JP4804393B2 - ダクト付きファン大気データシステム - Google Patents

ダクト付きファン大気データシステム Download PDF

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Publication number
JP4804393B2
JP4804393B2 JP2007081643A JP2007081643A JP4804393B2 JP 4804393 B2 JP4804393 B2 JP 4804393B2 JP 2007081643 A JP2007081643 A JP 2007081643A JP 2007081643 A JP2007081643 A JP 2007081643A JP 4804393 B2 JP4804393 B2 JP 4804393B2
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Japan
Prior art keywords
aircraft
pressure
air
atmospheric data
lip
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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
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JP2007081643A
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English (en)
Japanese (ja)
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JP2007263962A (ja
JP2007263962A5 (enExample
Inventor
エムレイ・アール・グーセン
ジョナサン・リー・フレミング
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Honeywell International Inc
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Honeywell International Inc
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Publication date
Application filed by Honeywell International Inc filed Critical Honeywell International Inc
Publication of JP2007263962A publication Critical patent/JP2007263962A/ja
Publication of JP2007263962A5 publication Critical patent/JP2007263962A5/ja
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    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D43/00—Arrangements or adaptations of instruments
    • 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D45/00—Aircraft indicators or protectors not otherwise provided for
    • B64D45/04—Landing aids; Safety measures to prevent collision with earth's surface
    • B64D45/06—Landing aids; Safety measures to prevent collision with earth's surface mechanical
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D47/00—Equipment not otherwise provided for
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
  • Measuring Temperature Or Quantity Of Heat (AREA)
JP2007081643A 2006-03-27 2007-03-27 ダクト付きファン大気データシステム Expired - Fee Related JP4804393B2 (ja)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
US78662506P 2006-03-27 2006-03-27
US60/786,625 2006-03-27
US11/685,532 2007-03-13
US11/685,532 US7841563B2 (en) 2006-03-27 2007-03-13 Ducted fan air data system

Publications (3)

Publication Number Publication Date
JP2007263962A JP2007263962A (ja) 2007-10-11
JP2007263962A5 JP2007263962A5 (enExample) 2010-05-06
JP4804393B2 true JP4804393B2 (ja) 2011-11-02

Family

ID=38180135

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2007081643A Expired - Fee Related JP4804393B2 (ja) 2006-03-27 2007-03-27 ダクト付きファン大気データシステム

Country Status (5)

Country Link
US (1) US7841563B2 (enExample)
EP (1) EP1840578B1 (enExample)
JP (1) JP4804393B2 (enExample)
KR (1) KR20070096981A (enExample)
DE (1) DE602007006853D1 (enExample)

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US8123460B2 (en) * 2008-07-23 2012-02-28 Honeywell International Inc. UAV pod cooling using integrated duct wall heat transfer
US8387911B2 (en) * 2008-07-25 2013-03-05 Honeywell International Inc. Ducted fan core for use with an unmanned aerial vehicle
US8070103B2 (en) * 2008-07-31 2011-12-06 Honeywell International Inc. Fuel line air trap for an unmanned aerial vehicle
US8240597B2 (en) 2008-08-06 2012-08-14 Honeywell International Inc. UAV ducted fan lip shaping
US8070092B2 (en) * 2008-10-31 2011-12-06 Honeywell International Inc. Noise-suppressing strut support system for an unmanned aerial vehicle
US8123169B2 (en) * 2008-11-12 2012-02-28 Honeywell International Inc. Vertical non-bladdered fuel tank for a ducted fan vehicle
US8242623B2 (en) * 2008-11-13 2012-08-14 Honeywell International Inc. Structural ring interconnect printed circuit board assembly for a ducted fan unmanned aerial vehicle
US8225822B2 (en) * 2008-11-14 2012-07-24 Honeywell International Inc. Electric fueling system for a vehicle that requires a metered amount of fuel
US20110001017A1 (en) * 2008-12-08 2011-01-06 Honeywell International Inc. Uav ducted fan swept and lean stator design
US8328130B2 (en) * 2008-12-08 2012-12-11 Honeywell International Inc. Vertical take off and landing unmanned aerial vehicle airframe structure
US8375837B2 (en) * 2009-01-19 2013-02-19 Honeywell International Inc. Catch and snare system for an unmanned aerial vehicle
US8348190B2 (en) * 2009-01-26 2013-01-08 Honeywell International Inc. Ducted fan UAV control alternatives
US8205820B2 (en) * 2009-02-03 2012-06-26 Honeywell International Inc. Transforming unmanned aerial-to-ground vehicle
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US11175202B2 (en) 2018-01-02 2021-11-16 Arthur W Mohr, Jr. Apparatus and method for collecting environmental samples
CN107161352B (zh) * 2017-05-04 2023-08-18 安徽工程大学 一种浮体式四旋翼飞行机器人降落平台
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US12084181B2 (en) * 2020-01-10 2024-09-10 The Board Of Regents Of The University Of Oklahoma Unmanned aerial system for sampling atmospheric data
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Also Published As

Publication number Publication date
EP1840578A2 (en) 2007-10-03
US7841563B2 (en) 2010-11-30
DE602007006853D1 (de) 2010-07-15
US20070221790A1 (en) 2007-09-27
EP1840578B1 (en) 2010-06-02
KR20070096981A (ko) 2007-10-02
EP1840578A3 (en) 2008-10-01
JP2007263962A (ja) 2007-10-11

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