CA2359623A1 - System and apparatus for determining the center of gravity of an aircraft - Google Patents

System and apparatus for determining the center of gravity of an aircraft Download PDF

Info

Publication number
CA2359623A1
CA2359623A1 CA002359623A CA2359623A CA2359623A1 CA 2359623 A1 CA2359623 A1 CA 2359623A1 CA 002359623 A CA002359623 A CA 002359623A CA 2359623 A CA2359623 A CA 2359623A CA 2359623 A1 CA2359623 A1 CA 2359623A1
Authority
CA
Canada
Prior art keywords
aircraft
frame
wheel
determining
load
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.)
Granted
Application number
CA002359623A
Other languages
French (fr)
Other versions
CA2359623C (en
Inventor
Don S. Godwin
Kenneth D. Driver
Joseph C. Gray
Richard J. Gritter
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.)
ATLANTIC AERO Inc
Original Assignee
Aero Modifications & Consulting, Llc
Don S. Godwin
Kenneth D. Driver
Joseph C. Gray
Richard J. Gritter
Atlantic Aero Holdings, Inc.
Atlantic Aero, Inc.
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 Aero Modifications & Consulting, Llc, Don S. Godwin, Kenneth D. Driver, Joseph C. Gray, Richard J. Gritter, Atlantic Aero Holdings, Inc., Atlantic Aero, Inc. filed Critical Aero Modifications & Consulting, Llc
Publication of CA2359623A1 publication Critical patent/CA2359623A1/en
Application granted granted Critical
Publication of CA2359623C publication Critical patent/CA2359623C/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Classifications

    • G—PHYSICS
    • G01—MEASURING; TESTING
    • G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M1/00—Testing static or dynamic balance of machines or structures
    • G01M1/12—Static balancing; Determining position of centre of gravity
    • G01M1/122—Determining position of centre of gravity
    • G01M1/125—Determining position of centre of gravity of aircraft

Abstract

A method and apparatus for determining the center of gravity of an aircraft having a plurality of wheels includes the steps of determining the load on one of the plurality of aircraft wheels, determining the aircraft inclination with respect to level, relating the wheel load to the aircraft center of gravity based on the aircraft inclination. The load determination may be conducted on the aircraft nose wheel (60) using a lever apparatus (10) including a frame (14) having a forward end and an aft end the aft end including an attachment device located at the aft end for providing detachable engagement with the wheel axle (62). The lever apparatus (10) also includes a pivot arm (12) having a first end and a second end, the first end pivotally attached to the frame (14) at a pivot point (12b) located between the forward end and the aft end of the frame (14). A load cell is positioned on the frame (14) so as to be engaged by the pivot arm (12) as the pivot arm pivots about the pivot point (12b) for generating a signal indicative of the force generated on the frame as the wheel is raised. The lever apparatus operates about a fulcrum point located forward of the frame aft end about which the lever apparatus raises the aircraft wheel. A processor may be provided for receiving the load cell signal and determining wheel load.
CA002359623A 1999-02-01 2000-01-20 System and apparatus for determining the center of gravity of an aircraft Expired - Fee Related CA2359623C (en)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US09/243,392 1999-02-01
US09/243,392 US6353793B1 (en) 1999-02-01 1999-02-01 System and apparatus for determining the center of gravity of an aircraft
PCT/US2000/001414 WO2000049377A2 (en) 1999-02-01 2000-01-20 System and apparatus for determining the center of gravity of an aircraft

Publications (2)

Publication Number Publication Date
CA2359623A1 true CA2359623A1 (en) 2000-08-24
CA2359623C CA2359623C (en) 2006-02-14

Family

ID=22918601

Family Applications (1)

Application Number Title Priority Date Filing Date
CA002359623A Expired - Fee Related CA2359623C (en) 1999-02-01 2000-01-20 System and apparatus for determining the center of gravity of an aircraft

Country Status (4)

Country Link
US (1) US6353793B1 (en)
AU (1) AU5265400A (en)
CA (1) CA2359623C (en)
WO (1) WO2000049377A2 (en)

