GB2584464B - Aircraft - Google Patents

Aircraft Download PDF

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Publication number
GB2584464B
GB2584464B GB1907984.7A GB201907984A GB2584464B GB 2584464 B GB2584464 B GB 2584464B GB 201907984 A GB201907984 A GB 201907984A GB 2584464 B GB2584464 B GB 2584464B
Authority
GB
United Kingdom
Prior art keywords
aircraft
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.)
Active
Application number
GB1907984.7A
Other versions
GB201907984D0 (en
GB2584464A (en
Inventor
Frank Ellison William
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.)
BAE Systems PLC
Original Assignee
BAE Systems 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 BAE Systems PLC filed Critical BAE Systems PLC
Priority to GB1907984.7A priority Critical patent/GB2584464B/en
Publication of GB201907984D0 publication Critical patent/GB201907984D0/en
Priority to PCT/GB2020/051349 priority patent/WO2020245588A1/en
Priority to EP20731179.6A priority patent/EP3980334B1/en
Priority to US17/615,135 priority patent/US11774466B2/en
Publication of GB2584464A publication Critical patent/GB2584464A/en
Application granted granted Critical
Publication of GB2584464B publication Critical patent/GB2584464B/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P13/00—Indicating or recording presence, absence, or direction, of movement
    • G01P13/02—Indicating direction only, e.g. by weather vane
    • G01P13/025—Indicating direction only, e.g. by weather vane indicating air data, i.e. flight variables of an aircraft, e.g. angle of attack, side slip, shear, yaw
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/14—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid
    • G01P5/16—Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring differences of pressure in the fluid using Pitot tubes, e.g. Machmeter
    • 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
    • B64D43/02—Arrangements or adaptations of instruments for indicating aircraft speed or stalling conditions
GB1907984.7A 2019-06-05 2019-06-05 Aircraft Active GB2584464B (en)

Priority Applications (4)

Application Number Priority Date Filing Date Title
GB1907984.7A GB2584464B (en) 2019-06-05 2019-06-05 Aircraft
PCT/GB2020/051349 WO2020245588A1 (en) 2019-06-05 2020-06-04 Aircraft with air data sensor
EP20731179.6A EP3980334B1 (en) 2019-06-05 2020-06-04 Aircraft with air data sensor
US17/615,135 US11774466B2 (en) 2019-06-05 2020-06-04 Aircraft with skin layer air data sensor

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1907984.7A GB2584464B (en) 2019-06-05 2019-06-05 Aircraft

Publications (3)

Publication Number Publication Date
GB201907984D0 GB201907984D0 (en) 2019-07-17
GB2584464A GB2584464A (en) 2020-12-09
GB2584464B true GB2584464B (en) 2023-03-22

Family

ID=67385686

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1907984.7A Active GB2584464B (en) 2019-06-05 2019-06-05 Aircraft

Country Status (1)

Country Link
GB (1) GB2584464B (en)

Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262316A (en) * 1962-08-28 1966-07-26 Douglas Aircraft Co Inc Static position error compensation system and apparatus
GB2173861A (en) * 1985-04-22 1986-10-22 Gen Electric Directing air flow to an airstream probe
US6253166B1 (en) * 1998-10-05 2001-06-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Stable algorithm for estimating airdata from flush surface pressure measurements
US20030115948A1 (en) * 2001-12-21 2003-06-26 Rouse Gordon F. Flush surface air data sensor
GB2424285A (en) * 2005-03-16 2006-09-20 Rosemount Aerospace Inc Method and Apparatus for Extending Useful Range of Air Data Parameter Calculation In Flush Air Data Systems
GB2424957A (en) * 2005-04-06 2006-10-11 Rosemount Aerospace Inc Calculating system level air data for an aircraft using pressure ratios
FR2912214A1 (en) * 2007-02-05 2008-08-08 Airbus France Sa Parietal head for measuring static pressure on aircraft, has measurement orifice arranged in concavity at right of symmetrical center of ellipse, which has large axis that is parallel to main axis of fuselage of aircraft
US20160266164A1 (en) * 2013-10-23 2016-09-15 Bae Systems Plc Air data sensor for an aircraft

Patent Citations (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3262316A (en) * 1962-08-28 1966-07-26 Douglas Aircraft Co Inc Static position error compensation system and apparatus
GB2173861A (en) * 1985-04-22 1986-10-22 Gen Electric Directing air flow to an airstream probe
US6253166B1 (en) * 1998-10-05 2001-06-26 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Stable algorithm for estimating airdata from flush surface pressure measurements
US20030115948A1 (en) * 2001-12-21 2003-06-26 Rouse Gordon F. Flush surface air data sensor
GB2424285A (en) * 2005-03-16 2006-09-20 Rosemount Aerospace Inc Method and Apparatus for Extending Useful Range of Air Data Parameter Calculation In Flush Air Data Systems
GB2424957A (en) * 2005-04-06 2006-10-11 Rosemount Aerospace Inc Calculating system level air data for an aircraft using pressure ratios
FR2912214A1 (en) * 2007-02-05 2008-08-08 Airbus France Sa Parietal head for measuring static pressure on aircraft, has measurement orifice arranged in concavity at right of symmetrical center of ellipse, which has large axis that is parallel to main axis of fuselage of aircraft
US20160266164A1 (en) * 2013-10-23 2016-09-15 Bae Systems Plc Air data sensor for an aircraft

Also Published As

Publication number Publication date
GB201907984D0 (en) 2019-07-17
GB2584464A (en) 2020-12-09

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