WO2007006310A3 - Method of making data available to a pilot - Google Patents

Method of making data available to a pilot Download PDF

Info

Publication number
WO2007006310A3
WO2007006310A3 PCT/DK2006/000405 DK2006000405W WO2007006310A3 WO 2007006310 A3 WO2007006310 A3 WO 2007006310A3 DK 2006000405 W DK2006000405 W DK 2006000405W WO 2007006310 A3 WO2007006310 A3 WO 2007006310A3
Authority
WO
WIPO (PCT)
Prior art keywords
pilot
airplane
landing
runway
values
Prior art date
Application number
PCT/DK2006/000405
Other languages
French (fr)
Other versions
WO2007006310A2 (en
Inventor
Steen Bach Sandal
Original Assignee
Sandal Consulting
Steen Bach Sandal
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 Sandal Consulting, Steen Bach Sandal filed Critical Sandal Consulting
Publication of WO2007006310A2 publication Critical patent/WO2007006310A2/en
Publication of WO2007006310A3 publication Critical patent/WO2007006310A3/en

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01D—MEASURING NOT SPECIALLY ADAPTED FOR A SPECIFIC VARIABLE; ARRANGEMENTS FOR MEASURING TWO OR MORE VARIABLES NOT COVERED IN A SINGLE OTHER SUBCLASS; TARIFF METERING APPARATUS; MEASURING OR TESTING NOT OTHERWISE PROVIDED FOR
    • G01D7/00—Indicating measured values
    • G01D7/02—Indicating value of two or more variables simultaneously
    • G01D7/08—Indicating value of two or more variables simultaneously using a common indicating element for two or more variables
    • B60K35/213—
    • B60K35/60—
    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01C—MEASURING DISTANCES, LEVELS OR BEARINGS; SURVEYING; NAVIGATION; GYROSCOPIC INSTRUMENTS; PHOTOGRAMMETRY OR VIDEOGRAMMETRY
    • G01C23/00—Combined instruments indicating more than one navigational value, e.g. for aircraft; Combined measuring devices for measuring two or more variables of movement, e.g. distance, speed or acceleration
    • 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
    • G05D1/0083—Control of position, course or altitude of land, water, air, or space vehicles, e.g. automatic pilot to help an aircraft pilot in the rolling phase

Abstract

Information allowing a pilot to safer and faster determine the status of an airplane, especially at take-off and landing. The information graphically illustrates to the pilot a relation between the length of a runway and a distance required for the airplane to accelerate to a predetermined velocity and decelerate to zero velocity. The information also comprises a graphical relation between a lowest, a highest weight of the airplane and the actual weight of the airplane and an illustration of the surroundings of the runway with an indication of the most relevant obstacle. During landing the display will show the highest weight for landing using wheel brake only. Different autobrake settings will also be depicted on the runway selected for landing. If values for idle and maximum reverse thurst exist these values will also be show adjacent to the non reverser value. Calculated values will depict the actual conditions loaded into the computer by the operator/pilot. As well as approach speeds and missed approach climb restrictions will apply.
PCT/DK2006/000405 2005-07-11 2006-07-10 Method of making data available to a pilot WO2007006310A2 (en)

Applications Claiming Priority (4)

Application Number Priority Date Filing Date Title
DKPA200501021 2005-07-11
DKPA200501021 2005-07-11
US70103305P 2005-07-21 2005-07-21
USPA60/701,033 2005-07-21

Publications (2)

Publication Number Publication Date
WO2007006310A2 WO2007006310A2 (en) 2007-01-18
WO2007006310A3 true WO2007006310A3 (en) 2007-12-21

Family

ID=37526994

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/DK2006/000405 WO2007006310A2 (en) 2005-07-11 2006-07-10 Method of making data available to a pilot

Country Status (1)

Country Link
WO (1) WO2007006310A2 (en)

