GB2300167B - Aircraft instruments - Google Patents

Aircraft instruments

Info

Publication number
GB2300167B
GB2300167B GB9607429A GB9607429A GB2300167B GB 2300167 B GB2300167 B GB 2300167B GB 9607429 A GB9607429 A GB 9607429A GB 9607429 A GB9607429 A GB 9607429A GB 2300167 B GB2300167 B GB 2300167B
Authority
GB
United Kingdom
Prior art keywords
aircraft instruments
aircraft
instruments
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
GB9607429A
Other versions
GB9607429D0 (en
GB2300167A (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 GB9607429D0 publication Critical patent/GB9607429D0/en
Publication of GB2300167A publication Critical patent/GB2300167A/en
Application granted granted Critical
Publication of GB2300167B publication Critical patent/GB2300167B/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • G—PHYSICS
    • G05—CONTROLLING; REGULATING
    • G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D1/00—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot
    • G05D1/08—Control of attitude, i.e. control of roll, pitch, or yaw
    • G05D1/0808—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft
    • G05D1/0816—Control of attitude, i.e. control of roll, pitch, or yaw specially adapted for aircraft to ensure stability
GB9607429A 1995-04-28 1996-04-10 Aircraft instruments Expired - Fee Related GB2300167B (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 (3)

Publication Number Publication Date
GB9607429D0 GB9607429D0 (en) 1996-06-12
GB2300167A GB2300167A (en) 1996-10-30
GB2300167B true GB2300167B (en) 1999-10-06

Family

ID=10773680

Family Applications (2)

Application Number Title Priority Date Filing Date
GBGB9508659.1A Pending GB9508659D0 (en) 1995-04-28 1995-04-28 Aircraft instruments
GB9607429A Expired - Fee Related GB2300167B (en) 1995-04-28 1996-04-10 Aircraft instruments

Family Applications Before (1)

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

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
WO2015069228A1 (en) * 2013-11-05 2015-05-14 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

Citations (10)

* 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
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
GB2134866A (en) * 1980-11-28 1984-08-22 Sundstrand Data Control Angle of attack based pitch generator and head up display
GB2141394A (en) * 1983-06-10 1984-12-19 Sundstrand Data Control Excessive pitch attitude warning system for rotary wing aircraft
GB2179612A (en) * 1982-07-12 1987-03-11 Secr Defence Aircraft instrumentation
EP0224278A2 (en) * 1985-11-20 1987-06-03 The Boeing Company Apparatus for generating an aircraft situation display
US5169090A (en) * 1991-08-28 1992-12-08 United Technologies Corporation Attitude synchronization for model following control systems
US5170163A (en) * 1990-02-17 1992-12-08 Smiths Industries Public Limited Company Aircraft performance monitoring

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
SE335248B (en) * 1970-05-11 1971-05-17 Saab Scania Ab
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

Patent Citations (11)

* 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
US3309923A (en) * 1962-11-20 1967-03-21 Smith & Sons Ltd S Aircraft instruments
GB1042170A (en) * 1963-11-28 1966-09-14 Smiths Industries Ltd Improvements in or relating to aircraft instruments
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
GB2134866A (en) * 1980-11-28 1984-08-22 Sundstrand Data Control Angle of attack based pitch generator and head up display
GB2179612A (en) * 1982-07-12 1987-03-11 Secr Defence Aircraft instrumentation
GB2141394A (en) * 1983-06-10 1984-12-19 Sundstrand Data Control Excessive pitch attitude warning system for rotary wing aircraft
EP0224278A2 (en) * 1985-11-20 1987-06-03 The Boeing Company Apparatus for generating an aircraft situation display
US5170163A (en) * 1990-02-17 1992-12-08 Smiths Industries Public Limited Company 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
GB9607429D0 (en) 1996-06-12
GB9508659D0 (en) 1995-06-14
FR2733597B1 (en) 1999-08-13
CA2175030A1 (en) 1996-10-29
GB2300167A (en) 1996-10-30
DE19615258A1 (en) 1996-10-31
FR2733597A1 (en) 1996-10-31

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee

Effective date: 20060410