GB1163209A - Accelerometer - Google Patents

Accelerometer

Info

Publication number
GB1163209A
GB1163209A GB42892/67A GB4289267A GB1163209A GB 1163209 A GB1163209 A GB 1163209A GB 42892/67 A GB42892/67 A GB 42892/67A GB 4289267 A GB4289267 A GB 4289267A GB 1163209 A GB1163209 A GB 1163209A
Authority
GB
United Kingdom
Prior art keywords
axis
magnet
mass
diameter
coil
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
Application number
GB42892/67A
Inventor
Robert Edward Stewart
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.)
Litton Industries Inc
Original Assignee
Litton Industries 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
Priority to NL136155D priority Critical patent/NL136155C/xx
Priority to US578172A priority patent/US3498138A/en
Application filed by Litton Industries Inc filed Critical Litton Industries Inc
Priority to GB42892/67A priority patent/GB1163209A/en
Priority to GB57688/68A priority patent/GB1163210A/en
Priority to DE19671673402 priority patent/DE1673402B1/en
Priority to NL6713054A priority patent/NL6713054A/xx
Priority to FR122705A priority patent/FR1538245A/en
Priority to BE704569D priority patent/BE704569A/xx
Publication of GB1163209A publication Critical patent/GB1163209A/en
Priority to NL7212862.A priority patent/NL158616B/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P15/00Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
    • G01P15/02Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
    • G01P15/08Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values
    • G01P15/13Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by measuring the force required to restore a proofmass subjected to inertial forces to a null position
    • G01P15/132Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses with conversion into electric or magnetic values by measuring the force required to restore a proofmass subjected to inertial forces to a null position with electromagnetic counterbalancing means
    • GPHYSICS
    • G01MEASURING; TESTING
    • G01RMEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
    • G01R17/00Measuring arrangements involving comparison with a reference value, e.g. bridge
    • G01R17/02Arrangements in which the value to be measured is automatically compared with a reference value
    • G01R17/06Automatic balancing arrangements
    • G01R17/08Automatic balancing arrangements in which a force or torque representing the measured value is balanced by a force or torque representing the reference value

Landscapes

  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Electromagnetism (AREA)
  • Gyroscopes (AREA)
  • Indication And Recording Devices For Special Purposes And Tariff Metering Devices (AREA)
  • Reciprocating, Oscillating Or Vibrating Motors (AREA)

Abstract

1,163,209. Measuring acceleration electrically. LITTON INDUSTRIES Inc. Sept. 20, 1967, No.42892/67. Heading G1N. An accelerometer comprises an annular body 84, Fig. 8, attached to a fixed annular member 42 by diametrically arranged flexible hinges 92, 94, 98, 101, Fig.10, so that the body is free to pivot about diametrical axis 170 through its centre of mass. An additional mass, e.g. 150, is mounted on the body so that the centre of mass of the composite body is not coincident with the axis 170, an applied acceleration thus producing a turning force on the body. The position of the mass on the body depends on the plane of the applied acceleration, e.g. for accelerations transverse to the plane of the body, the mass is arranged round the circumference or equally at the ends of the diameter perpendicular to the axis 170; for accelerations in the plane of the body, the mass is arranged at one point on the circumference. As shown, ceramic body 84 and member 42 are hinged together by pieces of metal foil 92, 94, 98, 101, e.g. electrolessly deposited nickel, which are also used as electrical connections to and from the pivoting body 84. Movement of the body is sensed by changes in capacitance between two pieces of metal foils 91, 93, Fig. 10, on the lower surface of the body and a magnet body 50 forming a third common capacitor plate. The two capacitors (156, 158, Fig. 14, not shown), are connected in adjacent arms of an A. C. bridge circuit whose output after demodulation at (168) is fed to a force balance coil 82 attached to the circumference of the lower surface of the body 84. The coil is suspended in the flux gap between the annular magnet 50 of aluminium nickel alloy magnetized so that its poles lie at the ends of a diameter transverse to axis 170, and a ring 78 of magnetic material forming part of the return path of the magnetic flux. Thus application of current to the coil 82 produces a resolving torque in the coil which returns the body 84 to its zero position. This current is also indicative of the acceleration. Temperature compensation for magnet 50. The field strength of the magnet 50 tends to decrease with increasing temperature. Thus, to maintain the flux in the gap between magnet and ring 78 constant at the poles, the gap must be varied inversely with temperature. To this end an annular disc 52 of e. g. aluminium provided with an insulating layer 70 on its upper surface, is provided, having projections (79, 80, Fig. 13, not shown), at opposite ends of a diameter parallel to axis 170, which bear against the ring 78. As the temperature increases the disc 52 expands producing an elongation of the diameter of the ring 78 parallel to axis 170 and corresponding contraction of its diameter perpendicular to axis 170 (see dot-dash line (182)) producing the required reduction in the flux gap at the poles of the magnet. The above described temperature compensated magnetic system is also described and claimed in Specification 1,163, 210.
GB42892/67A 1966-09-09 1967-09-20 Accelerometer Expired GB1163209A (en)

