Gas turbine engine frame with an integral fluid reservoir...

Power plants – Combustion products used as motive fluid – With lubricators

Reexamination Certificate

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C060S039830, C184S006110

Reexamination Certificate

active

07377098

ABSTRACT:
Disclosed is a structural frame for a gas turbine engine comprising an integral fluid reservoir and air/fluid heat exchanger. A central hub includes a reservoir for storing a fluid and an outer rim circumscribes the hub. A heat exchanger is fluidly coupled to the reservoir and is in simultaneous communication with the fluid and an air stream.

REFERENCES:
patent: 3779345 (1973-12-01), Barnes et al.
patent: 4887424 (1989-12-01), Geidel et al.

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