Connecting element including a sacrificial ball joint, particularly for engine mounts
Patent Information
- Application Number
- FR2024004804
- Authority / Receiving Office
- FR · FR
- Patent Type
- Applications
- Current Assignee / Owner
- Filing Date
- 2024-05-07
- Publication Date
- 2025-11-14
- Estimated Expiration
- 2044-05-07
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Abstract
Claims
and on which is fixed the inner ring (5) of the sacrificial ball joint (3c).
7. Connecting element (1) according to claim 6, wherein the fastening device further comprises a groove (8) formed on the body (2) or on the shaft (9) in the extension of the thread (7) and inside which is housed a protrusion of the inner ring (5) of the sacrificial ball joint (3c).
8. Connecting element (1) according to claim 6, wherein the fastening device further comprises a locking nut (12) for the sacrificial ball joint (3c), mounted on the body (2) or on the shaft (9).
9. Connecting element (1) according to any one of claims 1 to 8, wherein the first and second ball joints (3a, 3b) comprise two parallel axes of rotation (RI) and wherein the sacrificial ball joint (3c) comprises an axis of rotation (R2) orthogonal to said axes of rotation (RI).
10. Connecting element (1) according to any one of claims 1 to 9, wherein a first principal face A of the body 2 comprises a nickel and / or cobalt alloy and a second opposite principal face B of the body 2 comprises a titanium and / or nickel alloy. [Fig. 1] [Fig. 3] [Fig. 4]
Citation Information
Patent Citations
Engine assembly for aircraft
US20070205323A1
Rear engine attachment for an aircraft engine
US20200361618A1