US20010037684A1 - Permanent magnet rotary accelerometer - Google Patents
Permanent magnet rotary accelerometer Download PDFInfo
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- US20010037684A1 US20010037684A1 US09/904,399 US90439901A US2001037684A1 US 20010037684 A1 US20010037684 A1 US 20010037684A1 US 90439901 A US90439901 A US 90439901A US 2001037684 A1 US2001037684 A1 US 2001037684A1
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- cup
- magnetic
- return path
- stator core
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- 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
- G01P15/003—Kinematic accelerometers, i.e. measuring acceleration in relation to an external reference frame, e.g. Ferratis accelerometers
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- G—PHYSICS
- G01—MEASURING; TESTING
- G01P—MEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
- G01P3/00—Measuring linear or angular speed; Measuring differences of linear or angular speeds
- G01P3/42—Devices characterised by the use of electric or magnetic means
- G01P3/44—Devices characterised by the use of electric or magnetic means for measuring angular speed
- G01P3/49—Devices characterised by the use of electric or magnetic means for measuring angular speed using eddy currents
Definitions
- the invention disclosed broadly relates to the field of accelerometers and more particularly to permanent magnet accelerometers for sensing rotational or angular acceleration.
- Rotary accelerometers have been in existence for years. Rotary accelerometers may be used to provide closed loop motion control of a load through the use of feedback techniques. The acceleration signal from an accelerometer may be used to electronically simulate larger, smaller or varying system inertia.
- a DC (Direct Current) excited rotary accelerometer can be found in U.S. Pat. No. 2,090,521, entitled “Accelerometer”, by inventor Robert Serrell, and issued on Aug. 17, 1937. (Hereinafter this patent is referred to as Serrell.)
- This accelerometer makes use of the phenomenon of armature reaction in a rotating dynamo-electric apparatus to provide an indication of the magnitude of the acceleration.
- the magnitude of the magnetic field produced by currents induced in the armature of a generator varies with acceleration of the rotating member.
- stator winding core pieces 7 , 8 and 9 of FIG. 1 and FIG. 2 are constructed from distinct pieces of ferromagnetic material. Stated differently, the stator winding core pieces 7 , 8 , and 9 are fabricated from at least three different pieces. The use of separate stator winding core pieces does not provide maximum sensitivity of pickup coils 6 a and 6 b due to the increase in 0 magnetic reluctance. Moreover, for the application of accelerometers in a harsh environments such as aerospace applications, the exposure to wide temperature fluctuations, vibrations, and shock and high g-forces is not structurally sound. Accordingly, a need exists for an accelerometer that has very high sensitivity even in demanding applications in harsh environments.
- a rotary accelerometer is used to complement closed loop control systems such as brushless D.C. motors, stepper motors, A.C. motors, hydraulic motors, pneumatic motors, or any other device which is controlled through rotary motion.
- the rotary accelerometer provides a direct output of the acceleration signal and can be integrally mounted to a motor or other rotating machine.
- the four components whose configuration changes in the various embodiments are as follows: (i) nonrotating permanent magnets; (ii) a nonrotating stator core; (iii) a rotating electrically conductive cup; and (iv) a rotating or nonrotating (depending on the configuration) magnetically permeable return path. Five different embodiments are described for various configurations of these four components.
- a permanent magnet rotary accelerometer comprising: a cylindrical magnetic return path formed out of magnetic permeable material; an electrically conductive cup with an axis for rotation there around, the cup surrounding the magnetic return path; one or more sets of permanent magnets having opposite magnetic polarity, surrounding the cup, for a producing magnetic field through the cup into the magnetic return path, thereby inducing eddy currents inside the cup when rotating in the magnetic field; a stator core formed out of magnetic permeable material surrounding the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
- FIG. 1A is a partial side view of the first embodiment of the permanent magnet accelerometer with magnets positioned outside a rotating cup, a nonrotating stator core positioned outside the cup and a rotating magnetic return path inside the cup, according to the present invention.
- FIG. 1B is a cross-sectional view of the permanent magnet accelerometer of FIG. 1A taken along lines A-A′.
- FIG. 2A is a partial side view of the second embodiment of the permanent magnet accelerometer with magnets positioned outside a rotating cup, a nonrotating stator core positioned outside the cup and a nonrotating magnetic return path inside the cup, according to the present invention.
- FIG. 2B is a cross-sectional view of the permanent magnet accelerometer of FIG. 2A taken along lines A-A′.
- FIG. 3A is a partial side view of the third embodiment of the permanent magnet accelerometer with magnets positioned inside a rotating cup, a nonrotating stator core positioned outside the cup and a nonrotating magnetic return path inside the cup, according to the present invention.
- FIG. 3B is a cross-sectional view of the permanent magnet accelerometer of FIG. 3A taken along lines A-A′.
- FIG. 4A is a partial side view of the forth embodiment of the permanent magnet accelerometer with magnets positioned inside a rotating cup, a nonrotating stator core positioned inside the cup and a nonrotating magnetic return path outside the cup that rotates according to the present invention.
- FIG. 4B is a cross-sectional view of the permanent magnet accelerometer of FIG. 4A taken along lines A-A′.
- FIG. 5A is a partial side view of the fifth embodiment of the permanent magnet accelerometer with magnets positioned outside the cup, a nonrotating stator core positioned inside the cup and a nonrotating magnetic return path outside the cup that is stationary according to the present invention.
- FIG. 5B is a cross-sectional view of the permanent magnet accelerometer of FIG. 1A taken along lines A-A′.
- FIG. 6A is a graph of an open loop stepper motor without using an accelerometer.
- FIG. 6B is a graph of an open loop stepper motor of FIG. 6A using the accelerometer according to the present invention.
