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Title:
Re-heat and cogeneration heat load consistency by capacity consistency
Document Type and Number:
Japanese Patent JP6198856
Kind Code:
B2
Abstract:
One example of a gas turbine engine may include a gas generator, a reheat combustor that is disposed downstream of the gas generator, and a power turbine that is disposed downstream of the reheat combustor and includes a plurality of nozzle guide vanes. The reheat combustor is configured to increase a fuel flow so as to increase a temperature of the reheat combustor and match a required exhaust temperature. The nozzle guide vanes are configured to increase a real capacity at a power turbine inlet in proportion with the required exhaust temperature. A constant apparent capacity at a gas generator exit upstream of the reheat combustor remains constant, in response to proportionately increasing the temperature and the real capacity with respect to one another.

Inventors:
Jean-Francois Lebel
Carl Carson
Application Number:
JP2015561332A
Publication Date:
September 20, 2017
Filing Date:
December 23, 2013
Export Citation:
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Assignee:
Industrial Turbine Company (UK) Limited
International Classes:
F02C9/22; F01D15/08; F02C3/073; F02C3/10; F02C3/14; F02C6/00; F02C9/28; F23R3/34
Domestic Patent References:
JP2003083081A
JP3100331A
JP2002285860A
JP2001140657A
JP2011102548A
JP42023846B1
JP33007755B1
JP3175117A
JP5179904A
Attorney, Agent or Firm:
Einzel Felix-Reinhard
Morita Taku
Junichi Maekawa
Hiroyasu Ninomiya
Ueshima



 
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