ENGINE BACKBONE BENDING REDUCTION

The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first e...

Ausführliche Beschreibung

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Bibliographische Detailangaben
Hauptverfasser:	KHANDEPARKER MAHESH, COLEMAN JONATHAN EDWARD, SCHELFAUT TIMOTHY LEO, GARDNER DONALD L, JOSEPH THOMAS PETER, METZ ANTHONY MICHAEL, SHINDE KUDUM
Format:	Patent
Sprache:	chi ; 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 EQUIPMENT FOR FITTING IN OR TO AIRCRAFT FLYING SUITS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING PARACHUTES PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	The present invention discloses methods, apparatus, systems and articles of manufacture. A mechanical linkage for mounting a gas turbine engine to a pylon includes: a bending restraint having a first end and a second end; a first joint at the first end of the bending restraint to connect the first end of the bending restraint to a fan section of the gas turbine engine; and a second joint at the second end of the bending restraint to connect the second end of the bending restraint to the pylon. 公开方法、设备、系统和制品。一种用于将燃气涡轮发动机安装到支架的机械连杆机构包含：弯曲约束件，其具有第一端和第二端；第一接头，其在弯曲约束件的第一端处，使弯曲约束件的第一端连接到燃气涡轮发动机的风扇区段；以及第二接头，其在弯曲约束件的第二端处，使弯曲约束件的第二端连接到支架。