- FIG. 1A shows a partial side view of the first embodiment of the permanent magnet accelerometer 100 and FIG. 1B is a cross-sectional view of the permanent magnet accelerometer of FIG. 1A taken along lines A-A′, according to the present invention.
- a housing 102 with an end bell 104 encloses the internal components of accelerometer 100 .
- a mechanical input shaft 106 is coupled to a motor (not shown), such as a electrical, pneumatic, hydraulic, combustion orequivalent, rotating machine.
- a motor such as a electrical, pneumatic, hydraulic, combustion orequivalent, rotating machine.
- an electrical rotating machine is a stepper motor.
- a plurality of bearings 108 are used to reduce the friction of input shaft 106 turning in housing 102 .
- a stator core 110 forms an integral return path with pickup members 112 .
- the stator core 110 senses the change in eddy currents induced in an electrically conductive cup 120 as further described below. It is important to note that the stator core 110 is formed out of magnetic permeable material, such as silicon iron or Hyperco 50, for example. All of the stator core 110 including the integral return path with pickup members 112 are formed from one continuous piece of material. This single piece design of stator core 110 provides lower reluctance, higher output voltages and increased sensitivity to the eddy currents induced in the cup 120 .
- the stator core 110 is machined from one piece of magnetically permeable material.
- the stator core is a laminate or of sintered construction, where two or more layers of magnetically permeable material are sandwiched together. At least one layer is one piece that forms a low reluctance path between the pickup members 112 .
- the single piece design of stator core 110 is very rugged and can operate effectively in harsh environments, such as aerospace, where the accelerometer 100 is subjected to a wide range of temperature fluctuations, constant shock and vibration, and large gravitational forces.
- Stator windings 114 are wound around or embedded in the stator core 110 near pickup members 112 .
- Electrical output wires 116 provide a signal from the stator windings 114 which is proportional to the eddy currents induced in the cup 120 rotating in a magnetic field formed between magnets 118 .
- the complementary components of housing 102 , mechanical input shaft 106 , end bell 104 and bearings 108 are only one of many mechanical adaptations to the accelerometer 100 according to the present invention and several other configurations of these complementary components are possible to provide the proper alignment of these components with the components that are discussed in FIG. 1B.
- FIGS. 2A, 3A, 4 A and 5 A have similar construction for these components.
- One or more pairs of nonrotating permanent magnets 116 are positioned outside the electrically conductive rotating cup 120 .
- the cup 120 is mounted on shaft 108 and is made out of any material, such as copper, that has low electrical resistance but high magnetic reluctance.
- a magnetically permeable return path 122 is disposed on shaft 106 .
- the magnetically permeable return path 122 and the shaft 106 are formed from a single piece of magnetically permeable material.
- the magnetically permeable return path 122 is a separate price of magnetically permeable material attached to shaft 106 .
- the pair of permanent magnets 116 with opposite magnet polarity, form a magnetic field (not shown) through the cup into the magnetic return path.
- the cup 120 mounted on input shaft 108 rotates through the magnetic field formed by magnets 118 and induces eddy currents within the cup 120 under principals know in the art, such as Faraday's and Maxwell's Laws.
- the eddy currents formed in the cup 120 are proportional to the angular acceleration at which the cup 120 moves through the magnetic field.
- the pickup members 112 of stator core 110 sense the magnitude of the secondary magnetic field generated by the eddy currents that form in the cup 120 .
- the word “secondary” magnetic field is used to distinguish from the magnetic field produced by the permanent magnets.
- a signal is produced by the stator windings 114 on to wire 114 directly proportional to the eddy currents. It should be understood that no D.C. excitation is needed with the permanent magnets so that the power requirements of prior art D.C. accelerometers are eliminated.
- FIG. 6A is a graph of an open loop stepper motor without using an accelerometer 100 .
- a C.D.A. Intercorp type 16-206-20 stepper motor coupled to a 100:1 gear head with a inertia factor of 38 is used.
- the Y-axes of the graph is in pulses per second and the X-axes are in units of Torque (lb.-in).
- FIG. 6B is a graph of the stepper motor of FIG. 6A using the accelerometer according to the present invention. It is important to note that the scale and the components of FIGS. 6A and 6B are identical.
- FIG. 6A illustrates several performance enhancements.
- the use of the accelerometer according to the present invention provides performance enhancements of higher torques and operating velocities.
- the accelerometer of the present invention has no “lost steps” and pulse by pulse information is provided.
- the resonance areas, or unstable performance are inherently nullified, and dynamic speed versus torque is realized.
- stepper motor application will notice the performance enhancements of the response rate, 610 , the pull in torque 612 , and the torque at low pulse rate 614 , as compared with the FIG. 6A.
- the accelerometer 100 is an extremely useful component in high performance and/or high load inertia servo actuator systems. Since the accelerometer 100 requires no excitation or demodulation, the DC output may be directly Op-Amp integrated for an angular rate damping signal of the motor. This information, along with the angular acceleration signal provides tremendous flexibility in contouring the system response, and controlling the transfer function.
- the accelerometer 100 can make the motor rotor inertia electronically “look” larger or smaller through this feedback technique.
- This electronic technique is like adding a variable electronic “flywheel” to the system, and provides a higher order effect, as compared to electronic damping through tachometer feedback. This may provide high forward loop gain, while maintaining a stable servo system.
- the electronic flywheel may be controlled to provide these characteristics dynamically in the system. Other advantages include acceleration control, and disturbance attenuation.
- FIGS. 2A and 2B The second embodiment of an accelerometer 200 is illustrated in FIGS. 2A and 2B.
- the components are numbered to correspond to the similar components of FIG. 1.
- permanent magnets are 218 where in FIG. 1, they are numbered 118
- housing in FIG. 2 is numbered 202 where the housing in FIG. 1 is numbered 102 and so on.
