FR2034656A1 - - Google Patents

Info

Publication number
FR2034656A1
FR2034656A1 FR6938805A FR6938805A FR2034656A1 FR 2034656 A1 FR2034656 A1 FR 2034656A1 FR 6938805 A FR6938805 A FR 6938805A FR 6938805 A FR6938805 A FR 6938805A FR 2034656 A1 FR2034656 A1 FR 2034656A1
Authority
FR
France
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.)
Withdrawn
Application number
FR6938805A
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Publication of FR2034656A1 publication Critical patent/FR2034656A1/fr
Withdrawn legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/006Safety devices
    • B64C27/007Safety devices adapted for detection of blade cracks
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01LMEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
    • G01L9/00Measuring steady of quasi-steady pressure of fluid or fluent solid material by electric or magnetic pressure-sensitive elements; Transmitting or indicating the displacement of mechanical pressure-sensitive elements, used to measure the steady or quasi-steady pressure of a fluid or fluent solid material, by electric or magnetic means
    • G01L9/0033Transmitting or indicating the displacement of bellows by electric, electromechanical, magnetic, or electromagnetic means

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Electromagnetism (AREA)
  • General Physics & Mathematics (AREA)
  • Measuring Fluid Pressure (AREA)
  • Measurement Of Current Or Voltage (AREA)
FR6938805A 1969-03-05 1969-11-12 Withdrawn FR2034656A1 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US80444869A 1969-03-05 1969-03-05

Publications (1)

Publication Number Publication Date
FR2034656A1 true FR2034656A1 (fr) 1970-12-11

Family

ID=25189012

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6938805A Withdrawn FR2034656A1 (fr) 1969-03-05 1969-11-12

Country Status (4)

Country Link
US (1) US3547555A (fr)
DE (1) DE1954857A1 (fr)
FR (1) FR2034656A1 (fr)
GB (1) GB1258608A (fr)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2342892A1 (fr) * 1976-03-05 1977-09-30 Westland Aircraft Ltd Rotor d'helicoptere

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2304213C2 (de) * 1972-02-14 1983-01-13 United Technologies Corp., 06101 Hartford, Conn. Rotorblatt und Verfahren zur Herstellung desselben
US3765124A (en) * 1972-07-19 1973-10-16 United Aircraft Corp Helicopter rotor blade
US3981611A (en) * 1975-02-12 1976-09-21 United Technologies Corporation Electrical interconnection circuitry from a rotating body to a relatively stationary body
JPS51137299A (en) * 1975-04-15 1976-11-27 Kawasaki Heavy Ind Ltd Crack monitoring device of a rotor
US4082001A (en) * 1977-04-19 1978-04-04 The United States Of America As Represented By The United States National Aeronautics And Space Administration Non-destructive method for applying and removing instrumentation on helicopter rotor blades
DE2936761C2 (de) * 1979-09-12 1984-07-12 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Kontrollsystem zur Überwachung von unter Gasdruck stehenden Rotorblättern
US4439106A (en) * 1982-06-14 1984-03-27 United Technologies Corporation Rotor blade shaft integrity monitoring system
US4717907A (en) * 1986-03-10 1988-01-05 Arinc Research Corporation Remote parameter monitoring system with location-specific indicators
US5205710A (en) * 1991-04-04 1993-04-27 The United States Of America As Represented By The Secretary Of The Air Force Helicopter blade crack detection system
CA2426711C (fr) * 2002-05-02 2009-11-17 General Electric Company Centrale eolienne, mecanisme de commande de centrale eolienne et methode d'exploitation d'une centrale eolienne
DE10356230A1 (de) * 2003-12-02 2005-07-07 Zf Friedrichshafen Ag Rotoreinheit an einem Drehflügler
EP2572982B1 (fr) * 2011-09-20 2014-06-18 AIRBUS HELICOPTERS DEUTSCHLAND GmbH Profil avec système de contrôle de circulation

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2485245A (en) * 1944-07-07 1949-10-18 Curtiss Wright Corp Control system
US3134445A (en) * 1962-05-31 1964-05-26 United Aircraft Corp Blade inspection system
US3417727A (en) * 1967-01-27 1968-12-24 Nemes Laszlo Pressure responsive signal and indicator

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2342892A1 (fr) * 1976-03-05 1977-09-30 Westland Aircraft Ltd Rotor d'helicoptere

Also Published As

Publication number Publication date
GB1258608A (fr) 1971-12-30
US3547555A (en) 1970-12-15
DE1954857A1 (de) 1970-12-17

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Legal Events

Date Code Title Description
ST Notification of lapse