Nova Patents
EP1568868A3

High by-pass ratio turbofan

Abstract

Turbojet engine, comprising at least one fan, a compressor, a combustion chamber, a turbine, and a substantially cylindrical envelope (10) rigid and fixed at its upstream end (19) on an intermediate casing and at its downstream end (26) on an exhaust casing, the casing (10) ensuring a transmission of forces between the intermediate casing and the exhaust casing.

EP1568868A3, drawing sheet 1
Sheet 1 of 1

Term

Term ended

Projected expiry passed 20 January 2025, 1.7 years ago.

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