- the structural difference between the second embodiment and the first embodiment is that like first embodiment, the cup 220 rotates, but the magnetic return path 222 inside the cup 220 , unlike in the first embodiment, does not rotate. There is a small air gap 224 formed between the rotating cup 220 and the nonrotating magnetic return path 222 . Only the rotating cup 220 is coupled to the mechanical input shaft 206 .
- the end bell 204 may serve as an optional magnetic return path.
- This design of accelerometer 200 has lower rotating inertia as compared with the first embodiment because only the cup 220 and not the magnetically permeable return path 222 rotates.
- FIG. 3A and 3B The third embodiment of an accelerometer 300 is illustrated in FIG. 3A and 3B.
- the components are numbered to correspond to the similar components of FIG. 1.
- the structural difference between the third embodiment and the first embodiment is that like first embodiment, the cup 320 rotates, but the magnetic return path 322 inside the cup 320 , unlike in the first embodiment, does not rotate.
- Only the rotating cup 320 is coupled to the mechanical input shaft 306 .
- the permanent magnets 318 have been moved to be positioned inside the cup 320 .
- the permanent magnets are disposed on magnetically permeable return path 322 .
- the end bell 304 may serve as an optional magnetic return path.
- This design of accelerometer 300 has lower rotating inertia as compared with the first embodiment because only the cup 320 and not the magnetically permeable return path 322 rotates. Because the magnets are positioned inside the cup 320 , bonded ring magnets may be used for permanent magnets 318 . In addition, this design of accelerometer 300 exhibits some of the most rugged design characteristics for harsh environments and some of the highest output voltage as compared with other embodiments.
- FIGS. 4A and 4B The fourth embodiment of an accelerometer 400 is illustrated in FIGS. 4A and 4B.
- the components are numbered to correspond to the similar components of FIG. 1.
- the structural difference between the fourth embodiment and the first embodiment is that like first embodiment, the cup 420 rotates, but all of the other components, unlike the first embodiment, all of the components, the stator core 410 including the integral return path with pickup members 412 , the permanent magnets 418 , and the windings 414 are all mounted inside the rotating cup 420 .
- the magnetic permeable return path 422 is outside the rotating cup 420 .
- the housing 402 serves as the magnetic permeable return path.
- the magnetic permeable return path 422 is a sleeve inside the housing 402 .
- This design of accelerometer 400 exhibits some of the lowest cost to manufacture because of the ease of construction.
- FIGS. 5A and 5B The fifth embodiment of an accelerometer 500 is illustrated in FIGS. 5A and 5B.
- the components are numbered to correspond to the similar components of FIG. 1.
- the structural difference between the fifth embodiment and the first embodiment is that like first embodiment, the cup 520 rotates, but all of the other components, unlike the first embodiment, all of the components, the stator core 510 including the integral return path with pickup members 512 , and the windings 514 are all mounted inside the rotating cup 520 .
- the magnetic permeable return path 522 and the permanent magnets are outside the rotating cup 520 .
- the housing 502 serves as the magnetic permeable return path.
- the magnetic permeable return path 522 is a sleeve inside the housing 502 .
- This design of accelerometer 500 exhibits some of the lowest cost to manufacture because of the ease of construction.
Abstract
A permanent magnet rotary accelerometer comprising: a cylindrical magnetic return path formed out of magnetic permeable material; an electrically conductive cup with an axis for rotation there around, the cup surrounding the magnetic return path; one or more sets of permanent magnets having opposite magnetic polarity, surrounding the cup, for a producing magnetic field through the cup into the magnetic return path, thereby inducing eddy currents inside the cup when rotating in the magnetic field; a stator core formed out of magnetic permeable material surrounding the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
Description
- Not applicable
- 1. Field of the Invention
- The invention disclosed broadly relates to the field of accelerometers and more particularly to permanent magnet accelerometers for sensing rotational or angular acceleration.
- 2. Description of the Related Art
- Rotary accelerometers have been in existence for years. Rotary accelerometers may be used to provide closed loop motion control of a load through the use of feedback techniques. The acceleration signal from an accelerometer may be used to electronically simulate larger, smaller or varying system inertia. One example of a DC (Direct Current) excited rotary accelerometer can be found in U.S. Pat. No. 2,090,521, entitled “Accelerometer”, by inventor Robert Serrell, and issued on Aug. 17, 1937. (Hereinafter this patent is referred to as Serrell.) This accelerometer makes use of the phenomenon of armature reaction in a rotating dynamo-electric apparatus to provide an indication of the magnitude of the acceleration. The magnitude of the magnetic field produced by currents induced in the armature of a generator varies with acceleration of the rotating member.
- Another accelerometer is disclosed in U.S. Pat. No. 3,178,641 entitled “Drag Cup Tachometer Accelerometer” by inventor J. H. Varterasian, issued on Apr. 13, 1965. (Hereinafter this patent is referred to as Varterasian.) This is a DC excited accelerometer that provides a conductive drag cup of a tachometer generator with alternating current and direct current excitation. The device processes an alternating current and a direct current output signals which are a function of the drag cup speed and acceleration respectfully.
- Another rotary accelerometer is disclosed is U.S. Pat. No. 4,507,607, entitled “AngularAccelerometer” by Inventor William R. Caputo, issued on Mar. 26, 1985. (Hereinafter this patent is referred to as Caputo.) Disclosed is an angular accelerometer with DC excitation which generates a direct usable signal and stationary coil proportional to the instantaneous acceleration rate of a rotary element.
