GB2045944A - Accelerometers - Google Patents

Accelerometers Download PDF

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Publication number
GB2045944A
GB2045944A GB8006891A GB8006891A GB2045944A GB 2045944 A GB2045944 A GB 2045944A GB 8006891 A GB8006891 A GB 8006891A GB 8006891 A GB8006891 A GB 8006891A GB 2045944 A GB2045944 A GB 2045944A
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GB
United Kingdom
Prior art keywords
accelerometer
cutting portion
steel
abutting
moveable member
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
GB8006891A
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GB2045944B (en
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UK Secretary of State for Defence
Original Assignee
UK Secretary of State for Defence
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 UK Secretary of State for Defence filed Critical UK Secretary of State for Defence
Priority to GB8006891A priority Critical patent/GB2045944B/en
Publication of GB2045944A publication Critical patent/GB2045944A/en
Application granted granted Critical
Publication of GB2045944B publication Critical patent/GB2045944B/en
Expired legal-status Critical Current

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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

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  • Physics & Mathematics (AREA)
  • General Physics & Mathematics (AREA)
  • Geophysics And Detection Of Objects (AREA)

Abstract

An accelerometer includes a thermocouple circuit which comprises a movable metal member (4) abutting a second member (1) made of dissimilar metals, one of the abutting parts (4) having a cutting portion and recording means (10) connected by (7, 8, 9) to the members for recording a thermoelectric signal generated when the cutting portion cuts the abutting part of the other member during acceleration. The members can be of steel and tungsten carbide. The device can be used to study the impact of a projectile. <IMAGE>

Description

SPECIFICATION Improvements in or relating to accelerometers This invention relates to accelerometers and particularly, though not exclusively, to accelerometers capable of recording impact shock signatures.
Known forms of accelerometer include the spring-mass accelerometer and the piezoelectric, piezoresistive, variable capacitance and strain gauge accelerometers. Of these, the piezoelectric and piezoresistive accelerometers are particularly suitable for recording impact shock signatures involving high rates of change of 'g'.
The invention provides an alternative form of accelerometer of simple, rugged construction which is capable of impact shock recording.
According to the present invention accelerometer comprises: a thermocouple circuit which includes a moveable member and a second member, part of which abuts the moveable member, wherein the abutting parts include a cutting edge and wherein the edge and the part which abuts the edge are of dissimilar metals, and means connected to the members for recording a thermoelectric signal generated when the cutting edge cuts the edge abutting part during acceleration.
The moveable member may constitute the seismic of the accelerometer.
Embodiments of the invention will now be described, by way of example only, with reference to the drawings which are schematic and of which Figures 1,2 and 3 show sectional side elevations of first, second and third embodiments respectively, of the invention.
Figure 1 shows an accelerometer which forms part of an acceleration recording system for a shell, and which includes a hollow, cylindrical body2 of steel which carries a conical headed member4 of tungsten carbide mounted on one end of the body by means of screw threaded portions on the body 2 and the member 4. A conical nose 1 of steel is mounted on a compressible spacer 3 of insulative plastics material which extends around the head of member 4 and over the end of the body 2. The apex of the conical headed member 4 extends through a small hole in the spacer 3 into a conical depression in the nose 1 making contact therewith. An insulated wire 7 extends through a bore 5 in the end of the body 2 and connects the member 4 with an input of a dual input operational amplifier 9.A second input of the amplifier 9 is connected by an insulated wire 8 which passes through a bore 6 in the end of the body 2 and through the spacer 3, to the conical nose 1. The wire 8, the steel nose 1, the tungsten carbide member 4 and the wire 7 form part of a thermocouple circuit, the amplifier 9 being arranged to amplify a ther moelectricvoltage produced in the circuit. The amplifier 9 has its output connected to a recorder 10. The amplifier 9 and the recorder 10 are housed in a cavity 11 of the body 2.
In operation, when the nose 1 of the shell travelling in the direction of the arrow A shown in Figure 1 strikes a target 12, the nose undergoes rapid deceleration and the body 2 acts as the seismic mass of the accelerometer and urges the conical headed member 4 into the conical depression in the nose 1, the member 4 cutting the nose 1 and thereby producing a thermoelectric voltage in the thermocouple circuit which is amplified by the amplifier 9.
The amplified voltage is recorded over the dura- tion of the impact by the recorder 10. The value of a thermoelectric voltage V produced in the circuit is given by V k(ba- Oi) where k = constant, and 02 - H, is the difference in speed, due to impact, between member 4 and the nose 1. The temperature at the points where the wires7 and 8 join the member 4 and the nose 1, respectively, will be substantially the same during the very short period of impact.
Figure 2 illustrates a second embodiment of the invention in which a seismic mass of lead 2 is carried on one side of an arm 15 of a U-shaped spring 16.
A conical headed member 4 of tungsten is carried on the other side of the arm 15. A second arm 17 of the spring 16 is fixed and carries a cube 1 of steel mounted on an insulative plastics pad 3 on the arm 17. The head of the cone 4 abuts part of a face of the cube 1. A pneumatic damper 14 is connected to the arms 17 and 15to damp movement of arm 15. An insulated wire 17 connects the member 4 to an input of a dual input operational amplifier 9 and a second insulated wire 8 connects the steel cube 1 to the other input of the amplifier 9. The amplifier 9 has its output connected to a recorder 10. The wires 7 and 8, the cube 1 and the cone 4 form part of a thermocouple circuit.
In operation, when the accelerometer is accelerated such that the cubel which constitutes the seismic mass of the accelerometer is urged in the direction of the arrow B in Figure 2 towards the steel cube, the head of the cone 4 will cut into the cube 1 and produce a thermoelectric voltage which is amplified by the amplifier 9 and the amplified voltage recorded in the recorder 10.
Figure 3 illustrates a third embodiment of the invention which forms part of an acceleration recording system for a shell includes a conical headed member 1 of steel which is carried on a closed end of a steel tube 3. The tube 3 is slidable along its axis in a coaxial bore 11 in a steel body 2 which forms part of a casing of the shell. The bore 11 terminates at one end in a longer diameter coaxial bore 5 and at the other end which is remote from the member 1 in a chamber 6. A tungsten blade 4 of arcuate configuration is ridigly fixed in a slot in the tube 3 and in the position shown in Figure 3 a tip 13 of the blade is closely spaced from the mouth of the bore 5 and is at a slightly greater distance from the axis of the tube than the radius of the bore 5. An insulated wire 7 extends through the tube 3 into the chamber 6 and connects the blade 4 with one input of a dual input amplifier 9. A second input of the amplifier 9 is connected by an insulated wire 8 to the body 2 at a region which forms part of a wall of the chamber 6.
As in the previous embodiments the amplifier 9 has its output connected to a recorder 10, and the wires 7 and 8, the steel body 2 and the tungsten blade 4 form part of a thermocouple circuit.
In operation, when the conical headed member 1 strikes a hard target 12 the tube 3 is urged along the bore 11 towards the chamber 6. The tungsten blade 4 cuts the body 2 in a region which forms a cylindrical wall of the bore 5 and a thermoelectric voltage is generated amplified and recorded as in the previous embodiments.

