IT1076142B - Apparecchio per la navigazione di un elicottero controllante il carico delle superfici aerodinamiche - Google Patents

Apparecchio per la navigazione di un elicottero controllante il carico delle superfici aerodinamiche

Info

Publication number
IT1076142B
IT1076142B IT22280/77A IT2228077A IT1076142B IT 1076142 B IT1076142 B IT 1076142B IT 22280/77 A IT22280/77 A IT 22280/77A IT 2228077 A IT2228077 A IT 2228077A IT 1076142 B IT1076142 B IT 1076142B
Authority
IT
Italy
Prior art keywords
helicopter
navigating
load
controlling
aerodynamic surfaces
Prior art date
Application number
IT22280/77A
Other languages
English (en)
Italian (it)
Original Assignee
United Technologies 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 Technologies Corp filed Critical United Technologies Corp
Application granted granted Critical
Publication of IT1076142B publication Critical patent/IT1076142B/it

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0066Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements for limitation of acceleration or stress

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Automation & Control Theory (AREA)
  • Navigation (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Emergency Alarm Devices (AREA)
IT22280/77A 1976-06-11 1977-04-08 Apparecchio per la navigazione di un elicottero controllante il carico delle superfici aerodinamiche IT1076142B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US05/695,501 US4115755A (en) 1976-06-11 1976-06-11 Aerodynamic surface load sensing

Publications (1)

Publication Number Publication Date
IT1076142B true IT1076142B (it) 1985-04-24

Family

ID=24793263

Family Applications (1)

Application Number Title Priority Date Filing Date
IT22280/77A IT1076142B (it) 1976-06-11 1977-04-08 Apparecchio per la navigazione di un elicottero controllante il carico delle superfici aerodinamiche

Country Status (8)

Country Link
US (1) US4115755A (enExample)
JP (1) JPS52153600A (enExample)
CA (1) CA1073074A (enExample)
DE (1) DE2715691A1 (enExample)
FR (1) FR2354540B1 (enExample)
GB (1) GB1530245A (enExample)
IL (1) IL51836A (enExample)
IT (1) IT1076142B (enExample)