- Yet another rotary accelerometer is disclosed in U.S. Pat. No. 3,555,326 entitled “Accelerometer for a Vehicular Anti-Skid System with Sheet Loader” by Inventors Abootaleb Talebi et al., issued Jan. 12, 1971. (Herein after this patent is referred to as Talebi.) This permanent rotary accelerometer has a solid cylindrical ferromagnetic rotor rotationally coupled to a vehicle wheel and coated with conductive non-ferromagnetic metal sheet.
- Although all these rotary accelerometers are useful they are not without their shortcomings. One shortcoming of other acceleration processes is the use of position or velocity signals to derive acceleration signal. The double differentiation of a position signal or the single differentiation of a velocity signal is accomplished using analog and digital differentiation circuitry. This differentiation process adds electrical noise to the output signal. This noise is undesirable for high performance systems. Accordingly, a need exists for an accelerometer that eliminates the differentiation circuitry and provides an acceleration output signal directly.
- Continuing further, several of the patents by Serrell, Varterasian and Caputo referenced above, use DC excitation. One shortcoming of the use of DC excited accelerometers is that the output gain signal for the acceleration is dependent on the excitation signal for the direct current excitation. The dependence on the excitation signal can lead to a wide drift in accelerometer output signal. Therefore, a need exists to provide an accelerometer whose output voltage is more stable and does not fluctuate when the input voltage shifts.
- Another shortcoming of the use of DC excited accelerometers is that a power source is required to produce the DC voltage along with the companion filtering circuitry and often times a rectifier to condition the power source. These additional components add cost and weight, and besides adding cost and adding weight, also increase the size of the accelerometers. Large accelerometer configurations are difficult to integrate on a motor or other rotating machine. Many times, designer engineers make use of mechanical couplings to integrate motors into specific applications. However, these couplings add weight and space. In addition, these couplings contribute to windup and electrical noise in the accelerometer output signal. Accordingly, a need exists for a compact configuration of an accelerometer which may be integrated directly into an electric motor or other similar rotating machine.
- Another shortcoming with the use of DC excited accelerometers is that in regards to the output, ripples, fluctuations or any noise present in a DC excitation source are translated to the accelerometer output signal. This produces an undesirable signal-to-noise ratio on the output. To eliminate this undesirable noise, the output signal requires filtering which adds lag between the rotation of the shaft being measured and the output of the signal being produced. Accordingly, a need exists for a rotary accelerometer that provides a direct output signal and does not require excessive filtering or demodulation.
- Another shortcoming of the use of DC excited accelerometers is that output power level or gain is lower than permanent magnet excitations. Stated differently, the output voltage per unit of acceleration is much lower within a given frame size. Accordingly, a need exists to provide an accelerometer that has high output voltage levels.
- Turning now to the permanent magnet accelerometers available today, such as the permanent magnet accelerometer disclosed by the Talebi patent, there are several shortcomings. One shortcoming of Talebi as shown in FIG. 2 is that pick up coil6A and 6B are separate from magnetic shells 4 and 5 of FIG. 2. These separate pieces reduce the amount of sensitivity that can be measured with this device. Accordingly, a need exists to provide a permanent magnet accelerometer with high acceleration sensitivity.
- Another shortcoming of the permanent magnet accelerometer disclosed by the Talebi patent is that the rotor uses a coating that is galvanically (electroplating) applied. The uniformity of coatings and platings are difficult to maintain during the manufacturing processes. Moreover, environmental conditions, such as shock, and vibrations, reduce the effectiveness of the plating. Accordingly, a need exists for an accelerometerthat overcomes this shortcoming and is able to perform in harsh environments.
- Still another shortcoming of the permanent magnet accelerometer disclosed by Talebi is that the stator winding core pieces7, 8 and 9 of FIG. 1 and FIG. 2 are constructed from distinct pieces of ferromagnetic material. Stated differently, the stator winding core pieces 7, 8, and 9 are fabricated from at least three different pieces. The use of separate stator winding core pieces does not provide maximum sensitivity of pickup coils 6 a and 6 b due to the increase in0 magnetic reluctance. Moreover, for the application of accelerometers in a harsh environments such as aerospace applications, the exposure to wide temperature fluctuations, vibrations, and shock and high g-forces is not structurally sound. Accordingly, a need exists for an accelerometer that has very high sensitivity even in demanding applications in harsh environments.
- Briefly, in accordance with the present invention, a rotary accelerometer is used to complement closed loop control systems such as brushless D.C. motors, stepper motors, A.C. motors, hydraulic motors, pneumatic motors, or any other device which is controlled through rotary motion. The rotary accelerometer provides a direct output of the acceleration signal and can be integrally mounted to a motor or other rotating machine. The four components whose configuration changes in the various embodiments are as follows: (i) nonrotating permanent magnets; (ii) a nonrotating stator core; (iii) a rotating electrically conductive cup; and (iv) a rotating or nonrotating (depending on the configuration) magnetically permeable return path. Five different embodiments are described for various configurations of these four components.
- In one embodiment, a permanent magnet rotary accelerometer comprising: a cylindrical magnetic return path formed out of magnetic permeable material; an electrically conductive cup with an axis for rotation there around, the cup surrounding the magnetic return path; one or more sets of permanent magnets having opposite magnetic polarity, surrounding the cup, for a producing magnetic field through the cup into the magnetic return path, thereby inducing eddy currents inside the cup when rotating in the magnetic field; a stator core formed out of magnetic permeable material surrounding the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
- The subject matter which is regarded as the invention is particularly pointed out and distinctly claimed in the claims at the conclusion of the specification. The foregoing and other objects, features, and advantages of the invention will be apparent from the following detailed description taken in conjunction with the accompanying drawings.
- FIG. 1A is a partial side view of the first embodiment of the permanent magnet accelerometer with magnets positioned outside a rotating cup, a nonrotating stator core positioned outside the cup and a rotating magnetic return path inside the cup, according to the present invention.