Families Citing this family (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US6564142B2 (en) * 1999-02-01 2003-05-13 Aero Modifications & Consulting, L.L.C. System and apparatus for determining the center of gravity of an aircraft
US6880258B2 (en) * 2003-08-26 2005-04-19 Horizon Hobby Digital inclinometer and related methods
FR2883967B1 (en) * 2005-04-04 2007-06-29 Messier Bugatti Sa DEVICE AND METHOD FOR DETERMINING THE WEIGHT AND / OR CHARACTERISTIC SIZE OF THE CENTERING OF AN AIRCRAFT
US7890249B2 (en) * 2007-07-06 2011-02-15 Nordic Industries, Inc. System and method for determining a center of gravity of an aircraft
US8060296B2 (en) * 2008-11-12 2011-11-15 Honeywell International Inc. Low cost aircraft center of gravity monitoring systems and methods
DE102011116975B3 (en) 2011-10-26 2013-03-21 Airbus Operations Gmbh Method for determining shear force of engine mounted in vehicle e.g. aircraft, involves determining shear force of engine as effective force component in the predetermined thrust direction of vehicle
CN102628723B (en) * 2012-04-19 2015-09-02 江苏大学 A kind of birds, beasts and eggs center of mass determination method
US9927319B2 (en) * 2013-10-01 2018-03-27 C. Kirk Nance Method for determining aircraft center of gravity independent of measuring the aircraft weight
CN105302151B (en) * 2014-08-01 2018-07-13 深圳中集天达空港设备有限公司 A kind of system and method for aircraft docking guiding and plane type recognition
CN105373135B (en) * 2014-08-01 2019-01-01 深圳中集天达空港设备有限公司 A kind of method and system of aircraft docking guidance and plane type recognition based on machine vision
US9550561B1 (en) 2014-08-11 2017-01-24 Amazon Technologies, Inc. Determining center of gravity of an automated aerial vehicle and a payload
US10089634B2 (en) 2015-10-27 2018-10-02 C Kirk Nance Method to recover non-recognized errors in aircraft weight determinations to increase weight and center of gravity limitations for regulated aircraft
GB2576787B (en) * 2018-09-03 2022-05-11 Ge Aviat Systems Ltd Measuring weight and balance and optimizing center of gravity
CN109632062B (en) * 2018-12-29 2020-09-22 成都纵横大鹏无人机科技有限公司 Weight and gravity center measuring device and measuring method
CN109459121A (en) * 2018-12-29 2019-03-12 中航电测仪器股份有限公司 A kind of bird weight center of gravity measurement method
US11001392B1 (en) 2019-11-10 2021-05-11 John Timothy Kern System of hardware and software for determining the weight and center of gravity location of an airplane or other vehicles, like a forklift, truck, and maritime vessel
CN110963074B (en) * 2019-12-25 2022-12-09 中航贵州飞机有限责任公司 Unmanned aerial vehicle undercarriage signal simulation system
CN116754133B (en) * 2023-08-16 2023-10-17 辽宁通用航空研究院 Distance measuring tool for measuring aircraft gravity center

