DE3382397D1 - Verfahren zum nachweis der durchbiegung von teilen einer rotierenden masse. - Google Patents

Verfahren zum nachweis der durchbiegung von teilen einer rotierenden masse.

Info

Publication number
DE3382397D1
DE3382397D1 DE8383301422T DE3382397T DE3382397D1 DE 3382397 D1 DE3382397 D1 DE 3382397D1 DE 8383301422 T DE8383301422 T DE 8383301422T DE 3382397 T DE3382397 T DE 3382397T DE 3382397 D1 DE3382397 D1 DE 3382397D1
Authority
DE
Germany
Prior art keywords
bowing
detecting
parts
rotating mass
mass
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.)
Expired - Fee Related
Application number
DE8383301422T
Other languages
English (en)
Inventor
Christpher Ian Moir
Walter Allan Clearwater
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.)
HELITUNE LTD., MALVERN, WORCESTESHIRE, GB
Original Assignee
Micro Control Technology 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
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=26282255&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=DE3382397(D1) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Micro Control Technology Ltd filed Critical Micro Control Technology Ltd
Application granted granted Critical
Publication of DE3382397D1 publication Critical patent/DE3382397D1/de
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B11/00—Measuring arrangements characterised by the use of optical techniques
    • G01B11/16—Measuring arrangements characterised by the use of optical techniques for measuring the deformation in a solid, e.g. optical strain gauge
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01B—MEASURING LENGTH, THICKNESS OR SIMILAR LINEAR DIMENSIONS; MEASURING ANGLES; MEASURING AREAS; MEASURING IRREGULARITIES OF SURFACES OR CONTOURS
    • G01B17/00—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations
    • G01B17/04—Measuring arrangements characterised by the use of infrasonic, sonic or ultrasonic vibrations for measuring the deformation in a solid, e.g. by vibrating string

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Testing Of Balance (AREA)
  • Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
  • Investigating Or Analysing Biological Materials (AREA)
  • Radar Systems Or Details Thereof (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Measurement Of Velocity Or Position Using Acoustic Or Ultrasonic Waves (AREA)
DE8383301422T 1982-03-16 1983-03-15 Verfahren zum nachweis der durchbiegung von teilen einer rotierenden masse. Expired - Fee Related DE3382397D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB8207575 1982-03-16
GB8207574 1982-03-16

Publications (1)

Publication Number Publication Date
DE3382397D1 true DE3382397D1 (de) 1991-10-10

Family

ID=26282255

Family Applications (1)

Application Number Title Priority Date Filing Date
DE8383301422T Expired - Fee Related DE3382397D1 (de) 1982-03-16 1983-03-15 Verfahren zum nachweis der durchbiegung von teilen einer rotierenden masse.

Country Status (8)

Country Link
US (1) US4887087A (de)
EP (1) EP0089228B1 (de)
KR (1) KR840004018A (de)
CA (1) CA1212771A (de)
DE (1) DE3382397D1 (de)
DK (1) DK99383A (de)
GB (2) GB2116804B (de)
NO (1) NO172155C (de)