- FIG. 1B is a cross-sectional view of the permanent magnet accelerometer of FIG. 1A taken along lines A-A′.
- FIG. 2A is a partial side view of the second embodiment of the permanent magnet accelerometer with magnets positioned outside a rotating cup, a nonrotating stator core positioned outside the cup and a nonrotating magnetic return path inside the cup, according to the present invention.
- FIG. 2B is a cross-sectional view of the permanent magnet accelerometer of FIG. 2A taken along lines A-A′.
- FIG. 3A is a partial side view of the third embodiment of the permanent magnet accelerometer with magnets positioned inside a rotating cup, a nonrotating stator core positioned outside the cup and a nonrotating magnetic return path inside the cup, according to the present invention.
- FIG. 3B is a cross-sectional view of the permanent magnet accelerometer of FIG. 3A taken along lines A-A′.
- FIG. 4A is a partial side view of the forth embodiment of the permanent magnet accelerometer with magnets positioned inside a rotating cup, a nonrotating stator core positioned inside the cup and a nonrotating magnetic return path outside the cup that rotates according to the present invention.
- FIG. 4B is a cross-sectional view of the permanent magnet accelerometer of FIG. 4A taken along lines A-A′.
- FIG. 5A is a partial side view of the fifth embodiment of the permanent magnet accelerometer with magnets positioned outside the cup, a nonrotating stator core positioned inside the cup and a nonrotating magnetic return path outside the cup that is stationary according to the present invention.
- FIG. 5B is a cross-sectional view of the permanent magnet accelerometer of FIG. 1A taken along lines A-A′.
- FIG. 6A is a graph of an open loop stepper motor without using an accelerometer.
- FIG. 6B is a graph of an open loop stepper motor of FIG. 6A using the accelerometer according to the present invention.
- Overview of Mechanical Configuration for Housing
- Referring now in more detail to the drawings in which like numerals refer to like parts throughout several views FIG. 1A shows a partial side view of the first embodiment of the
permanent magnet accelerometer 100 and FIG. 1B is a cross-sectional view of the permanent magnet accelerometer of FIG. 1A taken along lines A-A′, according to the present invention. Ahousing 102 with anend bell 104 encloses the internal components ofaccelerometer 100. Amechanical input shaft 106 is coupled to a motor (not shown), such as a electrical, pneumatic, hydraulic, combustion orequivalent, rotating machine. One example of an electrical rotating machine is a stepper motor. A plurality ofbearings 108, such as roller, needle, ball bearings or equivalent, are used to reduce the friction ofinput shaft 106 turning inhousing 102. Astator core 110 forms an integral return path withpickup members 112. Thestator core 110 senses the change in eddy currents induced in an electricallyconductive cup 120 as further described below. It is important to note that thestator core 110 is formed out of magnetic permeable material, such as silicon iron orHyperco 50, for example. All of thestator core 110 including the integral return path withpickup members 112 are formed from one continuous piece of material. This single piece design ofstator core 110 provides lower reluctance, higher output voltages and increased sensitivity to the eddy currents induced in thecup 120. In one embodiment, thestator core 110 is machined from one piece of magnetically permeable material. In another embodiment, the stator core is a laminate or of sintered construction, where two or more layers of magnetically permeable material are sandwiched together. At least one layer is one piece that forms a low reluctance path between thepickup members 112. In addition, the single piece design ofstator core 110 is very rugged and can operate effectively in harsh environments, such as aerospace, where theaccelerometer 100 is subjected to a wide range of temperature fluctuations, constant shock and vibration, and large gravitational forces.Stator windings 114 are wound around or embedded in thestator core 110 nearpickup members 112.Electrical output wires 116, provide a signal from thestator windings 114 which is proportional to the eddy currents induced in thecup 120 rotating in a magnetic field formed betweenmagnets 118. - The complementary components of
housing 102,mechanical input shaft 106,end bell 104 andbearings 108, are only one of many mechanical adaptations to theaccelerometer 100 according to the present invention and several other configurations of these complementary components are possible to provide the proper alignment of these components with the components that are discussed in FIG. 1B. - Next several alternative embodiments are described and shown for various configurations of four components of the
accelerometer 100 according to the present invention. The four components whose configuration changes in the various embodiments are as follows: (i) nonrotating permanent magnets; (ii) a nonrotating stator core; (iii) a rotating electrically conductive cup; and (iv) a rotating or nonrotating (depending on the configuration) magnetically permeable return path. Five different embodiments are described for various configurations of these four components. The first configuration is used to provide a brief overview of the magnetic theory and the measured results. The basic mechanical configurations for thehousing 102,mechanical input shaft 106,end bell 104,bearings 108, the construction ofstator core 110 andstator windings 114,permanent magnets 118 andcup 120 is similar in all rest of embodiments described below. In other words, FIGS. 2A, 3A, 4A and 5A have similar construction for these components. - First Embodiment of Accelerometer Components
- One or more pairs of nonrotating
permanent magnets 116 are positioned outside the electrically conductiverotating cup 120. Thecup 120 is mounted onshaft 108 and is made out of any material, such as copper, that has low electrical resistance but high magnetic reluctance. A magneticallypermeable return path 122 is disposed onshaft 106. In one embodiment, the magneticallypermeable return path 122 and theshaft 106 are formed from a single piece of magnetically permeable material. In another embodiment, the magneticallypermeable return path 122 is a separate price of magnetically permeable material attached toshaft 106. The pair ofpermanent magnets 116, with opposite magnet polarity, form a magnetic field (not shown) through the cup into the magnetic return path. Thecup 120 mounted oninput shaft 108 rotates through the magnetic field formed bymagnets 118 and induces eddy currents within thecup 120 under principals know in the art, such as Faraday's and Maxwell's Laws. The eddy currents formed in thecup 120 are proportional to the angular acceleration at which thecup 120 moves through the magnetic field. Thepickup members 112 ofstator core 110 sense the magnitude of the secondary magnetic field generated by the eddy currents that form in thecup 120. The word “secondary” magnetic field is used to distinguish from the magnetic field produced by the permanent magnets. A signal is produced by thestator windings 114 on towire 114 directly proportional to the eddy currents. It should be understood that no D.C. excitation is needed with the permanent magnets so that the power requirements of prior art D.C. accelerometers are eliminated. - Turning now to FIG. 6, shown are two graphs that illustrate the performance enhancements realized with the accelerometer300 (as described below) according to the present invention. More specifically, FIG. 6A is a graph of an open loop stepper motor without using an
