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COUPLING JOINTS TO INTERCONNECT AND TRANSMIT ROTATIONAL TORQUE BETWEEN ADJACENT IMPELLER BODIES IN A TURBOMACHINE

发明专利审中
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19权利要求 · 2 独立
§ Ⅰ

卷宗概要

发明人

Mark J. Kuzdzal; David J. Peer

IPC 分类

F4D 29/28F4D 17/12F4D 29/8F4D 29/26

CPC 分类

F4D29/286F4D17/122F4D29/83F4D29/266

Improved coupling joints configured to interconnect and transmit torque between adjacent impeller bodies in a turbomachine are provided. A plurality of impeller bodies is stacked on a tie bolt. A respective coupling joint is defined by features in adjacent impeller bodies to couple to one another the adjacent impeller bodies. The coupling joint involves a pair of corresponding axially engaging faces and a pair of corresponding radially engaging faces that define a coupling pilot fit. A torque transmitting arrangement is interposed between the axially engaging faces and radially engaging face. The pair of axially engaging faces in operation defines a compressed joint effective to form a seal between the pair of axially engaging faces to inhibit leakage of a process fluid being processed in the compressor section of the turbomachine. This allows elimination of separate seal arrangements, such as otherwise could involve sleeves with O-rings, etc.

原文(中文)

Improved coupling joints configured to interconnect and transmit torque between adjacent impeller bodies in a turbomachine are provided. A plurality of impeller bodies is stacked on a tie bolt. A respective coupling joint is defined by features in adjacent impeller bodies to couple to one another the adjacent impeller bodies. The coupling joint involves a pair of corresponding axially engaging faces and a pair of corresponding radially engaging faces that define a coupling pilot fit. A torque transmitting arrangement is interposed between the axially engaging faces and radially engaging face. The pair of axially engaging faces in operation defines a compressed joint effective to form a seal between the pair of axially engaging faces to inhibit leakage of a process fluid being processed in the compressor section of the turbomachine. This allows elimination of separate seal arrangements, such as otherwise could involve sleeves with O-rings, etc.