IP Library Granted Patent US 6,986,482
Granted Patent B2
US 6,986,482 · App. 10/450,701 · Granted Jan 17, 2006

Suspension part of a turbojet 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 6,986,482
App. No.
10/450,701
Granted
Jan 17, 2006
Kind
B2
Abstract

A suspension part for mounting a turbojet engine includes two ends equipped with two elements, juxtaposed in a widthwise direction of the suspension part, for fixing the suspension part to the fixed structure. The ends are shaped into pairs of yokes respectively flanking connecting rods and each including fixing elements and a bearing of a journal of a connecting rod which bearing is situated underneath a fixing element. The suspension part also includes slots passing through the two ends of the suspension part and running between the yokes without running over a central portion of the suspension part. Each of the yokes has an upper portion with an additional thickness located on an inside of each of the yokes.

Claims (27)

1. A suspension part for mounting a turbojet engine to a fixed structure, said suspension part comprising:

at least two connecting rods; and

two ends equipped with two fixing elements, juxtaposed in a widthwise direction of the suspension part, the ends being shaped into pairs of yokes respectively flanking the connecting rods and each comprising one of the fixing elements and a drilling for a journal of a connecting rod, the drilling being situated underneath said fixing element,

wherein slots passing through the two ends of the suspension part run between the yokes without running over a central portion of the suspension part, and

each of said yokes has an upper portion with an additional thickness located on an inside of each of said yokes.

2. The suspension part as claimed in claim 1 , wherein the yokes are thicker at the fixing elements than said yokes are at the drillings for the journal.

3. The suspension part as claimed in claim 1 , wherein said additional thickness is located over the connecting rods.

4. The suspension part as claimed in claim 1 , wherein each of said slots is narrower than a shortest distance between said yokes.

5. The suspension part as claimed in claim 1 , wherein each of said yokes has a bottom portion located under said upper portion and configured to support said connecting rods.

6. The suspension part as claimed in claim 1 , wherein each of said slots runs toward said central portion at least as far as the ends of the yokes.

7. The suspension part as claimed in claim 1 , wherein each of said slots ends with an opening which is larger than other portions of the slots.

8. The suspension part as claimed in claim 1 , further comprising ribs configured to connect corresponding yokes together, said corresponding yokes being positioned at opposite ends of said suspension part.

9. The suspension part as claimed in claim 8 , wherein each of said ribs has an arch shape with a thinner portion under said central portion arid a thicker portion toward said yokes.

10. A suspension part for mounting an engine to a fixed structure, said suspension part comprising:

at least two fixation elements positioned at each end of said suspension part;

a pair of yokes at each end of said suspension part, each yoke comprising an upper portion located under one of said fixation element and a lower portion located under said upper portion, wherein a distance between inner faces of the upper portions for two yokes of said pair of yokes at a same end of the suspension part is shorter than a distance between inner faces of corresponding lower portions for said two yokes at said same end; and

at least two slots, each slot passing through one of the ends of said suspension part and between two of said yokes without reaching a central portion of the suspension part.

11. The suspension part as claimed in claim 10 , further comprising at least two connecting rods, each connecting rod being connected to a pair of said yokes.

12. The suspension part as claimed in claim 11 , wherein said connecting rods are configured to be articulated to said engine.

13. The suspension part as claimed in claim 11 , wherein said connecting rods are connected to said yokes below said upper portions of said yokes.

14. The suspension part as claimed in claim 13 , wherein said connecting rods are connected to said yokes at said lower portions.

15. The suspension part as claimed in claim 14 , wherein said slots define openings which are narrower than said distance between said inner faces of said corresponding lower portions.

16. The suspension part as claimed in claim 15 , wherein said slots define openings which are narrower than said distance between said inner faces of said upper portions.

17. The suspension part as claimed in claim 14 , wherein said upper portions are thicker than said lower portions.

18. The suspension part as claimed in claim 10 , wherein each of said slots ends with an opening which is larger than other portions of the slots.

19. The suspension part as claimed in claim 10 , further comprising ribs configured to connect corresponding yokes together, said corresponding yokes being positioned at opposite ends of said suspension part.

20. The suspension part as claimed in claim 19 , wherein each of said ribs has an arch shape with a thinner portion under said central portion and a thicker portion toward said yokes.

Assignments (2)
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 →