GB1163209A - Accelerometer - Google Patents
AccelerometerInfo
- 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
Links
Classifications
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P15/00—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration
- G01P15/02—Measuring acceleration; Measuring deceleration; Measuring shock, i.e. sudden change of acceleration by making use of inertia forces using solid seismic masses
- G01P15/08—Measuring 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
- G01P15/13—Measuring 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
- G01P15/132—Measuring 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
-
- G—PHYSICS
- G01—MEASURING; TESTING
- G01R—MEASURING ELECTRIC VARIABLES; MEASURING MAGNETIC VARIABLES
- G01R17/00—Measuring arrangements involving comparison with a reference value, e.g. bridge
- G01R17/02—Arrangements in which the value to be measured is automatically compared with a reference value
- G01R17/06—Automatic balancing arrangements
- G01R17/08—Automatic 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.
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)
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)
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)
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 |
-
0
- NL NL136155D patent/NL136155C/xx active
-
1966
- 1966-09-09 US US578172A patent/US3498138A/en not_active Expired - Lifetime
-
1967
- 1967-09-20 GB GB42892/67A patent/GB1163209A/en not_active Expired
- 1967-09-20 GB GB57688/68A patent/GB1163210A/en not_active Expired
- 1967-09-23 DE DE19671673402 patent/DE1673402B1/en not_active Withdrawn
- 1967-09-25 NL NL6713054A patent/NL6713054A/xx unknown
- 1967-09-28 FR FR122705A patent/FR1538245A/en not_active Expired
- 1967-10-02 BE BE704569D patent/BE704569A/xx not_active IP Right Cessation
-
1972
- 1972-09-22 NL NL7212862.A patent/NL158616B/en not_active IP Right Cessation
Cited By (2)
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 |