended to be supported on one end of the spindle, or the spindle is rigidly connected to one end of a threaded rod for screwing the nut intended to be supported on one end of the ring, or the spindle comprises, at one end, a tapped opening in which a screw is screwed, the head of which is intended to be supported on one end of the ring.

5. Device according to claim 1 , wherein the ring comprises, at the second end thereof, an internal annular rim, on the internal periphery of which the head of the screw or a nut is intended to be supported.

6. Ball joint device for suspending a turbine engine from a pylon or suspending equipment on the body of a turbine engine, comprising a first element, one end of which bears a ball and which is inserted between two lugs of a second element, the ball having a boring for the passage of a spindle, the ends of which pass through bushings mounted so as to be clamped in openings of the lugs, the device further comprising a screw or a nut co-operating with the spindle in order to ensure clamping and axial locking of the ball joint, wherein the ball joint is mounted so as to be clamped between a first of the aforementioned bushings and a first end of a cylindrical ring which is mounted around a part of the spindle and, in a second of the aforementioned bushings, this ring being urged towards the ball joint by clamping of the screw or of the nut, and having, at the first end thereof, removable means for axial retention of the ring with respect to the second element during an operation of dismantling of the device,

wherein the device comprises a third bushing mounted so as to be clamped in the opening of the lug in which the first bushing is mounted, these first and third bushings being coaxial and mounted side by side in the opening of the lug, each of these bushings comprising an external annular rim for support on a lateral face of the lug of the second element.

7. Device according to claim 6 , wherein the third bushing is inserted between the aforementioned lateral face of the lug and an external annular rim of the spindle, this rim being axially urged towards the third bushing by clamping of the screw or of the nut.

8. Device according to claim 6 , wherein the first and third bushings are separated from one another by an axial clearance.

9. Device according to claim 1 , wherein the first element is a connecting rod and the second element is a clevis, or the first element is a clevis and the second element is a connecting rod.

10. Turbine engine comprising at least one ball joint device comprising a first element, one end of which bears a ball and which is inserted between two lugs of a second element, the ball having a boring for the passage of a spindle, the ends of which pass through bushings mounted so as to be clamped in openings of the lugs, the device further comprising a screw or a nut co-operating with the spindle in order to ensure clamping and axial locking of the ball joint, wherein the ball joint is mounted so as to be clamped between a first of the aforementioned bushings and a first end of a ring, cylindrical in shape, the ring being mounted around a part of the spindle and engaged in a second of the aforementioned bushings, the second bushing comprising a rim axially supported on an external lateral face of the lug in which the second bushing is mounted and having a free end extending beyond an internal face of the lug, this ring passing through the second bushing and being urged axially towards and against the ball joint by clamping of the screw or of the nut, the ring having, at the first end thereof, removable means for axial retention of the ring with respect to the second element during an operation of dismantling of the device.

11. Device according to claim 1 , wherein the device comprises a third bushing mounted so as to be clamped in the opening of the lug in which the first bushing is mounted, these first and third bushings being coaxial and mounted side by side in the opening of the lug, each of these bushings comprising an external annular rim for support on a lateral face of the lug of the second element.

12. Device according to claim 11 , wherein the third bushing is inserted between the aforementioned lateral face of the lug and an external annular rim of the spindle, this rim being axially urged towards the third bushing by clamping of the screw or of the nut.

13. Device according to claim 11 , wherein the first and third bushings are separated from one another by an axial clearance.

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 Oct 26, 2015
From: BESNARD, MARYLINE; LAPORTE, ARNAUD GUY
To: SNECMA
Reel/Frame 036882/0616 →