FR2733597B1 - ON-BOARD INSTRUMENT INTENDED TO CONTROL THE PITCH SPEED OF AN AIRPLANE DURING TAKE-OFF - Google Patents

ON-BOARD INSTRUMENT INTENDED TO CONTROL THE PITCH SPEED OF AN AIRPLANE DURING TAKE-OFF

Info

Publication number
FR2733597B1
FR2733597B1 FR9605587A FR9605587A FR2733597B1 FR 2733597 B1 FR2733597 B1 FR 2733597B1 FR 9605587 A FR9605587 A FR 9605587A FR 9605587 A FR9605587 A FR 9605587A FR 2733597 B1 FR2733597 B1 FR 2733597B1
Authority
FR
France
Prior art keywords
control
during take
pitch speed
instrument intended
airplane during
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
FR9605587A
Other languages
French (fr)
Other versions
FR2733597A1 (en
Inventor
James Frederick Moore
Brian William Rawnsley
Alison Frances Starr
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.)
Smiths Group PLC
Original Assignee
Smiths Group PLC
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 Smiths Group PLC filed Critical Smiths Group PLC
Publication of FR2733597A1 publication Critical patent/FR2733597A1/en
Application granted granted Critical
Publication of FR2733597B1 publication Critical patent/FR2733597B1/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00Arrangements or adaptations of instruments
    • 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
    • G05D1/08Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability

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)
  • Traffic Control Systems (AREA)
  • Instrument Panels (AREA)
FR9605587A 1995-04-28 1996-04-25 ON-BOARD INSTRUMENT INTENDED TO CONTROL THE PITCH SPEED OF AN AIRPLANE DURING TAKE-OFF Expired - Fee Related FR2733597B1 (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GBGB9508659.1A GB9508659D0 (en) 1995-04-28 1995-04-28 Aircraft instruments

Publications (2)

Publication Number Publication Date
FR2733597A1 FR2733597A1 (en) 1996-10-31
FR2733597B1 true FR2733597B1 (en) 1999-08-13

Family

ID=10773680

Family Applications (1)

Application Number Title Priority Date Filing Date
FR9605587A Expired - Fee Related FR2733597B1 (en) 1995-04-28 1996-04-25 ON-BOARD INSTRUMENT INTENDED TO CONTROL THE PITCH SPEED OF AN AIRPLANE DURING TAKE-OFF

Country Status (4)

Country Link
CA (1) CA2175030A1 (en)
DE (1) DE19615258A1 (en)
FR (1) FR2733597B1 (en)
GB (2) GB9508659D0 (en)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JP2939234B1 (en) 1998-03-24 1999-08-25 株式会社コミュータヘリコプタ先進技術研究所 Flight path display device
DE19930559B4 (en) * 1999-07-02 2004-08-12 Airbus Deutschland Gmbh Arrangement and method for protecting an aircraft fuselage
GB2510608B (en) * 2013-02-08 2015-02-25 Ge Aviat Systems Ltd Method for predicting a horizontal stabilizer fault
US9828113B2 (en) 2013-11-05 2017-11-28 Safe Flight Instrument Corporation Tailstrike warning system
EP3066651A4 (en) * 2013-11-05 2017-07-19 Safe Flight Instrument Corporation Tailstrike warning system
US20170008639A1 (en) 2015-07-08 2017-01-12 Safe Flight Instrument Corporation Aircraft turbulence detection
CN110069070B (en) * 2019-05-08 2022-01-18 成都高威节能科技有限公司 Method for improving safety of large airplane in takeoff process
CN113286087B (en) * 2021-05-28 2022-09-02 杭州微影软件有限公司 Screen control method and device and thermal imager

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1032466A (en) * 1962-11-20 1966-06-08 Smiths Industries Ltd Improvements in or relating to aircraft instruments
GB1042170A (en) * 1963-11-28 1966-09-14 Smiths Industries Ltd Improvements in or relating to aircraft instruments
SE335248B (en) * 1970-05-11 1971-05-17 Saab Scania Ab
US4043526A (en) * 1976-02-23 1977-08-23 The United States Of America As Represented By The Secretary Of The Navy Autopilot hardover failure protection system
US4046993A (en) * 1976-06-28 1977-09-06 The United States Of America As Represented By The Secretary Of The Navy Target for torpedo launch system
US4071893A (en) * 1976-07-06 1978-01-31 Societe Francaise D'equipements Pour La Navigation Aerienne Flying method and system using total power for an aircraft
GB2134866B (en) * 1980-11-28 1985-06-19 Sundstrand Data Control Angle of attack based pitch generator and head up display
GB2179612B (en) * 1982-07-12 1987-08-26 Secr Defence Aircraft instrumentation
US4769645A (en) * 1983-06-10 1988-09-06 Sundstrand Data Control, Inc. Excessive pitch attitude warning system for rotary wing aircraft
EP0224278B1 (en) * 1985-11-20 1991-05-08 The Boeing Company Apparatus for generating an aircraft situation display
GB9003653D0 (en) * 1990-02-17 1990-04-11 Smiths Industries Plc Aircraft performance monitoring
US5169090A (en) * 1991-08-28 1992-12-08 United Technologies Corporation Attitude synchronization for model following control systems

Also Published As

Publication number Publication date
GB9508659D0 (en) 1995-06-14
DE19615258A1 (en) 1996-10-31
GB2300167B (en) 1999-10-06
GB9607429D0 (en) 1996-06-12
CA2175030A1 (en) 1996-10-29
FR2733597A1 (en) 1996-10-31
GB2300167A (en) 1996-10-30

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Legal Events

Date Code Title Description
CD Change of name or company name
ST Notification of lapse

Effective date: 20061230