MOUNTING ASSEMBLY FOR GAS TURBINE ENGINE FLUID CONDUIT

The present disclosure is directed to a mounting assembly 100 for a fluid conduit 70. The mounting assembly 100 includes a casing 34, 38, a first fluid conduit segment 74, and a second fluid conduit segment 76. A fitting 102 is spaced apart from the casing 34, 38. The fitting 102 couples the first f...

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Bibliographische Detailangaben
Hauptverfasser:	FLANAGAN, James Scott, BROWN, Jerome David, LEMON, Donald Timothy
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION APPARATUS COMBUSTION ENGINES COMBUSTION PROCESSES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MECHANICAL ENGINEERING WEAPONS
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Beschreibung
Zusammenfassung:	The present disclosure is directed to a mounting assembly 100 for a fluid conduit 70. The mounting assembly 100 includes a casing 34, 38, a first fluid conduit segment 74, and a second fluid conduit segment 76. A fitting 102 is spaced apart from the casing 34, 38. The fitting 102 couples the first fluid conduit segment 74 and the second fluid conduit segment 76. A bracket 104 includes a casing mounting portion 130 coupled to the casing 34, 38, a first fitting mounting portion 136 spaced apart from the casing mounting portion 130 and coupled to the fitting 102, and a thickness 120. The thickness 120 of the bracket 104 permits the fitting 102 to move relative to the casing 34, 38.