Self-calibrating torque measuring system
AssigneeAvco Corporation
InventorsStanley Janik, Kimball J. Rumford, Timothy Warner
Life of this patent
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AssigneeAvco Corporation
InventorsStanley Janik, Kimball J. Rumford, Timothy Warner
Estimating the term…
A universal torque measuring system for hollow drive shafts which automatically compensates for variations in wall thickness exhibited by different drive shafts having the same nominal dimensions. During a calibration procedure, the drive shaft is subjected to a first predetermined torque which causes a certain amount of twist dependent upon its wall thickness. At this time, target indicia are positioned and affixed to the drive shaft to produce an initial phase shift relative to indicia on a reference shaft. Thereafter, when the drive shaft is incorporated into an engine and rotated under load subjecting it to a second predetermined torque less than the first predetermined torque, there is a resulting second phase shift. This second phase shift and the second predetermined torque define a second operating condition of the drive shaft. In turn, the first and second operating conditions define a characteristic relationship between torque and phase shift for the drive shaft. A sensor is positioned to detect deviations in phase shift of the first and second target teeth from the initial phase shift and generates a signal proportional to such deviations. A microprocessor is responsive to the signal from the sensor for automatically deriving a value of torque being experienced by the drive shaft as a function of each such deviation according to the characteristic relationship.
A universal torque measuring system for hollow drive shafts which automatically compensates for variations in wall thickness exhibited by different drive shafts having the same nominal dimensions comprising:
In combination with a power plant having an output shaft, a universal torque measuring system for hollow drive shafts which automatically compensates variations in wall thickness exhibited by different drive shafts having the same nominal dimensions comprising:
A universal method of measuring torque sustained by hollow drive shafts which automatically compensates for variations in wall thickness exhibited by different drive shafts having the same nominal dimensions comprising the steps of:
Dependencies are inferred from the claim text.
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No related US applications are recorded in the indexed filing history.
Testing or calibrating of apparatus for measuring force, torque, work, mechanical power, or mechanical efficiency: for measuring torque
Involving electric or magnetic means for indicating: involving magnetic or electromagnetic means
Involving electric or magnetic means for indicating: involving measuring phase difference of two signals or pulse trains
Measuring force, stress, torque, work, mechanical power, mechanical efficiency, or fluid pressure
Term ended 4 May 2008 (estimated)
USPTO file history isn’t available for this patent, so only indexed dates are shown.
1. Field of the Invention
The present invention relates generally to a system including method and apparatus for measuring the torque transmitted by a shaft and, in particular, a system which automatically compensates for variations in wall thickness exhibited by different drive shafts having the same nominal dimensions.
2. Description of the Prior Art
FIG. 1 is a detail side elevation view, certain parts cut away and shown in section, of a gas turbine engine which incorporates a drive shaft embodying the present invention;
FIG. 2 is a longitudinal cross section view of the novel drive shaft illustrated in FIG. 1;
FIGS. 3 and 4 are detail cross section views of components illustrated in FIG. 2;
Turn now to the drawings and initially to FIG. 1 which illustrates portions of a gas turbine engine 20 which utilizes a universal torque measuring system in accordance with the invention. While the engine 20 is illustrated as being a gas turbine engine, indeed, it may be any form of prime mover. That is, the benefits and advantages of the invention are of a universal nature and need not be restricted to gas turbine engines.
Returning now to FIG. 1, in customary fashion the gas turbine engine 20 has a turbine at the aft end (not shown) with a drive shaft 30. A mounting flange 28 at an extreme end of the drive shaft 30 is attached to a similar mounting flange 26 provided at an extreme end of an output shaft 24 and the flanges 26, 28 are firmly joined by means of a plurality of mounting bolts 32 such that the shafts 24 and 30 are aligned and coaxial. When the engine 20 is in operation, it is desirable and even necessary for the operator of the engine, or the pilot in the event the engine powers an aircraft, to know the magnitude of the torque being transmitted by the drive shaft 30 at all times.
It is conventional practice, before incorporating the drive shaft 30 into the engine 20 to perform a calibration operation on the shaft. This calibration operation is performed in order to make compensation between thin walled shafts and thick walled shafts since, as previously mentioned, thin walled shafts are caused to twist to a greater extent under a given torque load than are thick walled shafts. However, also as previously mentioned, the calibration operation performed in accordance with the invention does not require the use of any additional component separate from the drive shaft which must accompany it in transit from a fabrication location to a location at which it is being installed into a particular engine. Nor does the drive shaft require any specialized machining procedures of the type noted with respect to U.S. Pat. No. 4,602,515.