Exhaust dissipator/disrupter device

Acoustics – Sound-modifying means – Muffler – fluid conducting type

Patent

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Details

181217, F02K 144

Patent

active

047097809

ABSTRACT:
A dissipator device comprises a container having an inlet for connection to a rocket exhaust and a plurality of exhaust orifices of smaller dimensions than the inlet for exhaust flow out of the container in a plurality of different directions. A deflector member is positioned in the container in alignment with the inlet in the path of incoming exhaust gases for deflecting the flow. A disrupter member is positioned between the inlet and deflector member, and has a through bore defining an orifice of area less than the exhaust flow area at the plane of the disrupter member, so that exhaust gases flow both through and around the disrupter member, substantially reducing the downstream pressure and impingement heat transfer.

REFERENCES:
patent: 2150768 (1939-03-01), Hedrick
patent: 2547936 (1951-04-01), Grow
patent: 2692480 (1958-10-01), Viaud et al.
patent: 2957537 (1960-10-01), Morgan
patent: 2979151 (1961-06-01), Blackwell et al.
patent: 2987136 (1961-12-01), Lilley et al.
patent: 3011584 (1961-12-01), Lemmerman et al.
patent: 3076521 (1963-02-01), House et al.
patent: 3561561 (1971-02-01), Trainor
patent: 3635039 (1972-01-01), Nemcansky et al.

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