Universalgelenk mit Vereinfachter Struktur
Anmelder: Airbus Operations S.A.S. 🇫🇷
Details
- Veröffentlichungs-Nr.
- EP3222865
- Aktenzeichen
- EP17160221
- Anmeldetag
- 10. März 2017
- Veröffentlichung
- 9. Mai 2018
- Erteilung
- 9. Mai 2018
- Rechtsraum
- EP
- IPC
- F16D3/00F16D3/56
Abstract
The invention relates to a universal joint (100) comprising: - a first band (102a) and a second band (102b) which are separated by a slot (104), are cylindrical and coaxial with one another with respect to a common axis (15), - a first stiffener (108a) whose ends are joined to the first band (102a), and a second stiffener (108b) whose ends are joined to the second band (102b), - a stem (110) which extends between the first stiffener (108a) and the second stiffener (108b), - a crown (112) around the stem (110), - four torsion bars (106a-b), of which two extend between the crown (112) and the first band (102a) and two extend between the crown (112) and the second band (102b). Such a universal joint (100) thus has a relatively simple structure.
Anmelder
- Firma
- Airbus Operations S.A.S.
- Land
- 🇫🇷 Frankreich
Französische Betriebsgesellschaft des Airbus-Konzerns mit Sitz in Toulouse. Zuständig für Entwicklung, Fertigung und Endmontage ziviler Verkehrsflugzeuge.
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