accelerometer 100. A C.D.A. Intercorp type 16-206-20 stepper motor coupled to a 100:1 gear head with a inertia factor of 38 is used. The Y-axes of the graph is in pulses per second and the X-axes are in units of Torque (lb.-in). FIG. 6B is a graph of the stepper motor of FIG. 6A using the accelerometer according to the present invention. It is important to note that the scale and the components of FIGS. 6A and 6B are identical. To those skilled in the art, a comparison of FIG. 6A with 6B illustrates several performance enhancements. The use of the accelerometer according to the present invention provides performance enhancements of higher torques and operating velocities. In addition, the accelerometer of the present invention has no “lost steps” and pulse by pulse information is provided. The resonance areas, or unstable performance are inherently nullified, and dynamic speed versus torque is realized. Those skilled in the art of stepper motor application will notice the performance enhancements of the response rate, 610, the pull intorque 612, and the torque atlow pulse rate 614, as compared with the FIG. 6A. - The
accelerometer 100 is an extremely useful component in high performance and/or high load inertia servo actuator systems. Since theaccelerometer 100 requires no excitation or demodulation, the DC output may be directly Op-Amp integrated for an angular rate damping signal of the motor. This information, along with the angular acceleration signal provides tremendous flexibility in contouring the system response, and controlling the transfer function. - The
accelerometer 100 can make the motor rotor inertia electronically “look” larger or smaller through this feedback technique. This electronic technique is like adding a variable electronic “flywheel” to the system, and provides a higher order effect, as compared to electronic damping through tachometer feedback. This may provide high forward loop gain, while maintaining a stable servo system. The electronic flywheel may be controlled to provide these characteristics dynamically in the system. Other advantages include acceleration control, and disturbance attenuation. - Second Embodiment of Accelerometer Components
- The second embodiment of an
accelerometer 200 is illustrated in FIGS. 2A and 2B. The components are numbered to correspond to the similar components of FIG. 1. For example permanent magnets are 218 where in FIG. 1, they are numbered 118, and housing in FIG. 2 is numbered 202 where the housing in FIG. 1 is numbered 102 and so on. The structural difference between the second embodiment and the first embodiment, is that like first embodiment, thecup 220 rotates, but themagnetic return path 222 inside thecup 220, unlike in the first embodiment, does not rotate. There is asmall air gap 224 formed between therotating cup 220 and the nonrotatingmagnetic return path 222. Only therotating cup 220 is coupled to themechanical input shaft 206. In addition, theend bell 204 may serve as an optional magnetic return path. This design ofaccelerometer 200 has lower rotating inertia as compared with the first embodiment because only thecup 220 and not the magneticallypermeable return path 222 rotates. - Third Embodiment of Accelerometer Components
- The third embodiment of an
accelerometer 300 is illustrated in FIG. 3A and 3B. The components are numbered to correspond to the similar components of FIG. 1. The structural difference between the third embodiment and the first embodiment, is that like first embodiment, thecup 320 rotates, but themagnetic return path 322 inside thecup 320, unlike in the first embodiment, does not rotate. There is asmall air gap 324 formed between therotating cup 320 and the nonrotatingmagnetic return path 322. Only therotating cup 320 is coupled to themechanical input shaft 306. Thepermanent magnets 318 have been moved to be positioned inside thecup 320. The permanent magnets are disposed on magneticallypermeable return path 322. In addition, theend bell 304 may serve as an optional magnetic return path. This design ofaccelerometer 300 has lower rotating inertia as compared with the first embodiment because only thecup 320 and not the magneticallypermeable return path 322 rotates. Because the magnets are positioned inside thecup 320, bonded ring magnets may be used forpermanent magnets 318. In addition, this design ofaccelerometer 300 exhibits some of the most rugged design characteristics for harsh environments and some of the highest output voltage as compared with other embodiments. - Fourth Embodiment of Accelerometer Components
- The fourth embodiment of an
accelerometer 400 is illustrated in FIGS. 4A and 4B. The components are numbered to correspond to the similar components of FIG. 1. The structural difference between the fourth embodiment and the first embodiment, is that like first embodiment, thecup 420 rotates, but all of the other components, unlike the first embodiment, all of the components, thestator core 410 including the integral return path withpickup members 412, thepermanent magnets 418, and thewindings 414 are all mounted inside therotating cup 420. The magneticpermeable return path 422 is outside therotating cup 420. In one embodiment is thehousing 402 serves as the magnetic permeable return path. And in another embodiment, the magneticpermeable return path 422 is a sleeve inside thehousing 402. This design ofaccelerometer 400 exhibits some of the lowest cost to manufacture because of the ease of construction. - Fifth Embodiment of Accelerometer Components
- The fifth embodiment of an
accelerometer 500 is illustrated in FIGS. 5A and 5B. The components are numbered to correspond to the similar components of FIG. 1. The structural difference between the fifth embodiment and the first embodiment, is that like first embodiment, thecup 520 rotates, but all of the other components, unlike the first embodiment, all of the components, thestator core 510 including the integral return path withpickup members 512, and thewindings 514 are all mounted inside therotating cup 520. The magnetic permeable return path 522 and the permanent magnets are outside therotating cup 520. In one embodiment is thehousing 502 serves as the magnetic permeable return path. And in another embodiment, the magnetic permeable return path 522 is a sleeve inside thehousing 502. This design ofaccelerometer 500 exhibits some of the lowest cost to manufacture because of the ease of construction. - Although a specific embodiment of the invention has been disclosed, it will be understood by those having skill in the art that changes can be made to this specific embodiment without departing from the spirit and scope of the invention. The scope of the invention is not to be restricted, therefore, to the specific embodiment, and it is intended that the appended claims cover any and all such applications, modifications, and embodiments within the scope of the present invention.
