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기록

EXHAUST CONE HEAT EXCHANGER (HEX)

발명심사 중
21청구항 · 4 독립항
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개요

발명자

Henrik Strömberg; Sonny Andersson; Anders Lundbladh

IPC 분류

B64D 37/34B64D 27/10F2C 7/224F2K 1/4

CPC 분류

B64D37/34B64D27/10F2C7/224F2K1/4

An aircraft fuel heating arrangement comprises an exhaust cone for a gas turbine engine, the exhaust cone having an outer body defining an internal cone cavity, the internal cone cavity comprising one or more conduits passing therethrough for communicating fuel through the cavity, and wherein the outer body of the exhaust cone comprises at least one inlet and at least one outlet to allow exhaust gas to pass into through and out of the exhaust cone.

원문 (중국어)

An aircraft fuel heating arrangement comprises an exhaust cone for a gas turbine engine, the exhaust cone having an outer body defining an internal cone cavity, the internal cone cavity comprising one or more conduits passing therethrough for communicating fuel through the cavity, and wherein the outer body of the exhaust cone comprises at least one inlet and at least one outlet to allow exhaust gas to pass into through and out of the exhaust cone.