Priority Applications (9)

Application Number Priority Date Filing Date Title
NL136155D NL136155C (en) 1966-09-09
US578172A US3498138A (en) 1966-09-09 1966-09-09 Accelerometer
GB42892/67A GB1163209A (en) 1966-09-09 1967-09-20 Accelerometer
GB57688/68A GB1163210A (en) 1966-09-09 1967-09-20 Temperature compensating of Electromagnetic systems of Measuring Instruments
DE19671673402 DE1673402B1 (en) 1966-09-09 1967-09-23 Accelerometer
NL6713054A NL6713054A (en) 1966-09-09 1967-09-25
FR122705A FR1538245A (en) 1966-09-09 1967-09-28 Accelerometer
BE704569D BE704569A (en) 1966-09-09 1967-10-02
NL7212862.A NL158616B (en) 1966-09-09 1972-09-22 TEMPERATURE COMPENSATED, ELECTROMAGNETICALLY OPERATING MEASUREMENT INSTRUMENT.

Applications Claiming Priority (7)

Application Number Priority Date Filing Date Title
US57817266A 1966-09-09 1966-09-09
GB42892/67A GB1163209A (en) 1966-09-09 1967-09-20 Accelerometer
GB57688/68A GB1163210A (en) 1966-09-09 1967-09-20 Temperature compensating of Electromagnetic systems of Measuring Instruments
DEL0057481 1967-09-23
NL6713054A NL6713054A (en) 1966-09-09 1967-09-25
FR122705A FR1538245A (en) 1966-09-09 1967-09-28 Accelerometer
NL7212862.A NL158616B (en) 1966-09-09 1972-09-22 TEMPERATURE COMPENSATED, ELECTROMAGNETICALLY OPERATING MEASUREMENT INSTRUMENT.

Publications (1)

Publication Number Publication Date
GB1163209A true GB1163209A (en) 1969-09-04

Family

ID=27561665

Family Applications (2)

Application Number Title Priority Date Filing Date
GB42892/67A Expired GB1163209A (en) 1966-09-09 1967-09-20 Accelerometer
GB57688/68A Expired GB1163210A (en) 1966-09-09 1967-09-20 Temperature compensating of Electromagnetic systems of Measuring Instruments

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB57688/68A Expired GB1163210A (en) 1966-09-09 1967-09-20 Temperature compensating of Electromagnetic systems of Measuring Instruments

Country Status (6)

Country Link
US (1) US3498138A (en)
BE (1) BE704569A (en)
DE (1) DE1673402B1 (en)
FR (1) FR1538245A (en)
GB (2) GB1163209A (en)
NL (3) NL6713054A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2194341A (en) * 1986-07-26 1988-03-02 Messerschmitt Boelkow Blohm Capacitive acceleration sensors