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
AU3055289A (en) * 1988-01-13 1989-08-11 Stewart Hughes Limited Apparatus and method for tracking a rotating blade to determine parameters associated with the rotation of that blade
US5054918A (en) * 1990-02-02 1991-10-08 Fmc Corporation Light scanning system for measurement of orientation and physical features of a workpiece
WO1992007282A1 (en) * 1990-10-10 1992-04-30 Bell Helicopter Textron Inc. Multibeam radar system mounted on an aircraft with a rotor
KR0154445B1 (ko) * 1994-02-19 1999-01-15 윤종용 에어콘의 소음감소 장치
FR2731795B1 (fr) * 1995-03-16 1997-06-06 Eurocopter France Banc d'essai pour rotors de giravions
US5760731A (en) * 1995-12-19 1998-06-02 Fisher Controls International, Inc. Sensors and methods for sensing displacement using radar
EP1132730B1 (de) * 2000-03-07 2003-04-09 Sulzer Markets and Technology AG Verfahren und Anordnung zur Beurteilung des Reibverhaltens zwischen zwei Gegenlaufpartnern
DE50100149D1 (de) 2000-03-07 2003-05-15 Sulzer Markets & Technology Ag Verfahren und Anordnung zur Beurteilung des Reibverhaltens zwischen zwei Gegenlaufpartnern
US7403294B2 (en) * 2003-03-07 2008-07-22 Boxboro Systems, Llc Optical measurement device and method
US7546975B2 (en) * 2004-09-14 2009-06-16 The Boeing Company Tandem rotor wing rotational position control system
US8041520B2 (en) * 2007-09-26 2011-10-18 Gilbert Ronald Mesec Method to detect mechanical faults and dynamic instability in rotor systems of helicopters, tilt rotor aircraft, and whirl towers
DE102008058029B3 (de) * 2008-11-18 2010-01-07 Deutsches Zentrum für Luft- und Raumfahrt e.V. Hubschrauber
US9482573B2 (en) * 2010-05-24 2016-11-01 Honeywell International Inc. Condition based monitoring system based on radar sensor
KR101334733B1 (ko) 2012-06-07 2013-11-29 국방과학연구소 방향 탐지 시스템의 테일 로터 영향성 보정 장치, 방향 탐지 시스템의 테일 로터 영향성 처리 장치 및 방법
US10065732B2 (en) * 2012-08-21 2018-09-04 Technology For Energy Corporation Systems and methods of tracking rotor blades
US9470793B2 (en) * 2013-02-13 2016-10-18 Sikorsky Aircraft Corporation Optical tracking of rotor blade motion
US9638601B2 (en) 2013-10-09 2017-05-02 Simmonds Precision Products, Inc. Systems and methods for determining rotary blade track and balance adjustments
US9696232B2 (en) * 2013-10-09 2017-07-04 Simmonds Precision Products, Inc. Systems and methods for track and balance visualization
US9632000B1 (en) 2014-01-27 2017-04-25 RMCI, Inc. Track measurement by phase-based signal extraction
US9815565B1 (en) * 2015-03-02 2017-11-14 RPX Technologies, Inc. Tracker and vibration analysis system
US20170008621A1 (en) * 2015-07-08 2017-01-12 Honeywell International Inc. Accurate object detection in free space using controlled light source techniques
US9911344B2 (en) 2015-07-24 2018-03-06 Honeywell International Inc. Helicopter landing system using a camera for obstacle detection
CN108593243B (zh) * 2018-04-23 2024-02-13 中国空气动力研究与发展中心低速空气动力研究所 一种直升机组合模型试验装置
CN108802732A (zh) * 2018-06-14 2018-11-13 中航金林科技(北京)有限公司 直升机翼尖显示装置
US11643194B2 (en) * 2019-12-17 2023-05-09 The Boeing Company System and method for dynamically measuring blade position during flight of a rotorcraft
CN112781516B (zh) * 2020-12-29 2022-11-22 中国航空工业集团公司西安飞机设计研究所 一种高速旋翼动态挠度测量装置

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2552739A (en) * 1951-05-15 Method of tracking kotor blades
US2960908A (en) * 1956-01-26 1960-11-22 Chicago Aerial Ind Inc Parallax interval sensing device
US2913700A (en) * 1956-05-31 1959-11-17 Stanley S Brody Supersonic deviation-measuring apparatus
DE1406574B2 (de) * 1963-08-09 1970-10-01 Licentia Patent-Verwaltungs-GmbH, 6OOO Frankfurt Anordnung für eine berührungslose Spurlaufmessung
GB1116748A (en) * 1964-10-05 1968-06-12 Licentia Gmbh An arrangement on a helicopter for observing or measuring the position of its rotor blades
US3386031A (en) * 1965-06-01 1968-05-28 Sweeney Mfg Co B K Helicopter rotor blade trackers
GB1277748A (en) * 1969-09-02 1972-06-14 Rolls Royce Improvements in or relating to proximity sensing apparatus
SE383046B (sv) * 1973-11-12 1976-02-23 G Hellgren Anordning for indikering av ett foremals legesforendringar
US4053123A (en) * 1976-04-16 1977-10-11 Chadwick-Helmuth Company, Inc. Method and apparatus to determine need for rotor blade pitch adjustment and/or blade substitution
DE2928907A1 (de) * 1979-07-18 1981-06-19 Siemens AG, 1000 Berlin und 8000 München Verfahren zur klassifizierung bewegter ziele
GB2055269B (en) * 1979-08-04 1983-10-05 Emi Ltd Checking the location of moving parts in a machine
DE3044242A1 (de) * 1979-12-11 1981-09-03 Smiths Industries Ltd., London Anzeigesystem zur anzeige des abstandes der blaetter einer turbine zu einem bezugspunkt
US4465367A (en) * 1981-11-03 1984-08-14 L'etat Francais Process and device for measuring and adjusting out-of-track distances of helicopter rotor blades

Also Published As

Publication number Publication date
GB2116803A (en) 1983-09-28
US4887087A (en) 1989-12-12
EP0089228A2 (de) 1983-09-21
GB2116804B (en) 1986-03-26
CA1212771A (en) 1986-10-14
NO830905L (no) 1983-09-19
GB2116804A (en) 1983-09-28
NO172155C (no) 1993-06-09
NO172155B (no) 1993-03-01
EP0089228A3 (en) 1987-04-22
KR840004018A (ko) 1984-10-06
US4887087B1 (de) 1992-03-24
DK99383D0 (da) 1983-02-28
DK99383A (da) 1983-09-17
EP0089228B1 (de) 1991-09-04

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Legal Events

Date Code Title Description
8327 Change in the person/name/address of the patent owner

Owner name: HELITUNE LTD., MALVERN, WORCESTESHIRE, GB

8363 Opposition against the patent
8339 Ceased/non-payment of the annual fee