GB174726A - Improvements in or relating to power-transmission and powerindicating couplings - Google Patents
Improvements in or relating to power-transmission and powerindicating couplingsInfo
- Publication number
- GB174726A GB174726A GB3075020A GB3075020A GB174726A GB 174726 A GB174726 A GB 174726A GB 3075020 A GB3075020 A GB 3075020A GB 3075020 A GB3075020 A GB 3075020A GB 174726 A GB174726 A GB 174726A
- Authority
- GB
- United Kingdom
- Prior art keywords
- fluid
- piston
- pressure
- screw
- angular relationship
- 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
- G01L—MEASURING FORCE, STRESS, TORQUE, WORK, MECHANICAL POWER, MECHANICAL EFFICIENCY, OR FLUID PRESSURE
- G01L3/00—Measuring torque, work, mechanical power, or mechanical efficiency, in general
- G01L3/02—Rotary-transmission dynamometers
- G01L3/14—Rotary-transmission dynamometers wherein the torque-transmitting element is other than a torsionally-flexible shaft
- G01L3/1464—Rotary-transmission dynamometers wherein the torque-transmitting element is other than a torsionally-flexible shaft involving screws and nuts, screw-gears or cams
Landscapes
- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Testing Of Devices, Machine Parts, Or Other Structures Thereof (AREA)
- Testing Of Engines (AREA)
Abstract
174,726. Bush, H. D., and Merton, H. Oct. 30, 1920. Shaft couplings.-In means for indicating or producing, by fluid pressure, a variation in angular relationship between two aligned rotary members, the fluid-pressure device is in the form of a non-rotating annular piston and cylinder in endthrust engagement with the two rotary members, which directly engage one another by screwthreads. When used as a torque-dynamometer, the engine to be tested is coupled, for example by rods sliding in orifices 14, to the rotary member 4 engaging by 45‹ screw-threads 5 a shaft 1, to which is keyed the other member 2, similarly coupled bv sliding rods to a calibrated air-screw or other brake. The parts 2, 4 thrust respectively by antifriction bearings 9, 10 against an annular chamber and piston 7. The chamber 6 is filled through an orifice 12 with fluid, such as thin lubricating-oil, and is fitted with a pressure-gauge 11, which may be graduated to give torque readings directly. The apparatus may be put out of action by screwing up a nut 15. Means may be provided for varying the quantity of fluid in order to change the angular relationship of the parts 2, 4, in which case the piston may be doubleacting, so that motion is positive in both directions.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3075020A GB174726A (en) | 1920-10-30 | 1920-10-30 | Improvements in or relating to power-transmission and powerindicating couplings |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3075020A GB174726A (en) | 1920-10-30 | 1920-10-30 | Improvements in or relating to power-transmission and powerindicating couplings |
Publications (1)
Publication Number | Publication Date |
---|---|
GB174726A true GB174726A (en) | 1922-01-30 |
Family
ID=10312542
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3075020A Expired GB174726A (en) | 1920-10-30 | 1920-10-30 | Improvements in or relating to power-transmission and powerindicating couplings |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB174726A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2444363A (en) * | 1944-08-30 | 1948-06-29 | United Aircraft Corp | Helical spline torque indicator |
US2603107A (en) * | 1949-05-21 | 1952-07-15 | United Aircraft Corp | Reduction gearing |
US3581562A (en) * | 1969-04-28 | 1971-06-01 | Allspeeds Holdings Ltd | Torque-sensing devices |
-
1920
- 1920-10-30 GB GB3075020A patent/GB174726A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2444363A (en) * | 1944-08-30 | 1948-06-29 | United Aircraft Corp | Helical spline torque indicator |
US2603107A (en) * | 1949-05-21 | 1952-07-15 | United Aircraft Corp | Reduction gearing |
US3581562A (en) * | 1969-04-28 | 1971-06-01 | Allspeeds Holdings Ltd | Torque-sensing devices |
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