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* Cited by examiner, † Cited by third party
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US8359542B2 (en) 2010-08-13 2013-01-22 Lockheed Martin Corporation Machines, program products, and computer-implemented methods for interactive aircraft performance substantiation
US8599046B2 (en) * 2011-04-06 2013-12-03 Honeywell International Inc. Systems and methods for informing a pilot of an aircraft about a topographical condition
CN103619881B (en) 2011-04-07 2017-07-28 安姆根有限公司 New EGFR associated proteins
US8849480B2 (en) 2013-03-01 2014-09-30 Honeywell International Inc. Aircraft gross weight and center of gravity validator
US20140336849A1 (en) * 2013-05-08 2014-11-13 Honeywell International Inc. System and method for displaying rate-of-climb on an avionics vertical speed indicator
US10096253B2 (en) 2015-11-30 2018-10-09 Honeywell International Inc. Methods and systems for presenting diversion destinations
US10304344B2 (en) 2016-02-09 2019-05-28 Honeywell International Inc. Methods and systems for safe landing at a diversion airport
US9640079B1 (en) 2016-02-09 2017-05-02 Honeywell International Inc. Methods and systems facilitating holding for an unavailable destination
US10134289B2 (en) 2016-02-18 2018-11-20 Honeywell International Inc. Methods and systems facilitating stabilized descent to a diversion airport
US9738378B1 (en) * 2016-04-08 2017-08-22 The Boeing Company Display-based flight deck autobrake selection
US9884690B2 (en) 2016-05-03 2018-02-06 Honeywell International Inc. Methods and systems for conveying destination viability
US10109203B2 (en) 2016-09-07 2018-10-23 Honeywell International Inc. Methods and systems for presenting en route diversion destinations
US10214300B2 (en) * 2016-11-10 2019-02-26 Honeywell International Inc. System and method for displaying runway overrun information
US10540899B2 (en) 2016-11-21 2020-01-21 Honeywell International Inc. Flight plan segmentation for en route diversion destinations
US11932412B2 (en) 2022-01-05 2024-03-19 Honeywell International Inc. Systems and methods for providing reduced flaps takeoff and landing advice
EP4209419A1 (en) * 2022-01-05 2023-07-12 Honeywell International Inc. Systems and methods for providing reduced flaps takeoff and landing advice

Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2665860A (en) * 1951-07-14 1954-01-12 Rohr Aircraft Corp Aircraft control system for operating auxiliary power source at take-off
US3111577A (en) * 1960-11-17 1963-11-19 Avien Inc Takeoff monitor for jet aircraft
US3128445A (en) * 1958-09-04 1964-04-07 Bendix Corp Aircraft take-off monitoring
US3182498A (en) * 1959-03-10 1965-05-11 Avien Inc Aircraft takeoff monitor
US4251868A (en) * 1978-09-15 1981-02-17 Compania De Transport Aerian Tarom Take-off director system
GB2062876A (en) * 1979-11-06 1981-05-28 Secr Defence Aircraft load indicator
US4638437A (en) * 1984-06-25 1987-01-20 The Boeing Company Aircraft performance margin indicator
US4843554A (en) * 1987-08-06 1989-06-27 The United States Of America As Represented By The United States National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5351045A (en) * 1991-06-19 1994-09-27 University Corporation For Atmospheric Research Low-level wind-shear alert system

Patent Citations (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2665860A (en) * 1951-07-14 1954-01-12 Rohr Aircraft Corp Aircraft control system for operating auxiliary power source at take-off
US3128445A (en) * 1958-09-04 1964-04-07 Bendix Corp Aircraft take-off monitoring
US3182498A (en) * 1959-03-10 1965-05-11 Avien Inc Aircraft takeoff monitor
US3111577A (en) * 1960-11-17 1963-11-19 Avien Inc Takeoff monitor for jet aircraft
US4251868A (en) * 1978-09-15 1981-02-17 Compania De Transport Aerian Tarom Take-off director system
GB2062876A (en) * 1979-11-06 1981-05-28 Secr Defence Aircraft load indicator
US4638437A (en) * 1984-06-25 1987-01-20 The Boeing Company Aircraft performance margin indicator
US4843554A (en) * 1987-08-06 1989-06-27 The United States Of America As Represented By The United States National Aeronautics And Space Administration Airplane takeoff and landing performance monitoring system
US5351045A (en) * 1991-06-19 1994-09-27 University Corporation For Atmospheric Research Low-level wind-shear alert system

Also Published As

Publication number Publication date
WO2007006310A2 (en) 2007-01-18

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