[go: up one dir, main page]

JPS5783612A - Device for monitoring gap on tip of moving vane of axial-flow turbo-machine - Google Patents

Device for monitoring gap on tip of moving vane of axial-flow turbo-machine

Info

Publication number
JPS5783612A
JPS5783612A JP15831180A JP15831180A JPS5783612A JP S5783612 A JPS5783612 A JP S5783612A JP 15831180 A JP15831180 A JP 15831180A JP 15831180 A JP15831180 A JP 15831180A JP S5783612 A JPS5783612 A JP S5783612A
Authority
JP
Japan
Prior art keywords
moving vane
tip
gap
laser
rays
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Pending
Application number
JP15831180A
Other languages
Japanese (ja)
Inventor
Koichi Tsuzuki
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Hitachi Ltd
Original Assignee
Hitachi Ltd
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Hitachi Ltd filed Critical Hitachi Ltd
Priority to JP15831180A priority Critical patent/JPS5783612A/en
Publication of JPS5783612A publication Critical patent/JPS5783612A/en
Pending legal-status Critical Current

Links

Landscapes

  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

PURPOSE: To simply minotor the size of the gap on the tip of a moving vane, by irradiating laser rays in parallel with the axis of rotation, upon a point at a prescribed distance from the inside surface of a casing and by monitoring whether or not the tip of the moving vane intercepts the laser light rays.
CONSTITUTION: A laser light emitter 6 is housed in an opening 3a' provided in a stationary valne 3a located downstream to a moving vane 4. Laser rays 8 generated by the laser light emitter 6' are conducted into the gap 5 between the moving vane 4 and the inside surface 2' of a casing by way of a lens 6a, a reflector 6c, etc. The laser rays 8 having passed through the gap 5 are received by the receiver 7a of a laser ray reception unit 7 provided in an opening 8b' and are conducted to a photomultiplier tube 7' through an optical fiber 7" and converted into an electric signal (e). When the gap 5 on the tip of the moving vane 4 decreases and the moving vane intercepts the laser rays 8 and the electric signal (e) is cut off, the rotational frequency is reduced to prevent the moving vane from coming into contact with the casing 2.
COPYRIGHT: (C)1982,JPO&Japio
JP15831180A 1980-11-12 1980-11-12 Device for monitoring gap on tip of moving vane of axial-flow turbo-machine Pending JPS5783612A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP15831180A JPS5783612A (en) 1980-11-12 1980-11-12 Device for monitoring gap on tip of moving vane of axial-flow turbo-machine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP15831180A JPS5783612A (en) 1980-11-12 1980-11-12 Device for monitoring gap on tip of moving vane of axial-flow turbo-machine

Publications (1)

Publication Number Publication Date
JPS5783612A true JPS5783612A (en) 1982-05-25

Family

ID=15668850

Family Applications (1)

Application Number Title Priority Date Filing Date
JP15831180A Pending JPS5783612A (en) 1980-11-12 1980-11-12 Device for monitoring gap on tip of moving vane of axial-flow turbo-machine

Country Status (1)

Country Link
JP (1) JPS5783612A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5411364A (en) * 1993-12-22 1995-05-02 Allied-Signal Inc. Gas turbine engine failure detection system

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5411364A (en) * 1993-12-22 1995-05-02 Allied-Signal Inc. Gas turbine engine failure detection system

Similar Documents

Publication Publication Date Title
EP0148497A3 (en) Method and device for guiding and collecting light in photometry or the like
CA1111929A (en) Optical smoke detector with scattered light collecting elements
CA2155892A1 (en) Optical pressure detector
EP0179036A3 (en) Arrangement of a sighting mark and a light-producing source of energy therefor
ES8200496A1 (en) Optical arrangement for a smoke detector using the light scattering principle.
US4430646A (en) Forward scatter smoke detector
DE59804533D1 (en) SMOKE DETECTOR
CA1109541A (en) Optical smoke detector
USRE32105E (en) Forward scatter smoke detector
BR9704931A (en) Optical safety device for cooking appliance
EP0078443A3 (en) Fire detection system
GB1501698A (en) Photoelectric smoke detectors
JPS5783612A (en) Device for monitoring gap on tip of moving vane of axial-flow turbo-machine
JPS57182713A (en) Light signal coupling-extractor
JPS55138620A (en) Photometric device
JPS54161768A (en) Lamp for automobile
JPS56101517A (en) Pulse oscillator
JPS5576321A (en) Wide band light isolator
JPS57165704A (en) Detecting system for light spot position
JPS5444582A (en) Smoke detector
JPS5710172A (en) Original size detecting method of copying machine
JPS5523575A (en) Numeric control unit
JPS556239A (en) Rotation detector for tachometer
JPS56168502A (en) Film thickness gauge utilizing infrared ray
JPS53118145A (en) Detecting method of light beam position