General Electric GE38

http://dbpedia.org/resource/General_Electric_GE38 an entity of type: MeanOfTransportation

The General Electric GE38 is a gas turbine developed by GE Aviation for turboprop and turboshaft applications. It powers the Sikorsky CH-53K King Stallion as the T408. rdf:langString
Le General Electric GE38 est un turbomoteur de conception américaine en cours de développement (2017). Conçu par GE Aviation pour être à la fois utilisé comme turbomoteur ou turbopropulseur, il a actuellement pour objectif de propulser le Sikorsky CH-53K King Stallion, portant alors la désignation de T408. rdf:langString
ゼネラル・エレクトリック GE38（General Electric GE38）（アメリカ軍識別符号：T407/T408）は、GE・アビエーションが開発したガスタービンエンジン。 rdf:langString
O General Electric GE38 é um motor de turbina a gás desenvolvido pela GE Aviation para aplicações turboélice e turboeixo. Este motor deve ser utilizado no como T408. rdf:langString
rdf:langString General Electric GE38
rdf:langString General Electric GE38
rdf:langString ゼネラル・エレクトリック GE38
rdf:langString General Electric GE38
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rdf:langString * Allison T406 * Honeywell T55 * Pratt & Whitney PW150
rdf:langString About
rdf:langString a 3-Stage Power Turbine, a 2-stage-single crystal cooled HP turbine
rdf:langString GE Aviation.
rdf:langString * CFE CFE738 * General Electric GE36
rdf:langString Turboprop/turboshaft
rdf:langString The General Electric GE38 is a gas turbine developed by GE Aviation for turboprop and turboshaft applications. It powers the Sikorsky CH-53K King Stallion as the T408.
rdf:langString Le General Electric GE38 est un turbomoteur de conception américaine en cours de développement (2017). Conçu par GE Aviation pour être à la fois utilisé comme turbomoteur ou turbopropulseur, il a actuellement pour objectif de propulser le Sikorsky CH-53K King Stallion, portant alors la désignation de T408.
rdf:langString ゼネラル・エレクトリック GE38（General Electric GE38）（アメリカ軍識別符号：T407/T408）は、GE・アビエーションが開発したガスタービンエンジン。
rdf:langString O General Electric GE38 é um motor de turbina a gás desenvolvido pela GE Aviation para aplicações turboélice e turboeixo. Este motor deve ser utilizado no como T408.
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xsd:date 1989-12-26
rdf:langString * List of aircraft engines
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