Claims (12)
1. A rotary accelerometer comprising: (FOR RA-001 and RA-002)
a cylindrical magnetic return path formed out of magnetic permeable material;
an electrically conductive cup with an axis for rotation there around, the cup surrounding the magnetic return path;
one or more sets of permanent magnets having opposite magnetic polarity, surrounding the cup, for a producing magnetic field through the cup into the magnetic return path, thereby inducing eddy currents inside the cup when rotating in the magnetic field;
a stator core formed out of magnetic permeable material surrounding the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and
one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
2. The rotary accelerometer of , further comprising a mechanical input shaft for coupling to a rotating machine and wherein the cup is dispose on magnetic return path, and the magnetic return path is coupled to the shaft and the cup and the magnetic return path rotates around the axis of the cup with the shaft.
claim 1
3. The rotary accelerometer of , further comprising a mechanical input shaft for coupling to a rotating machine and wherein the magnetic return path is nonrotatable and the cup surrounding the magnetic return path forms a gap therebetween to permit the cup to rotate with the shaft about the magnetic return path.
claim 1
4. The rotary accelerometer of , wherein the stator core is comprised of one or more layers of magnetic permeable materials laminated together so that at least one layer forms one continuous piece that includes the pickup members and stator core return path.
claim 1
5. The rotary accelerometer of , wherein the stator core includes one or more sets of mounts and where the one or more sets permanent magnets are held fixed on the mounts.
claim 1
6. The rotary accelerometer of , wherein the cup is coupled to a rotating electrical machine to provide a closed loop motion control therewith.
claim 1
7. The rotary accelerometer of , wherein the rotating electrical machine is a direct current stepper motor.
claim 1
8. The rotary accelerometer of , wherein the cup is coupled to a rotating pneumatic machine to provide a closed loop motion control therewith.
claim 1
9. The rotary accelerometer of , wherein the cup is coupled to a rotating combustion machine to provide a closed loop motion control therewith.
claim 1
10. A rotary accelerometer comprising: (FOR RA-003)
a nonrotatable cylindrical magnetic return path formed out of magnetic permeable material;
one or more permanent magnets, with two opposite magnetic poles, disposed around the magnetic return path;
an electrically conductive cup with an axis for rotation there around, the cup surrounding the permanent magnets and the permanent magnets are arranged so as to produce a magnetic field through the cup into magnetic return path thereby inducing eddy currents inside the cup when rotating in the magnetic field;
a stator core formed out of magnetic permeable material surrounding the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and
one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
11. A rotary accelerometer comprising: (FOR RA-004)
a nonrotatable cylindrical magnetic return path formed out of magnetic permeable material;
an electrically conductive cup rotatably mounted inside the magnetic return path;
one or more sets of permanent magnets having opposite magnetic polarity, mounted inside the cup, for a producing magnetic field through the cup into the magnetic return path, wherein eddy currents are induced inside the cup when rotating in the magnetic field;
a stator core formed out of magnetic permeable material mounted inside the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and
one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
12. A rotary accelerometer comprising: (FOR RA-005)
a nonrotatable cylindrical magnetic return path formed out of magnetic permeable material;
an electrically conductive cup rotatably mounted inside the magnetic return path;
one or more sets of permanent magnets having opposite magnetic polarity, mounted outside the cup, for a producing magnetic field through the cup into the magnetic return path, wherein eddy currents are induced inside the cup when rotating in the magnetic field;
a stator core formed out of magnetic permeable material mounted inside the cup and nonrotatable relative thereto, the stator core comprising at least two pick up members and a stator core return path therein, wherein the pick up members and the stator core return path are formed from at least one continuous piece of magnetic permeable material; and
one or more pickup coils disposed on the pickup members of the stator core for sensing changes in a secondary magnetic filed generated by the eddy currents in the cup.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/904,399 US6427534B2 (en) | 1999-09-24 | 2001-07-12 | Permanent magnet rotary accelerometer |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US09/405,876 US6282961B1 (en) | 1999-09-24 | 1999-09-24 | Permanent magnet rotary accelerometer |
US09/904,399 US6427534B2 (en) | 1999-09-24 | 2001-07-12 | Permanent magnet rotary accelerometer |
Related Parent Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/405,876 Continuation US6282961B1 (en) | 1999-09-24 | 1999-09-24 | Permanent magnet rotary accelerometer |
Publications (2)
Publication Number | Publication Date |
---|---|
