A DESIGN OF A ROTATING PROBE FOUR-AXIS TRAVERSE MECHANISM

Zhang Hong; Jiang Haokang; Xiao Ling; Xing Shuchu

Volume 7 Issue 3

Jul. 1992

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Article Navigation > Journal of Aerospace Power > 1992 > 7(3): 241-247,291

Zhang Hong, Jiang Haokang, Xiao Ling, Xing Shuchu. A DESIGN OF A ROTATING PROBE FOUR-AXIS TRAVERSE MECHANISM[J]. Journal of Aerospace Power, 1992, 7(3): 241-247,291.

Citation:

Zhang Hong, Jiang Haokang, Xiao Ling, Xing Shuchu. A DESIGN OF A ROTATING PROBE FOUR-AXIS TRAVERSE MECHANISM[J]. Journal of Aerospace Power, 1992, 7(3): 241-247,291.

Zhang Hong, Jiang Haokang, Xiao Ling, Xing Shuchu. A DESIGN OF A ROTATING PROBE FOUR-AXIS TRAVERSE MECHANISM[J]. Journal of Aerospace Power, 1992, 7(3): 241-247,291.

Citation:

Zhang Hong, Jiang Haokang, Xiao Ling, Xing Shuchu. A DESIGN OF A ROTATING PROBE FOUR-AXIS TRAVERSE MECHANISM[J]. Journal of Aerospace Power, 1992, 7(3): 241-247,291.

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A DESIGN OF A ROTATING PROBE FOUR-AXIS TRAVERSE MECHANISM

Beijing University of Aeronautics and Astronautics

Received Date: 1991-10-01
Publish Date: 1992-07-28

Abstract

Abstract

A mechanism fully controlled by computer and stepping motor can move a probe in four axes (Null,Radial,Tangential and Axial) for completing flow measurement inside the rotor passage of the turbomachine during rotation.The mechanism can also move the probe for flow measurement inside the stator passage as a fixed one.The technical characteristics,principle of operation,construction design and running balance of the mechanism are discussed in detail.