An engine mount may include a clevis and a lug defining a hole therethrough. A pin may be joined to the clevis and may extend through the hole of the lug with the pin and the lug defining a clearance therebetween. A trigger system may be disposed on the lug and operatively associated with the pin.
ENGINE MOUNT WAITING FAIL SAFE LUG JOINT WITH REDUCED DYNAMIC AMPLIFICATION FACTOR
AUSFALLSICHERE STOSSVERBINDUNG FÜR MOTORLAGER MIT VERRINGERTEM DYNAMISCHEM VERSTÄRKUNGSFAKTOR
BÂTI MOTEUR COMPRENANT UN ASSEMBLAGE À OREILLES À SÛRETÉ INTÉGRÉE EN ATTENTE, À FACTEUR D'AMPLIFICATION DYNAMIQUE RÉDUIT
15.02.2023
Patent
Elektronische Ressource
Englisch
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / F02C Gasturbinenanlagen , GAS-TURBINE PLANTS / F16B DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES , Vorrichtungen zum Befestigen oder Sichern von Konstruktionselementen oder Maschinenteilen, z.B. Nägel, Bolzen, Schrauben, Sprengringe, Klemmen, Klammern oder Keile |
Engine Mount Waiting Fail Safe Lug Joint with Reduced Dynamic Amplification Factor
Europäisches Patentamt | 2015
|Engine mount waiting fail safe lug joint with reduced dynamic amplification factor
Europäisches Patentamt | 2019
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