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Небесная энциклопедия

Космические корабли и станции, автоматические КА и методы их проектирования, бортовые комплексы управления, системы и средства жизнеобеспечения, особенности технологии производства ракетно-космических систем

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Применить Всего найдено 3. Отображено 3.
23-03-2011 дата публикации

Stator assembly including bleed ports for turbine engine compressor

Номер: GB0002454434B
Автор: DAMLE SACHIN V, ADJAN BACHAR, FREGOE JERRY MAR PHILIP, SACHIN V DAMLE, BACHAR ADJAN, JERRY MAR PHILIP FREGOE
Принадлежит: SOLAR TURBINES INC, SOLAR TURBINES INCORPORATED

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Номер записи: 1
23-10-2012 дата публикации

Stator assembly including bleed ports for turbine engine compressor

Номер: US8292567B2
Автор: Bachar Adjan, Jerry Mar Philip Fregoe, Sachin V. Damle
Принадлежит: Caterpillar Inc

A stator assembly for a turbine engine is disclosed. The stator assembly has a stator support ring, a plurality of stator vanes protruding radially inwardly from the stator support ring, and at least one bleed port disposed on the stator support ring between at least two adjacent stator vanes of the plurality of stator vanes. The at least one bleed port defines an oblong profile having a first end terminating near a leading edge of a first stator vane of the at least two adjacent stator vanes, and a second end, substantially opposed from the first end, terminating near a trailing edge of a second stator vane of the at least two adjacent stator vanes. The profile may be concave toward a suction sidewall of the second stator vane of the at least two adjacent stator vanes.

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Номер записи: 2
01-01-2009 дата публикации

Stator assembly including bleed ports for turbine engine compressor

Номер: US20090000306A1
Автор: Bachar Adjan, Jerry Mar Philip Fregoe, Sachin V. Damle
Принадлежит: Caterpillar Inc

A stator assembly for a turbine engine is disclosed. The stator assembly has a stator support ring, a plurality of stator vanes protruding radially inwardly from the stator support ring, and at least one bleed port disposed on the stator support ring between at least two adjacent stator vanes of the plurality of stator vanes. The at least one bleed port defines an oblong profile having a first end terminating near a leading edge of a first stator vane of the at least two adjacent stator vanes, and a second end, substantially opposed from the first end, terminating near a trailing edge of a second stator vane of the at least two adjacent stator vanes. The profile may be concave toward a suction sidewall of the second stator vane of the at least two adjacent stator vanes.

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Номер записи: 3