THRUST INVERSION DEVICE FOR TURBOFAN ENGINE WITH GATE HAVING STICKING EXTERNAL STRUCTURE

Title:

THRUST INVERSION DEVICE FOR TURBOFAN ENGINE WITH GATE HAVING STICKING EXTERNAL STRUCTURE

Document Type and Number:

Japanese Patent JPH10266894

Kind Code:

A

Abstract:

To prevent generation of steps due to pressure difference between surrounding pressure and pressure within a ring channel during flight.

A thrust inversion device of turbo fan engine is provided with an axis rotating gate 7 incorporated into an external wall of a duct 15 of flow of a blower and conducting a thrust inversion to constitute a deflecting obstruction in a direct injection. The gate 7 is constituted by a panel 23 forming external structure and an internal structure 22 connected by a connecting part formed of at least either of two elastic connecting parts 25 and 26 and separated mechanically.

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Inventors:

GONIDEC PATRICK
ROUYER PASCAL GERARD
VAUCHEL GUY BERNARD

Application Number:

JP6357098A

Publication Date:

October 06, 1998

Filing Date:

March 13, 1998

Export Citation:

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Assignee:

HISPANO SUIZA SA

International Classes:

B64D33/00; F02K1/70; (IPC1-7): F02K1/70; B64D33/00

Attorney, Agent or Firm:

Yoshio Kawaguchi (1 person outside)

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