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Patent Searching and Data


Title:
AXIS SYMMETRIC EXHAUST NOZZLE FOR TURBOJET ENGINE
Document Type and Number:
Japanese Patent JPS6463639
Kind Code:
A
Abstract:

PURPOSE: To lighten and improve a credibility of an exhaust nozzle provided with a control flap which is tapered and widens toward its end and so forth by constituting each flap so as to open and close freely syncronously through a prescribed link structure by the operation of a jack.

CONSTITUTION: The axis symmetric exhaust nozzle includes an annular structure which is installed at an extended part of an outlet of a fixed passage 1 and the structure is equipped with a plurality of beams 4 which are supported by a cap 3. A tapering flap 16 is installed at a joint point 10 of the beams 4, a flap 22 which is widened toward its end is installed at a joint part 20 provided at a point of a lower stream of the flap 16 and a cold flap 27 is installed at a joint point 12 of the beams 4. And each flaps 10, 22, 27 can change their angles through levers 34, 35 and a rod 42 by shaking a control lever 48 which is supported by a joint point 11 of the beams 4 through an axis 32 by the operation of a jack 13.


Inventors:
IBU ROJIE JIYAN BERUNUIYU
JIERAARU ERUNESUTO ANDORE JIYU
Application Number:
JP16863988A
Publication Date:
March 09, 1989
Filing Date:
July 06, 1988
Export Citation:
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Assignee:
SNECMA
International Classes:
F02K1/12; (IPC1-7): F02K1/12
Attorney, Agent or Firm:
Yoshio Kawaguchi (2 outside)