NO167907C - Varselinnretning i et luftfartoey - Google Patents

Varselinnretning i et luftfartoey

Info

Publication number
NO167907C
NO167907C NO873763A NO873763A NO167907C NO 167907 C NO167907 C NO 167907C NO 873763 A NO873763 A NO 873763A NO 873763 A NO873763 A NO 873763A NO 167907 C NO167907 C NO 167907C
Authority
NO
Norway
Prior art keywords
aircraft
alignment device
alignment
Prior art date
Application number
NO873763A
Other languages
English (en)
Norwegian (no)
Other versions
NO167907B (no
NO873763D0 (no
NO873763L (no
Inventor
Claude Vuichard
Original Assignee
Zermatt Air Ag
Claude Vuichard
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 Zermatt Air Ag, Claude Vuichard filed Critical Zermatt Air Ag
Publication of NO873763D0 publication Critical patent/NO873763D0/no
Publication of NO873763L publication Critical patent/NO873763L/no
Publication of NO167907B publication Critical patent/NO167907B/no
Publication of NO167907C publication Critical patent/NO167907C/no

Links

Classifications

    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
    • G05D1/0055—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots with safety arrangements
    • G05D1/0066—Control 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)
  • Automation & Control Theory (AREA)
  • Radar, Positioning & Navigation (AREA)
  • Remote Sensing (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Emergency Alarm Devices (AREA)
  • Arrangements For Transmission Of Measured Signals (AREA)
  • Mobile Radio Communication Systems (AREA)
  • Radio Relay Systems (AREA)
  • Position Fixing By Use Of Radio Waves (AREA)
  • Combined Controls Of Internal Combustion Engines (AREA)
NO873763A 1986-09-10 1987-09-09 Varselinnretning i et luftfartoey NO167907C (no)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CH3632/86A CH671555A5 (fr) 1986-09-10 1986-09-10

Publications (4)

Publication Number Publication Date
NO873763D0 NO873763D0 (no) 1987-09-09
NO873763L NO873763L (no) 1988-03-11
NO167907B NO167907B (no) 1991-09-16
NO167907C true NO167907C (no) 1991-12-27

Family

ID=4260151

Family Applications (1)

Application Number Title Priority Date Filing Date
NO873763A NO167907C (no) 1986-09-10 1987-09-09 Varselinnretning i et luftfartoey

Country Status (5)

Country Link
US (1) US4870412A (fr)
EP (1) EP0259675A3 (fr)
AU (1) AU604256B2 (fr)
CH (1) CH671555A5 (fr)
NO (1) NO167907C (fr)

Families Citing this family (14)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE4036241A1 (de) * 1990-11-14 1992-05-21 Joerg Golombek Verfahren und vorrichtung zur ermittlung und verwertung der physikalischen daten eines im betrieb befindlichen fahrzeugmodells
US5229956A (en) * 1991-03-06 1993-07-20 United Technologies Corporation Helicopter weight measurement
US5359326A (en) * 1993-03-16 1994-10-25 The United States Of America As Represented By The Administrator Of National Aeronautics And Space Administration Aircraft maneuver envelope warning system
US5607122A (en) * 1994-12-22 1997-03-04 Bell Helicopter Textron Inc. Tail rotor authority control for a helicopter
DE19822017A1 (de) * 1998-05-15 1999-12-16 Deep Blue Technology Ag Lenzbu Vorrichtung zur Erzeugung eines Warnsignals, insbesondere für Helikopter
US6449573B1 (en) * 1999-04-09 2002-09-10 Ian Amos Apparatus to calculate dynamic values for pressure density in an aircraft
US20060049303A1 (en) * 2004-08-23 2006-03-09 Wilkerson Darrell W Mechanical density altitude compensation device for helicopter tail rotors
US7765061B1 (en) * 2006-05-18 2010-07-27 Rockwell Collins, Inc. Flight display system with enhanced temporal depiction of navigation information
CA2677284C (fr) * 2007-02-08 2018-02-27 Bell Helicopter Textron Inc. Indicateur de variation cyclique de pas, de levee de pale et de charges de rotor d'aeronef a voilure tournante
DE102007061088B4 (de) * 2007-12-19 2017-08-17 Airbus Operations Gmbh Temperaturüberwachung eines Flugzeugs
CN102407945B (zh) * 2011-10-09 2014-08-06 中国航空无线电电子研究所 基于音频变频原理的告警装置
US9758243B1 (en) * 2013-03-06 2017-09-12 RMCI, Inc. Calculation of helicopter rotor balance adjustments and coefficients using mobile devices or custom coefficients
US10597167B1 (en) * 2018-07-09 2020-03-24 Rockwell Collins, Inc. Time to altitude display system and method
EP4190698A1 (fr) 2021-12-03 2023-06-07 Leonardo S.p.a. Unité de commande et indicateur pour un aéronef capable de vol stationnaire ou pour un système de simulation de vol dudit aéronef et procédé associé pour faciliter la performance d'une manoeuvre

Family Cites Families (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3104721A (en) * 1963-09-24 Helicopter engine failure warning system
US2806402A (en) * 1954-10-04 1957-09-17 Gen Motors Corp Propeller blade angle indicating device
US3537323A (en) * 1968-09-11 1970-11-03 Aerostructures Inc Hover-altitude performance indicator for a helicopter
US3616691A (en) * 1969-03-26 1971-11-02 Bendix Corp Mission capability indicating system
US3744928A (en) * 1971-10-07 1973-07-10 United Aircraft Corp Rotor overload protection
US3754440A (en) * 1972-08-16 1973-08-28 Us Navy Helicopter lift margin determining system
US3795151A (en) * 1972-08-18 1974-03-05 Bendix Corp Electromagnetic coupling for an altimeter
US3924262A (en) * 1974-12-02 1975-12-02 Us Navy Aural warning apparatus
US3925751A (en) * 1975-04-02 1975-12-09 Sundstrand Data Control Glide slope warning system with a variable warning rate
US4115755A (en) * 1976-06-11 1978-09-19 United Technologies Corporation Aerodynamic surface load sensing
US4263804A (en) * 1979-09-10 1981-04-28 Seemann Robert A Apparatus for directly measuring density altitude in an aircraft
US4488236A (en) * 1982-04-16 1984-12-11 United Technologies Corporation Helicopter cruise fuel conserving engine control
US4564908A (en) * 1983-02-28 1986-01-14 United Technologies Corporation Automatic limiting of helicopter engine torque
US4951047A (en) * 1983-05-13 1990-08-21 Sunstrand Data Control, Inc. Negative climb after take-off warning system
CA1234417A (fr) * 1983-05-13 1988-03-22 Noel S. Paterson Systeme avertissant le pilote de profils de vol dangereux au cours d'evolutions a basse altitude
US4619110A (en) * 1983-07-13 1986-10-28 Moore M Samuel Helicopter engine warning or control system
GB2169572B (en) * 1985-01-03 1988-02-10 Boeing Co A helicopter weight and torque advisory system
US4763285A (en) * 1985-10-04 1988-08-09 Semco Instruments, Inc. Helicopter low-g monitor, recorder and warning system

Also Published As

Publication number Publication date
CH671555A5 (fr) 1989-09-15
EP0259675A2 (fr) 1988-03-16
NO167907B (no) 1991-09-16
AU604256B2 (en) 1990-12-13
AU7733287A (en) 1988-03-17
NO873763D0 (no) 1987-09-09
EP0259675A3 (fr) 1990-02-28
US4870412A (en) 1989-09-26
NO873763L (no) 1988-03-11

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