Suspension assembly for a turbine engine
The invention concerns a suspension system (7) for a turbomachine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical part (15) articulated on a ball joint housing, the ball joint housing comprising a body (11), and a ball joint nut (16) articulated on the bo...
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| Main Authors | , |
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| Format | Patent |
| Language | English |
| Published |
29.08.2023
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| Subjects | |
| Online Access | Get full text |
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| Abstract | The invention concerns a suspension system (7) for a turbomachine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical part (15) articulated on a ball joint housing, the ball joint housing comprising a body (11), and a ball joint nut (16) articulated on the body (11), the cylindrical part (15) being mounted so as to pivot about its axis in the ball joint nut, characterized in that the cylindrical part (15) is intended to be integral with a fixed part (8) of the turbomachine (1), the body (11) of the ball joint housing being integral with the beam (10). |
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| AbstractList | The invention concerns a suspension system (7) for a turbomachine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical part (15) articulated on a ball joint housing, the ball joint housing comprising a body (11), and a ball joint nut (16) articulated on the body (11), the cylindrical part (15) being mounted so as to pivot about its axis in the ball joint nut, characterized in that the cylindrical part (15) is intended to be integral with a fixed part (8) of the turbomachine (1), the body (11) of the ball joint housing being integral with the beam (10). |
| Author | Hellegouarch, Antoine Elie Garnaud, Quentin Matthias Emmanuel |
| Author_xml | – fullname: Hellegouarch, Antoine Elie – fullname: Garnaud, Quentin Matthias Emmanuel |
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| Notes | Application Number: US201917283863 |
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| PublicationDateYYYYMMDD | 2023-08-29 |
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| RelatedCompanies | SAFRAN AIRCRAFT ENGINES |
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| Snippet | The invention concerns a suspension system (7) for a turbomachine, comprising a beam (10) intended to be attached to a pylon of an aircraft, and a cylindrical... |
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| SubjectTerms | AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION COSMONAUTICS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS PARACHUTES PERFORMING OPERATIONS TRANSPORTING |
| Title | Suspension assembly for a turbine engine |
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