THERMALLY PROTECTED THERMOPLASTIC DUCT AND ASSEMBLY

A cooling apparatus for a gas turbine engine includes a wall structure defining an air flowpath, the wall structure comprising a thermoplastic material; and a thermal barrier layer surrounding the wall structure. 一种用于燃气涡轮发动机的冷却装置包括：限定空气流径的壁结构，该壁结构包括热塑性材料；以及包绕壁结构的热障层。...

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Bibliographische Detailangaben
1. Verfasser:	SCHOFIELD RONALD BRUCE
Format:	Patent
Sprache:	chi ; eng
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LAYERED PRODUCTS LAYERED PRODUCTS, i.e. PRODUCTS BUILT-UP OF STRATA OF FLAT ORNON-FLAT, e.g. CELLULAR OR HONEYCOMB, FORM LIGHTING MECHANICAL ENGINEERING PERFORMING OPERATIONS TRANSPORTING WEAPONS
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Zusammenfassung:	A cooling apparatus for a gas turbine engine includes a wall structure defining an air flowpath, the wall structure comprising a thermoplastic material; and a thermal barrier layer surrounding the wall structure. 一种用于燃气涡轮发动机的冷却装置包括：限定空气流径的壁结构，该壁结构包括热塑性材料；以及包绕壁结构的热障层。