Families Citing this family (33)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
IL57402A (en) * 1978-09-20 1982-05-31 Israel Aircraft Ind Ltd Excessive descent-rate warning system
US4302745A (en) * 1980-01-10 1981-11-24 The United States Of America As Represented By The Secretary Of The Air Force Aircraft load factor overload warning system
US4574360A (en) * 1983-04-01 1986-03-04 Sundstrand Data Control, Inc. Helicopter weight measuring system
US4619110A (en) * 1983-07-13 1986-10-28 Moore M Samuel Helicopter engine warning or control system
US4763285A (en) * 1985-10-04 1988-08-09 Semco Instruments, Inc. Helicopter low-g monitor, recorder and warning system
CH671555A5 (enExample) * 1986-09-10 1989-09-15 Zermatt Air Ag
US4937758A (en) * 1987-09-04 1990-06-26 Technology Integration And Development Group, Inc. Method and apparatus for reducing vibration over the full operating range of a rotor and a host device
GB9211719D0 (en) * 1992-06-03 1992-07-15 Westland Helicopters Method & apparatus for in-flight shake testing of an aircraft fuselage
DE4420059C2 (de) * 1994-06-08 2000-12-14 Leubner Hans Peter Start- und Landeführungssystem für Drehflügler und andere Senkrechtstarter
WO1997020305A1 (en) 1995-11-30 1997-06-05 Virtual Technologies, Inc. Tactile feedback man-machine interface device
US6052069A (en) * 1997-10-29 2000-04-18 Sikorsky Aircraft Corporation Taxi and slope landing symbology for a helicopter
AU3303299A (en) * 1998-02-20 1999-09-06 Abraham E. Karem Optimum speed rotor
US6641365B2 (en) 1998-02-20 2003-11-04 Abraham E. Karem Optimum speed tilt rotor
DE19822017A1 (de) * 1998-05-15 1999-12-16 Deep Blue Technology Ag Lenzbu Vorrichtung zur Erzeugung eines Warnsignals, insbesondere für Helikopter
US5986582A (en) * 1998-06-24 1999-11-16 Safe Flight Instrument Corporation Helicopter rotor/engine warning system
US6002349A (en) 1998-08-14 1999-12-14 Safe Flight Instrument Corporation Helicopter anti-torque limit warning device
US8532957B2 (en) * 2000-11-15 2013-09-10 Borealis Technical Limited Aircraft weight estimation method
RU2193213C1 (ru) * 2001-05-18 2002-11-20 Государственное предприятие "Всероссийский научно-исследовательский институт физико-технических и радиотехнических измерений" Гидрооптическая аппаратура для обследования подводного объекта
IL143255A (en) 2001-05-20 2015-09-24 Simbionix Ltd Endoscopic ultrasonography simulation
US6748604B2 (en) * 2002-05-30 2004-06-15 Finger Fitting Products, Inc. Glove massager
US7850456B2 (en) 2003-07-15 2010-12-14 Simbionix Ltd. Surgical simulation device, system and method
WO2005083266A1 (ja) 2004-02-27 2005-09-09 Mitsubishi Heavy Industries, Ltd. 風力発電装置およびそのアクティブ制振方法並びに風車タワー
US7262712B2 (en) * 2004-04-12 2007-08-28 Safe Flight Instrument Corporation Helicopter tactile exceedance warning system
US7126496B2 (en) * 2004-09-30 2006-10-24 Safe Flight Instrument Corporation Tactile cueing system and method for aiding a helicopter pilot in making landings
US8543338B2 (en) 2007-01-16 2013-09-24 Simbionix Ltd. System and method for performing computerized simulations for image-guided procedures using a patient specific model
US8500451B2 (en) 2007-01-16 2013-08-06 Simbionix Ltd. Preoperative surgical simulation
US8752784B2 (en) 2011-04-07 2014-06-17 Lord Corporation Aircraft rotary wing motion control and instrumented motion control fluid device
US9734726B2 (en) 2014-02-17 2017-08-15 The Boeing Company Systems and methods for providing landing exceedance warnings and avoidance
US9588734B2 (en) * 2014-06-13 2017-03-07 Ati Technologies Ulc Translation layer for controlling bus access
WO2016039834A2 (en) * 2014-08-29 2016-03-17 Sikorsky Aircraft Corporation Vector limiting of a rotor control volume
US10160537B2 (en) 2017-03-13 2018-12-25 The Boeing Company Apparatus for using aircraft active vibration control system as pilot cueing aid
US10474237B2 (en) * 2017-07-25 2019-11-12 Rolls-Royce Corporation Haptic feedback for rotary wing aircraft
EP4190698B1 (en) * 2021-12-03 2025-01-15 Leonardo S.p.a. Control unit and indicator for an aircraft capable of hovering or for a flight simulation system of said aircraft, and relative method for assisting the performance of a maneuvre

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3076624A (en) * 1960-11-16 1963-02-05 U S Science Corp Oscillatory alarm for aircraft and the like
US3080546A (en) * 1961-02-07 1963-03-05 D Etnde Et De Construction De Indicator device for vertical landings
US3520499A (en) * 1968-05-29 1970-07-14 United Aircraft Corp Flight control system
US3590636A (en) * 1968-10-25 1971-07-06 Industrial Nucleonics Corp Method for determining aircraft lift capability using air density measurement
US3573323A (en) * 1969-02-28 1971-03-30 Upjohn Co 1,2,3,4,5,10-hexahydroazepino(2,3-b)indoles
US3616691A (en) * 1969-03-26 1971-11-02 Bendix Corp Mission capability indicating system
CA929264A (en) * 1969-04-21 1973-06-26 J. Carter Ivor Indicators
US3618002A (en) * 1970-03-02 1971-11-02 Boeing Co Windshear warning system and indicator
US3733039A (en) * 1971-05-20 1973-05-15 United Aircraft Corp Feel augmentation control system for helicopters
US4032083A (en) * 1976-04-12 1977-06-28 United Technologies Corporation Automatic gain control for stability augmentation systems

Also Published As

Publication number Publication date
FR2354540A1 (enExample) 1978-01-06
JPS52153600A (en) 1977-12-20
GB1530245A (en) 1978-10-25
US4115755A (en) 1978-09-19
FR2354540B1 (enExample) 1982-02-05
DE2715691A1 (de) 1977-12-22
CA1073074A (en) 1980-03-04
IL51836A (en) 1982-01-31

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