GAS SHIELDING ARRANGEMENTS FOR GAS TURBINE ENGINES

A gas shield arrangement for a gas turbine engine, the gas shield arrangement comprising: a first gas shield arranged to cover an inlet of a gas flow path of the gas turbine engine; and a second gas shield arranged to cover a first outlet of the gas flow path of the gas turbine engine.

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Bibliographische Detailangaben
1. Verfasser:	Heason, Christopher
Format:	Patent
Sprache:	eng ; fre ; ger
Schlagworte:	AIR INTAKES FOR JET-PROPULSION PLANTS BLASTING COMBUSTION ENGINES CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS ENGINE PLANTS IN GENERAL GAS-TURBINE PLANTS HEATING HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS LIGHTING MACHINES OR ENGINES IN GENERAL MECHANICAL ENGINEERING NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAMTURBINES STEAM ENGINES WEAPONS
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Beschreibung
Zusammenfassung:	A gas shield arrangement for a gas turbine engine, the gas shield arrangement comprising: a first gas shield arranged to cover an inlet of a gas flow path of the gas turbine engine; and a second gas shield arranged to cover a first outlet of the gas flow path of the gas turbine engine.