Helicopter with a turbine power unit fitted with an exhaust scre

Power plants – Combustion products used as motive fluid – With exhaust treatment

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2391273, F02C 712

Patent

active

047139331

ABSTRACT:
A helicopter with a turbine power unit on which fluid flow from the turbine exhaust nozzle, from a turbine bypass duct, from a duct communicating with the compartment housing the turbine engine, and from one or more ducts for cooling internal parts on the helicopter, converges inside a single manifold the output of which is connected to the input of a tubular screening device extending outwards from the manifold and provided with tubular transverse wing contours communicating externally and arranged in such a manner as to prevent the turbine exhaust nozzle from being directly visible from outside, and in such a manner as to define a number of ejectors for activating the fluid streams converging inside the manifold, and for mixing them together with outside air.

REFERENCES:
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patent: 4004416 (1977-01-01), Amelio et al.
patent: 4007587 (1977-02-01), Banthin et al.
patent: 4044555 (1977-08-01), McLoughlin et al.
patent: 4095417 (1978-06-01), Banthin
patent: 4214441 (1980-07-01), Mouritsen et al.
patent: 4295332 (1981-10-01), Steyer et al.
patent: 4355507 (1982-10-01), Coffey et al.
patent: 4537026 (1985-08-01), Nightingale

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