Claims (7)

1. An accelerometer comprising a thermocouple circuit which includes a moveable member and a second member part of which abuts the moveable member, wherein the abutting parts include a cutting portion and wherein the cutting portion and the part which abuts the portion are composed of dissimilar metals, and means connected to the members for recording a thermoelectric signal generated when the cutting portion cuts the edge abutting part during acceleration.
2. An accelerometer as claimed in claim 1 wherein the moveable member constitutes the accelerometer seismic mass.
3. An accelerometer as in claim 1 or claim 2 wherein the cutting portion comprises a cone.
4. An accelerometer as in claim 1 or claim 2 wherein the cutting portion comprises a knife edge.
5. An accelerometer as in any of the above claims wherein the cutting portion is composed of tungsten carbide and the abutting part of the other member is composed of steel.
6. An accelerometer as claimed in any of the above claims further including damping means connected to the moveable member and arranged to damp the movement thereof.
7. An accelerometersubstantially as described herein with reference to the drawings.
GB8006891A 1979-03-01 1980-02-29 Accelerometers Expired GB2045944B (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB8006891A GB2045944B (en) 1979-03-01 1980-02-29 Accelerometers

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
GB7907291 1979-03-01
GB8006891A GB2045944B (en) 1979-03-01 1980-02-29 Accelerometers

Publications (2)

Publication Number Publication Date
GB2045944A true GB2045944A (en) 1980-11-05
GB2045944B GB2045944B (en) 1983-03-09

Family

ID=26270741

Family Applications (1)

Application Number Title Priority Date Filing Date
GB8006891A Expired GB2045944B (en) 1979-03-01 1980-02-29 Accelerometers

Country Status (1)

Country Link
GB (1) GB2045944B (en)

Also Published As

Publication number Publication date
GB2045944B (en) 1983-03-09

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Legal Events

Date Code Title Description
PCNP Patent ceased through non-payment of renewal fee