GB612357A - Improvements in and relating to apparatus for balancing rotors - Google Patents
Improvements in and relating to apparatus for balancing rotorsInfo
- Publication number
- GB612357A GB612357A GB15213/46A GB1521346A GB612357A GB 612357 A GB612357 A GB 612357A GB 15213/46 A GB15213/46 A GB 15213/46A GB 1521346 A GB1521346 A GB 1521346A GB 612357 A GB612357 A GB 612357A
- Authority
- GB
- United Kingdom
- Prior art keywords
- rotor
- voltages
- wattmeter
- switch
- phase
- 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
- G01M—TESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
- G01M1/00—Testing static or dynamic balance of machines or structures
- G01M1/14—Determining imbalance
- G01M1/16—Determining imbalance by oscillating or rotating the body to be tested
- G01M1/22—Determining imbalance by oscillating or rotating the body to be tested and converting vibrations due to imbalance into electric variables
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Balance (AREA)
- Measurement Of Mechanical Vibrations Or Ultrasonic Waves (AREA)
Abstract
612,357. Electric indicating systems. BRITISH THOMSON-HOUSTON CO., Ltd. May 20, 1946, No. 15213. Convention date, May 23, 1945. [Class 40 (i)] [Also in Group XX] An indication of the out-of-balance of a rotor, e.g. of a gyroscope, is given by the resultant of two voltages induced in series connected coils due to the vibration of the two ends of a freely-supported stator surrounding the rotor, the coils being connected to a reversing switch. As shown, the rotor is surrounded by a stator (not shown), supported on a spring or springs and having secured at each end thereof a downwardly-extending flexible rod carrying a coil 20, 21, each arranged for movement between a pair of permanent magnets. If the unbalance is on the central vertical axis of the rotor, a simple vertical vibration will'result and the voltages will be equal being 180 degrees out of phase and the resultant zero when switch 26 is thrown right. If there is a pair of equal and symmetrically spaced out-ofbalance points away from the central axis, there will be a tilting tendency, but the voltages will still be equal, the zero resultant however occurring when the switch 26 is left. Generally, both such conditions will occur and the magnitude of each component (but not the position) will be proportional to the voltages with the switch in the two positions, and these voltages are applied in turn to the wattmeter 37 through an attenuator 41, filter 42 and amplifier 43. It is assumed that a voltage so obtained is displaced by an angle # from a voltage A derived from a photo cell 36 receiving light from a lamp 35 deflected by a patch 33 on the rotor, this voltage being converted to one of constant sine wave form by a device 38, and the wattmeter reading will be proportional to A, B, Cos # from which the magnitude of the out-of-balance can be ascertained if a reading is taken with the phase adjuster turned to give maximum wattmeter reading, signifying Cos # equals unity. If the phase.adjuster is then turned until the wattmeter reads zero, the phase angle between the voltages will be 90 degrees, and the angle of turn of the phase shifter to achieve this will give the angle 34 between the patch 33 and the out-of-balance position 32 on a scale previously calibrated by using a known mass in known positions on the rotor. The operation is repeated with the switch 26 thrown the other way to measure the out-of-balance producing a tilting effect as distinct from the purely vertical vibrations. The apparatus may be adapted for an oscillograph instead of a wattmeter.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US612357XA | 1945-05-23 | 1945-05-23 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB612357A true GB612357A (en) | 1948-11-11 |
Family
ID=22034506
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB15213/46A Expired GB612357A (en) | 1945-05-23 | 1946-05-20 | Improvements in and relating to apparatus for balancing rotors |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB612357A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3044304A (en) * | 1953-06-24 | 1962-07-17 | M Ten Bosch Inc | Rotor balancer |
US3130587A (en) * | 1961-02-23 | 1964-04-28 | Gen Motors Corp | Unbalance measuring apparatus |
CN102519672A (en) * | 2011-12-26 | 2012-06-27 | 北京航空航天大学 | Monocular-principle-based six-degree-of-freedom position and attitude measuring device for measuring static balance of gyroscope |
-
1946
- 1946-05-20 GB GB15213/46A patent/GB612357A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3044304A (en) * | 1953-06-24 | 1962-07-17 | M Ten Bosch Inc | Rotor balancer |
US3130587A (en) * | 1961-02-23 | 1964-04-28 | Gen Motors Corp | Unbalance measuring apparatus |
CN102519672A (en) * | 2011-12-26 | 2012-06-27 | 北京航空航天大学 | Monocular-principle-based six-degree-of-freedom position and attitude measuring device for measuring static balance of gyroscope |
CN102519672B (en) * | 2011-12-26 | 2013-11-27 | 北京航空航天大学 | Monocular-principle-based six-degree-of-freedom position and attitude measuring device for measuring static balance of gyroscope |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2451863A (en) | Apparatus for balancing rotors | |
US2131602A (en) | Dynamically balancing rotatable body | |
US2783648A (en) | Apparatus for determining dynamic unbalance | |
US2331617A (en) | Magnetic field responsive device | |
US3835712A (en) | Wheel balancing apparatus | |
GB555992A (en) | An improved apparatus for balancing rotating bodies such as aeroplane propellers | |
GB612357A (en) | Improvements in and relating to apparatus for balancing rotors | |
US2616289A (en) | Apparatus for dynamically balancing rotating elements | |
US2050073A (en) | Apparatus for dynamically balancing rotatable bodies | |
GB642916A (en) | An improved apparatus for testing the balance of rotating bodies | |
US2678558A (en) | Balancing machine with electrical indicating device | |
US2724971A (en) | Vibration detecting apparatus | |
US2493376A (en) | Magnetically biased indicating instrument | |
US2871693A (en) | Device for calibrating indicators of torsional oscillations during rotation | |
US1933327A (en) | Electrical instrument | |
US2966801A (en) | Device for central control of a wattmetric balancing system | |
US3618367A (en) | Vibration pick-up device | |
US2828626A (en) | Dynamic balance system | |
US1652502A (en) | Balancing machine | |
US3623374A (en) | Vibration analyzing apparatus | |
US3332290A (en) | Accelerometer | |
SU821916A1 (en) | Apparatus for determining object slope angles | |
US1612329A (en) | Indicating device for small balancing machines | |
SU127747A1 (en) | Oscilloscope vibrator | |
US3422668A (en) | Device for measuring mechanical vibration |