Families Citing this family (26)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4182187A (en) * 1978-04-24 1980-01-08 Sundstrand Data Control, Inc. Force balancing assembly for transducers
US4284096A (en) * 1980-06-04 1981-08-18 Ford Motor Company Automatic transmission governor having deceleration sensitive pressure switching feature
US4338819A (en) * 1980-09-08 1982-07-13 Systron-Donner Corporation Accelerometer including an overall arrangement for reducing temperature related errors
US4400979A (en) * 1981-07-14 1983-08-30 Sundstrand Data Control, Inc. Force transducer flexure with conductors on surfaces in the neutral bending plane
US4441366A (en) * 1981-07-14 1984-04-10 Sundstrand Data Control, Inc. Flexure with electrical conductor
US4394405A (en) * 1981-07-14 1983-07-19 Sundstrand Data Control, Inc. Method of making force transducer flexure
US4399700A (en) * 1981-07-14 1983-08-23 Sundstrand Data Control, Inc. Force transducer flexure with conductors on surfaces in the neutral bending plane
US4699006A (en) * 1984-03-19 1987-10-13 The Charles Stark Draper Laboratory, Inc. Vibratory digital integrating accelerometer
US4736629A (en) * 1985-12-20 1988-04-12 Silicon Designs, Inc. Micro-miniature accelerometer
DE3785736T2 (en) * 1986-06-27 1993-08-19 Sundstrand Data Control TRANSLATION ACCELERATOR.
US4872342A (en) * 1986-06-27 1989-10-10 Sundstrand Data Control, Inc. Translational accelerometer and accelerometer assembly method
US4987780A (en) * 1987-11-16 1991-01-29 Litton Systems, Inc. Integrated accelerometer assembly
JP2789218B2 (en) * 1989-05-29 1998-08-20 株式会社トキメック Accelerometer
US5253526A (en) * 1990-05-30 1993-10-19 Copal Company Limited Capacitive acceleration sensor with free diaphragm
US5249465A (en) * 1990-12-11 1993-10-05 Motorola, Inc. Accelerometer utilizing an annular mass
US5220835A (en) * 1991-09-12 1993-06-22 Ford Motor Company Torsion beam accelerometer
US5404749A (en) * 1993-04-07 1995-04-11 Ford Motor Company Boron doped silicon accelerometer sense element
US6199874B1 (en) 1993-05-26 2001-03-13 Cornell Research Foundation Inc. Microelectromechanical accelerometer for automotive applications
US5610335A (en) * 1993-05-26 1997-03-11 Cornell Research Foundation Microelectromechanical lateral accelerometer
US5600067A (en) * 1993-08-18 1997-02-04 Alliedsignal, Inc. Torque wire thermal strain relief
US5640133A (en) * 1995-06-23 1997-06-17 Cornell Research Foundation, Inc. Capacitance based tunable micromechanical resonators
US5978972A (en) * 1996-06-14 1999-11-09 Johns Hopkins University Helmet system including at least three accelerometers and mass memory and method for recording in real-time orthogonal acceleration data of a head
US5644086A (en) * 1996-10-08 1997-07-01 Tokyo Gas Co., Ltd. Preloaded linear beam vibration sensor
US5914553A (en) * 1997-06-16 1999-06-22 Cornell Research Foundation, Inc. Multistable tunable micromechanical resonators
US10180445B2 (en) 2016-06-08 2019-01-15 Honeywell International Inc. Reducing bias in an accelerometer via current adjustment
CN112798993B (en) * 2021-04-08 2021-07-13 中国电子科技集团公司第九研究所 Device and method for measuring temperature coefficient of permanent magnet material based on accelerometer

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2959459A (en) * 1953-08-04 1960-11-08 James J Ryan Flight recorder
GB783104A (en) * 1955-01-13 1957-09-18 Mini Of Supply Improvements in accelerometers
US3339419A (en) * 1964-07-02 1967-09-05 North American Aviation Inc Accelerometer

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2194341A (en) * 1986-07-26 1988-03-02 Messerschmitt Boelkow Blohm Capacitive acceleration sensors
GB2194341B (en) * 1986-07-26 1990-05-23 Messerschmitt Boelkow Blohm Capacitive acceleration sensors

Also Published As

Publication number Publication date
NL6713054A (en) 1969-03-27
DE1673402B1 (en) 1970-12-03
BE704569A (en) 1968-04-02
US3498138A (en) 1970-03-03
NL158616B (en) 1978-11-15
NL7212862A (en) 1972-12-27
FR1538245A (en) 1968-08-30
GB1163210A (en) 1969-09-04
NL136155C (en)

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PCNP Patent ceased through non-payment of renewal fee