Fan control apparatus

Aeronautics and astronautics – Aircraft – heavier-than-air – Fluid sustained

Reexamination Certificate

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C244S02300R, C060S233000

Reexamination Certificate

active

08038091

ABSTRACT:
When a FADEC detects an abnormality in any of engine+compressor combinations, a FCC controls the amount of air for driving the fan to a level that is lower than that before the abnormality has been detected, until a state is assumed in which the normally operating engine+compressor combination can supply the air at a flow rate necessary for a fan to generate a propulsion force that has been attained before the abnormality has been detected. As a result, the normally operating engine+compressor combination can be prevented from the occurrence of a surge and a resultant overload state. Therefore, when some drive sources from a plurality of drive sources fail, normally operating drive sources can be prevented from being in an overload state.

REFERENCES:
patent: 3095165 (1963-06-01), Rowe
patent: 3174284 (1965-03-01), McCarthy
patent: 3381295 (1968-04-01), Blackledge
patent: 3618875 (1971-11-01), Kappus
patent: 5082079 (1992-01-01), Lissaman et al.
patent: 6260796 (2001-07-01), Klingensmith
patent: 7188803 (2007-03-01), Ishiba
patent: 11-255199 (1999-09-01), None
patent: 2006-213168 (2006-08-01), None
patent: 2007-022268 (2007-02-01), None
patent: 2007--55372 (2007-03-01), None
patent: 2007-125976 (2007-05-01), None
JP2007-022268A Machine translation, Feb. 2007.
S. Iwase, “Unsteady Flow inside the Single Rotor Blade Row with Multistage Tip Turbine (2ndReport: Effects of bulkheads positioning on efficiency),” vol. 34, No. 2, Mar. 2006.
S. Iwase, et al., “The Fan Driven by High Pressure Tip Turbine,” vol. 33, No. 1, Jan. 2005.

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