Power plants – Reaction motor – Interrelated reaction motors
Reexamination Certificate
2004-12-07
2008-11-25
Kim, Ted (Department: 3746)
Power plants
Reaction motor
Interrelated reaction motors
C060S039080
Reexamination Certificate
active
07454894
ABSTRACT:
A gas turbine engine is provided with an oil cooler which receives cooling air from a turbo fan. At times when the turbo fan is operating at lower speeds, the volume of cooling air is also lowered. At such times, a supplemental airflow is provided over heat exchangers in the oil cooler. The supplemental airflow includes a supplemental airflow fan and valve for selectively controlling the supplemental airflow over the heat exchangers.
REFERENCES:
patent: 2625009 (1953-01-01), Leggett et al.
patent: 4397148 (1983-08-01), Stockton et al.
patent: 4546605 (1985-10-01), Mortimer et al.
patent: 4782658 (1988-11-01), Perry
patent: 5038560 (1991-08-01), Seed
patent: 5269135 (1993-12-01), Vermejan et al.
patent: 5553449 (1996-09-01), Rodgers et al.
patent: 5987877 (1999-11-01), Steiner
patent: 6282881 (2001-09-01), Beutin et al.
patent: 6931834 (2005-08-01), Jones
Eiler Donald C.
Larkin Michael J.
Carlson & Gaskey & Olds PC
Kim Ted
United Technologies Corporation
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