US20010037684A1 true US20010037684A1 (en) | 2001-11-08 |
US6427534B2 US6427534B2 (en) | 2002-08-06 |
Family
ID=23605607
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/405,876 Expired - Fee Related US6282961B1 (en) | 1999-09-24 | 1999-09-24 | Permanent magnet rotary accelerometer |
US09/904,399 Expired - Fee Related US6427534B2 (en) | 1999-09-24 | 2001-07-12 | Permanent magnet rotary accelerometer |
Family Applications Before (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
US09/405,876 Expired - Fee Related US6282961B1 (en) | 1999-09-24 | 1999-09-24 | Permanent magnet rotary accelerometer |
Country Status (3)
Country | Link |
---|---|
US (2) | US6282961B1 (en) |
EP (1) | EP1145016A4 (en) |
WO (1) | WO2001023896A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
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CN104034916A (en) * | 2014-06-11 | 2014-09-10 | 杭州电子科技大学 | Permanent magnet rotation angle acceleration sensor with unequal magnetic resistance of direct axis and quadrature axis |
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US6992476B2 (en) * | 2001-05-11 | 2006-01-31 | Siemens Aktiengesellschaft | Transmitter system for a ferraris motion transmitter |
US7253609B2 (en) * | 2001-10-08 | 2007-08-07 | Dr. Johannes Heidenhain Gmbh | Encapsulated measuring apparatus for detecting a velocity and/or acceleration of a rotationally or linearly moved component |
US6997882B1 (en) | 2001-12-21 | 2006-02-14 | Barron Associates, Inc. | 6-DOF subject-monitoring device and method |
DE10219091A1 (en) * | 2002-04-29 | 2003-11-20 | Siemens Ag | Rotational movement detector comprises a hollow cylindrical induction element inside which are arranged an Eddy current excitation arrangement and an Eddy current sensor arrangement |
US7411388B2 (en) * | 2005-08-30 | 2008-08-12 | Baker Hughes Incorporated | Rotary position sensor and method for determining a position of a rotating body |
US7436096B2 (en) * | 2005-10-31 | 2008-10-14 | Caterpillar Inc. | Rotor having permanent magnets and axialy-extending channels |
US7436095B2 (en) * | 2005-10-31 | 2008-10-14 | Caterpillar Inc. | Rotary electric machine |
US7504754B2 (en) * | 2005-10-31 | 2009-03-17 | Caterpillar Inc. | Rotor having multiple permanent-magnet pieces in a cavity |
CN110542412B (en) * | 2019-08-12 | 2021-06-11 | 北京航天控制仪器研究所 | Self-adaptive dynamic and static closed-loop control method for nuclear magnetic resonance gyroscope |
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US2090521A (en) | 1934-05-02 | 1937-08-17 | Gen Electric | Accelerometer |
US2460115A (en) * | 1946-06-18 | 1949-01-25 | Gen Electric | Rotation rate change generator |
FR1232969A (en) * | 1959-03-03 | 1960-10-12 | Normacem Sa | Improvement in means of measuring angular accelerations |
US3178641A (en) | 1961-02-06 | 1965-04-13 | Gen Motors Corp | Drag cup tachometer accelerometer |
NL303019A (en) * | 1963-12-31 | 1965-10-25 | ||
DE1673443B2 (en) | 1968-02-17 | 1972-11-02 | Alfred Teves Gmbh, 6000 Fankfurt | ROTATION ACCELERATION MEASURING DEVICE |
US4207769A (en) | 1978-07-24 | 1980-06-17 | Hughes Aircraft Company | Change of angular acceleration sensor |
US4507607A (en) | 1982-06-10 | 1985-03-26 | Westinghouse Electric Corp. | Angular accelerometer |
US4678994A (en) | 1984-06-27 | 1987-07-07 | Digital Products Corporation | Methods and apparatus employing apparent resonant properties of thin conducting materials |
US4798378A (en) | 1985-07-15 | 1989-01-17 | Jones Robert S | Rowing machine |
US4984463A (en) | 1988-09-28 | 1991-01-15 | Nippon Soken, Inc. | Two-dimensional acceleration sensor |
US5311111A (en) | 1991-05-29 | 1994-05-10 | Orbotech Ltd. | Method of calibrating a step motor |
JPH05215764A (en) | 1992-01-31 | 1993-08-24 | Canon Inc | Optical accelerometer and optical angular accelerometer |
US5251484A (en) | 1992-04-03 | 1993-10-12 | Hewlett-Packard Company | Rotational accelerometer |
JPH06147815A (en) * | 1992-09-18 | 1994-05-27 | Nippondenso Co Ltd | Rotational angle sensor for internal-combustion engine |
US5521772A (en) | 1993-11-30 | 1996-05-28 | International Business Machines Corporation | Disk drive with accerleration rate sensing |
JPH08178938A (en) * | 1994-12-27 | 1996-07-12 | Nippon Seiko Kk | Rolling bearing unit with rotating speed detecting device |
US5967669A (en) * | 1996-10-11 | 1999-10-19 | Nsk Ltd. | Rolling bearing unit with rotational speed sensor |
US5939878A (en) * | 1997-04-25 | 1999-08-17 | Phoenixcloud Explorations Ltd. | Angular displacement transducer having flux-directing target and multi-sectored pole piece |
-
1999
- 1999-09-24 US US09/405,876 patent/US6282961B1/en not_active Expired - Fee Related
-
2000
- 2000-09-13 EP EP00961867A patent/EP1145016A4/en not_active Withdrawn
- 2000-09-13 WO PCT/US2000/025057 patent/WO2001023896A1/en not_active Application Discontinuation
-
2001
- 2001-07-12 US US09/904,399 patent/US6427534B2/en not_active Expired - Fee Related
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN104034916A (en) * | 2014-06-11 | 2014-09-10 | 杭州电子科技大学 | Permanent magnet rotation angle acceleration sensor with unequal magnetic resistance of direct axis and quadrature axis |
Also Published As
Publication number | Publication date |
---|---|
WO2001023896A1 (en) | 2001-04-05 |
US6427534B2 (en) | 2002-08-06 |
EP1145016A4 (en) | 2003-06-04 |
EP1145016A1 (en) | 2001-10-17 |
US6282961B1 (en) | 2001-09-04 |
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