LINK PART FOR AIRCRAFT ENGINE FIXING SYSTEM

PROBLEM TO BE SOLVED: To provide a link part for an engine fixing system designed to have a resonant frequency not near to an excitation frequency of an engine for minimizing problems in weight and mounting of current links. SOLUTION: This link used in the aircraft engine fixing system comprises a f...

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Bibliographische Detailangaben
Hauptverfasser:	BOGER ETHAN, TROUP ROBERT EUGENE, MANTEIGNA JOHN ALAN, WILUSZ CHRISTOPHER JAMES, DYKHUIZEN CORNELIUS HARM, FRANCESCHELLI ANTHONY JOHN, JOSEPH THOMAS PETER
Format:	Patent
Sprache:	eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS AIRCRAFT ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSIONTRANSMISSIONS IN AIRCRAFT AVIATION BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS COSMONAUTICS ENGINE PLANTS IN GENERAL ENGINEERING ELEMENTS AND UNITS EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES PARACHUTES PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS STEAM ENGINES THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	PROBLEM TO BE SOLVED: To provide a link part for an engine fixing system designed to have a resonant frequency not near to an excitation frequency of an engine for minimizing problems in weight and mounting of current links. SOLUTION: This link used in the aircraft engine fixing system comprises a first connector formed on its end and a span part having a second connector formed on the other end. In order to set the resonant frequency of the link apart from the excitation frequency of the engine, concentrated mass is arranged at the span part.