GB201212252D0 - Turbo-machine assembly - Google Patents
Turbo-machine assemblyInfo
- Publication number
- GB201212252D0 GB201212252D0 GBGB1212252.9A GB201212252A GB201212252D0 GB 201212252 D0 GB201212252 D0 GB 201212252D0 GB 201212252 A GB201212252 A GB 201212252A GB 201212252 D0 GB201212252 D0 GB 201212252D0
- Authority
- GB
- United Kingdom
- Prior art keywords
- blade
- turbo
- detector
- machine assembly
- casing
- 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.)
- Ceased
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/003—Arrangements for testing or measuring
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/20—Devices dealing with sensing elements or final actuators or transmitting means between them, e.g. power-assisted
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B21/00—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant
- G01B21/16—Measuring arrangements or details thereof, where the measuring technique is not covered by the other groups of this subclass, unspecified or not relevant for measuring distance of clearance between spaced objects
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
- G01B7/00—Measuring arrangements characterised by the use of electric or magnetic techniques
- G01B7/14—Measuring arrangements characterised by the use of electric or magnetic techniques for measuring distance or clearance between spaced objects or spaced apertures
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2260/00—Function
- F05D2260/80—Diagnostics
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
- F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
- F05D2270/00—Control
- F05D2270/80—Devices generating input signals, e.g. transducers, sensors, cameras or strain gauges
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Abstract
There is disclosed a turbo-machine assembly configured to facilitate improved blade clearance management. In a disclosed arrangement, there is provided a turbo-machine assembly comprising: a casing (2); a fan or turbine including a blade (6) and mounted rotatably within the casing; and a detector (10) for measuring the clearance between the blade and a portion of the inner surface of the casing, wherein: the detector is configured to generate an output by interacting with the blade; and the blade (6) and detector (10) are configured so that a portion of the output from the detector that can be used to generate a measure of the clearance is independent of the axial position of the blade over a predetermined range of axial positions.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1212252.9A GB201212252D0 (en) | 2012-07-10 | 2012-07-10 | Turbo-machine assembly |
PCT/GB2013/051807 WO2014009709A1 (en) | 2012-07-10 | 2013-07-09 | Turbo-machine assembly |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GBGB1212252.9A GB201212252D0 (en) | 2012-07-10 | 2012-07-10 | Turbo-machine assembly |
Publications (1)
Publication Number | Publication Date |
---|---|
GB201212252D0 true GB201212252D0 (en) | 2012-08-22 |
Family
ID=46766421
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GBGB1212252.9A Ceased GB201212252D0 (en) | 2012-07-10 | 2012-07-10 | Turbo-machine assembly |
Country Status (2)
Country | Link |
---|---|
GB (1) | GB201212252D0 (en) |
WO (1) | WO2014009709A1 (en) |
Families Citing this family (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3071919B1 (en) * | 2017-10-03 | 2019-09-20 | Safran Aircraft Engines | SYSTEM AND METHOD FOR SHIFT MEASUREMENT |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE4019000A1 (en) * | 1990-06-13 | 1991-12-19 | Siemens Ag | TURBINE WITH A SHAFT AND FASTENED TURBINE BLADES |
US7215129B1 (en) * | 2006-03-30 | 2007-05-08 | General Electric Company | Multi tip clearance measurement system and method of operation |
DE102006043283A1 (en) * | 2006-09-14 | 2008-03-27 | Mtu Aero Engines Gmbh | Measuring arrangement for detecting a 1 / revolution pulse of an engine rotor and method for this purpose |
US8177474B2 (en) * | 2007-06-26 | 2012-05-15 | General Electric Company | System and method for turbine engine clearance control with rub detection |
-
2012
- 2012-07-10 GB GBGB1212252.9A patent/GB201212252D0/en not_active Ceased
-
2013
- 2013-07-09 WO PCT/GB2013/051807 patent/WO2014009709A1/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2014009709A1 (en) | 2014-01-16 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
AT | Applications terminated before publication under section 16(1) |