Assembly of a heat exchanger on a gas turbine engine

Power plants – Combustion products used as motive fluid – Combined with regulation of power output feature

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Details

60 39511, F02C 710, F02C 720

Patent

active

052438155

ABSTRACT:
Apparatus for the compact assembly of a gas turbine engine with a recuperative exhaust gas heat exchanger wherein inlet and outlet ducts of the core of the heat exchanger are supported by support plates attached to the casing of the heat exchanger. The support plates are connected to the engine casing with capability of relative movement between the ducts and the support plates so that thermally produced expansions and contractions are taken up without stress at the support points of the ducts with the support plates and within the heat exchanger. As a consequence, no expansion joints are necessary in the connection lines.

REFERENCES:
patent: 3643733 (1972-02-01), Hall et al.
patent: 3946801 (1976-03-01), Brunell et al.
patent: 3968834 (1976-07-01), Mangus et al.
patent: 4328860 (1982-05-01), Hoffmuller
patent: 4697633 (1987-10-01), Darragh et al.
patent: 4750327 (1988-06-01), Wohrl
patent: 4800955 (1989-01-01), Hagemeister
patent: 5065816 (1991-11-01), Darragh

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