Turbomachine with contrarotating fans

Rotary kinetic fluid motors or pumps – Working fluid passage or distributing means associated with... – With runner shaft of specific shape or material

Reexamination Certificate

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C060S226100, C416S129000

Reexamination Certificate

active

07458773

ABSTRACT:
A turbomachine comprising: a gas generator for producing combustion gas; a turbine section through which the combustion gas passes and comprising first and second rows of contrarotating turbine rotor blades respectively driving first and second low-pressure shafts in rotation; and a fan section comprising a first row of fan blades mounted on a front fan shaft that is connected to an upstream end of the first low-pressure shaft, and a second row of fan blades axially offset from the first row and mounted on a rear fan shaft that is connected to an upstream end of the second low-pressure shaft, the front fan shaft being connected to the upstream end of the first low-pressure shaft via a removable sleeve for transmitting torque.

REFERENCES:
patent: 4375906 (1983-03-01), Roberts et al.
patent: 4744214 (1988-05-01), Monsarrat et al.
patent: 5274999 (1994-01-01), Rohra et al.
patent: 2004/0055276 (2004-03-01), John Lewis et al.
patent: 2007/0006569 (2007-01-01), Brault et al.
patent: 0 298 014 (1989-01-01), None
patent: 0 521 379 (1993-01-01), None
patent: 1 403 485 (2004-03-01), None
European Search Report, FA 654219, dated Mar. 14, 2005.
U.S. Appl. No. 12/052,108, filed Mar. 20, 2008, Brault, et al.

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