航空機用後部エンジン - GENERAL ELECTRIC COMPANY

Title:

航空機用後部エンジン

Document Type and Number:

Japanese Patent JP6500002

Kind Code:

B2

Abstract:

A propulsion system for an aircraft (200) including a plurality of primary engines is provided. The plurality of primary engines includes at least a first primary engine (252) and a second primary engine (254), each configured for mounting to a respective one of a pair of wings (210) of the aircraft (200). The propulsion system additionally includes an aft engine configured for mounting at a tail section (208) of the aircraft (200). The plurality of primary engines are sized to provide an amount of thrust sufficient for the aircraft (200) to takeoff without use of the aft engine, such that the aft engine may be configured as a non-prime reliable engine.

Inventors:

Patrick Michael Marinan
Kurt David Mallow
Thomas Lee Becker Jr.

Application Number:

JP2016181120A

Publication Date:

April 10, 2019

Filing Date:

September 16, 2016

Export Citation:

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