Variable area exhaust nozzle

Fluid sprinkling – spraying – and diffusing – Reaction motor discharge nozzle – With means controlling amount – shape or direction of...

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Details

23926533, 23926519, 60271, B64C 1500

Patent

active

052210480

ABSTRACT:
A variable area exhaust nozzle for aircraft jet engines for optimizing thrust of the engines under different conditions, the nozzle having a fixed wall (11) and at the end thereof, two pivoting half shells (13) hinged around an axis of rotation A interdependent of the fixed wall, and having lateral edges (18) which are inserted into sliding tracks mounted in fixed beams (12), also interdependently of the fixed wall. A seal (35) ensures airtightness between the fixed wall (11) and the pivoting half shells (13).

REFERENCES:
patent: 4577814 (1986-03-01), Bayle-Laboure et al.

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