THRUST REVERSER OF TURBOJET ENGINE Russian patent published in 1996 - IPC

Abstract RU 2069782 C1

FIELD: aircraft engine engineering. SUBSTANCE: tube for inversion of the flow reversed by thrust reverser of a turbojet engine is bounded with the edge for changing the direction from one side. The edge is made in block with the fixed portion. The curvature of longitudinal sections (A, B, C) of the edge for changing the direction varies from one side edge to the other at the tube for inversion. EFFECT: improved control. 4 cl, 4 dwg

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RU 2 069 782 C1

Authors

Feliks Karimali[Fr]

Mishel' Zhan Ljus'En Legra[Fr]

Dates

1996-11-27—Published

1992-08-19—Filed