Family Cites Families (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2336142A (en) 1937-10-08 1943-12-07 Oliver H Watson Apparatus for locating the planes of gravity of objects
US2540807A (en) 1944-05-25 1951-02-06 Gen Electric Center of gravity indicator
US2425685A (en) 1944-11-14 1947-08-12 Joseph W Pinder Means for determining balance
US2929679A (en) 1957-03-28 1960-03-22 L E E Inc Aircraft load and blance computer
US3225590A (en) 1961-08-31 1965-12-28 Earl C Ward Method and apparatus for locating the center of gravity
US3584503A (en) 1969-12-04 1971-06-15 Blh Electronics Aircraft weight and center of gravity determination system which includes alarm,self-checking,and fault override circuitry
US3701279A (en) 1971-02-08 1972-10-31 Electro Dev Corp Aircraft weight and center of gravity indicator system
US4110605A (en) * 1977-02-25 1978-08-29 Sperry Rand Corporation Weight and balance computer apparatus for aircraft
US4463428A (en) 1981-10-26 1984-07-31 The United States Of America As Represented By The Secretary Of The Navy Aircraft weight and center of gravity cockpit readout system
SE438733B (en) 1982-03-05 1985-04-29 Bofors Ab LOAD CELL TYPE CELL
US4507742A (en) 1982-07-30 1985-03-26 Sundstrand Data Control, Inc. Aircraft weight and balance system with automatic loading error correction
US4574360A (en) * 1983-04-01 1986-03-04 Sundstrand Data Control, Inc. Helicopter weight measuring system
US4502555A (en) 1983-09-16 1985-03-05 Mcdonnell Douglas Corporation Portable weighing system for aircraft
US4639872A (en) 1984-02-10 1987-01-27 Aldis Consultants Inc. Method and apparatus for determining weight and center of gravity of a vehicle
US4935885A (en) * 1984-02-10 1990-06-19 Aldis Consultants Inc. Method and apparatus for determining weight and center of gravity of a vehicle
JPS61129532A (en) 1984-11-29 1986-06-17 Tokyo Electric Co Ltd Load cell scale
FR2609546B1 (en) * 1987-01-08 1991-01-04 Aerospatiale METHOD AND SYSTEM FOR DETERMINING THE LONGITUDINAL POSITION OF THE CENTER OF GRAVITY OF AN AIRCRAFT PROVIDED WITH AN ADJUSTABLE HORIZONTAL FENDER
DE4112675A1 (en) 1990-10-20 1992-04-23 Vdo Schindling ARRANGEMENT OF AT LEAST ONE SENSOR ON THE UNDERCARRIAGE OF AN AIRPLANE FOR MEASURING ITS WEIGHT AND FOCUS
CA2086891A1 (en) 1992-01-09 1993-07-10 Vivian Geoffrey Power Method and apparatus for determining the weight and center of gravity of a vehicle, particularly an aircraft
WO1993016359A1 (en) 1992-02-07 1993-08-19 Nance C Kirk Aircraft weight and center of gravity indicator
US5646376A (en) 1994-06-09 1997-07-08 Intercomp Company Aircraft weighing scale with improved base, platform and load cell mounting assembly
US5521827A (en) 1994-09-16 1996-05-28 General Electrodynamics Corporation On-board aircraft weighting and center of gravity determing apparatus and method
US6032090A (en) * 1997-05-06 2000-02-29 General Electrodynamics Corporation System and method for on-board determination of aircraft weight and load-related characteristics

Also Published As

Publication number Publication date
WO2000049377A2 (en) 2000-08-24
WO2000049377A3 (en) 2000-11-30
AU5265400A (en) 2000-09-04
US6353793B1 (en) 2002-03-05
CA2359623C (en) 2006-02-14

Similar Documents

Publication Publication Date Title
CA2359623A1 (en) System and apparatus for determining the center of gravity of an aircraft
US6779621B2 (en) Riderless stabilization of a balancing transporter
US7292925B1 (en) Acceleration estimation device and vehicle
CA2393418A1 (en) Balancing personal vehicle
EP1084901A3 (en) A passenger safety device for an automotive vehicle seat
WO2002042097A3 (en) Vehicle suspension system
CA2323594A1 (en) Independent wheel-lift having a chassis mounted pivot point
MY122293A (en) Apparatus and method for a pitch state estimator for a personal vehicle
EP1186527A3 (en) Rear wheel suspension structure in motorcycle
US20170225736A1 (en) Self-Balancing Load Bearing Vehicle
EP1010611A3 (en) Bicycle brake device
EP0732236A3 (en) Levelling system for motor vehicles
EP0341752A3 (en) Bicycle trainer, and quick release mechanism therefore
EP3419886A1 (en) Power-operated trailer comprising a motor control device
EP0982206A3 (en) Method of estimating vehicle yaw rate
EP1366972A3 (en) A trailing arm suspension assembly
FR2424141A1 (en) VEHICLE SUSPENSION SYSTEM
EP0952076A3 (en) Scooter type vehicle
FR3109764B3 (en) Electric scooter
CN206744776U (en) Manned luggage case
FR2755656B1 (en) DEVICE FOR STORING OR RETAINING OBJECTS IN A MOTOR VEHICLE
EP0887030A3 (en) Arm rest for seat
CN213323497U (en) Flywheel balance structure of automatic driving bicycle
CA2307601A1 (en) Vehicle winch arrangement
CN213555282U (en) VR bicycle device

Legal Events

Date Code Title Description
EEER Examination request
MKLA Lapsed