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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 5. Отображено 5.
23-07-2009 дата публикации

A MODULAR ROTOR BLADE FOR A POWER-GENERATING TURBINE AND A METHOD FOR ASSEMBLING A POWER-GENERATING TURBINE WITH MODULAR ROTOR BLADES

Номер: CA0002703641A1
Принадлежит:

The invention relates to a modular rotor blade for a power generating turbine that allows simple replacement of individual rotor blade sections in case of damage to or malfunction of a section. The modular rotor blade comprises at least two rotor blade sections (10, 11), wherein each rotor blade section (10, 11) comprises at least one connecting part (14, 16) having at least one conical opening (41, 42), the connecting parts (14, 16) of adjacent rotor blade sections (10, 11) rest against each other such that the conical openings (41, 42) of the connecting parts (14, 16) are aligned with each other and form a continuous conical connecting opening, receiving means (18) for receiving tensioning means (28) are arranged at the smaller diameter end of the conical connecting opening, a conical bolt (30) corresponding to the continuous conical connecting opening is arranged therein, and at least one tensioning means (28) passing through the conical bolt (30) and tensioning the conical bolt (30) ...

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29-12-2010 дата публикации

A modular rotor blade for a power-generating turbine and a method for assembling a power-generating turbine with modular rotor blades

Номер: CN0101932828A
Принадлежит:

The invention relates to a modular rotor blade for a power generating turbine that allows simple replacement of individual rotor blade sections in case of damage to or malfunction of a section. The modular rotor blade comprises at least two rotor blade sections (10, 11), wherein each rotor blade section (10, 11) comprises at least one connecting part (14, 16) having at least one conical opening (41, 42), the connecting parts (14, 16) of adjacent rotor blade sections (10, 11) rest against each other such that the conical openings (41, 42) of the connecting parts (14, 16) are aligned with each other and form a continuous conical connecting opening, receiving means (18) for receiving tensioning means (28) are arranged at the smaller diameter end of the conical connecting opening, a conical bolt (30) corresponding to the continuous conical connecting opening is arranged therein, and at least one tensioning means (28) passing through the conical bolt (30) and tensioning the conical bolt (30) ...

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