WO2009141261A1 - Dispositif de mesure de couple transmis par un arbre de puissance - Google Patents
Dispositif de mesure de couple transmis par un arbre de puissance Download PDFInfo
- Publication number
- WO2009141261A1 WO2009141261A1 PCT/EP2009/055818 EP2009055818W WO2009141261A1 WO 2009141261 A1 WO2009141261 A1 WO 2009141261A1 EP 2009055818 W EP2009055818 W EP 2009055818W WO 2009141261 A1 WO2009141261 A1 WO 2009141261A1
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- power shaft
- series
- teeth
- wheel
- angular
- Prior art date
Links
- 230000004048 modification Effects 0.000 description 4
- 238000012986 modification Methods 0.000 description 4
- 238000005259 measurement Methods 0.000 description 3
- 230000005540 biological transmission Effects 0.000 description 2
- 238000000926 separation method Methods 0.000 description 1
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
- G01L3/04—Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft
- G01L3/10—Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating
- G01L3/101—Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving magnetic or electromagnetic means
-
- 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
- G01L3/04—Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft
- G01L3/10—Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating
- G01L3/109—Rotary-transmission dynamometers wherein the torque-transmitting element comprises a torsionally-flexible shaft involving electric or magnetic means for indicating involving measuring phase difference of two signals or pulse trains
Definitions
- Torque measuring device transmitted by a power shaft
- the present invention relates to devices for measuring the torque transmitted by a shaft of an engine, such as for example a shaft of a turbomachine of an aircraft.
- the present invention is directed to a device based on such a measure of torsional deformation of the shaft.
- the invention relates to a torque measuring device comprising: - a power shaft for transmitting a torque around an axis of the power shaft;
- a reference shaft having a first end attached to one end of the power shaft and a second free end provided with a second wheel bearing angular marks which is concentric with the first sound wheel, a sensor arranged opposite at least one of said wheels capable of supplying a signal representative of an angular variation between the first and second wheels, said signal being intended to be transmitted to a calculation unit able to determine the torque transmitted by the power shaft to from the signal provided by the sensor.
- Such a measuring device is shown in FIG. 1 of document FR 2 595 821.
- the magnetic sensors arranged facing the teeth of the tone wheels make it possible to detect an angular variation between the tone wheels, following which the computation member determines the torsional deformation of the power shaft and then derives the torque.
- the torsional stiffness of the power shaft is related to the Young's modulus value of the material constituting the shaft, and the value of this module is a function of temperature. In other words, it is necessary to take into account the temperature of the power shaft in the calculation of the torque, otherwise the value obtained is significantly erroneous.
- FR 2 595 821 envisages the use of additional sensors for measuring the longitudinal expansion of the power shaft relative to the reference shaft and, to deduce the temperature therefrom.
- the measuring device FR 2 595 821 is therefore complex to produce and bulky insofar as it comprises several magnetic sensors.
- An object of the present invention is to provide a torque measurement device transmitted by a power shaft which requires fewer components and, consequently, has reduced bulk, weight and cost.
- the invention achieves its goal by the fact that: the first wheel comprises first and second sets of angular marks; and
- the second wheel comprises third and fourth sets of angular marks, the marks of the first and third series being parallel to each other, while the marks of the second and fourth series are parallel to each other while being inclined with respect to a first axial plane; containing the axis of the power shaft, the marks of the first series being inclined relative to the marks of the second series; whereby the signal supplied by said sensor is also representative of the temperature of the power shaft.
- the first and second wheels are phonic wheels, and the angular marks of the first, second, third and fourth series consist of teeth.
- An advantage of the present invention is that it requires only one sensor while the devices of the prior art require several sensors to obtain a torque value taking into account the temperature of the shaft.
- the magnetic sensor detects the passage of teeth belonging to each series of teeth of the tone wheels.
- the representative signal generated by the magnetic sensor therefore constitutes a signal train where, schematically, each "peak" corresponds to a tooth.
- the computation unit is programmed so that it is able to recognize to which tooth is associated each of the peaks of the signal.
- the signal train transmitted by the sensor thus makes it possible to determine a first angular difference between a tooth of the first series and a tooth of the third series, as well as a second angular difference between a tooth of the second series and a tooth of the second series. fourth series, these angular differences being able to be determined from the duration between two successive peaks.
- Each of the first and second angular deviation variations contains the torsion deformation information and, moreover, at least one of the determined variations further comprises temperature information.
- the teeth of the second and fourth series of parallel teeth are inclined relative to the first axial plane containing the axis of the power shaft, the axial thermal expansion of the power shaft relative to the The reference axis results in a modification of the angular difference between two teeth of these two series, which modification is representative of the temperature.
- the modification of the angular deviation due to the temperature is added to the variation of the angular difference due to the torsional deformation of the shaft resulting from the transmission of the torque.
- Knowing the angle of inclination of the teeth it is possible, from the first and second variations of angular deviations, to determine the angular variation resulting solely from the torsion of the power shaft on the one hand, and that resulting of the axial distance between the two shafts due to the expansion, it is therefore from this variation resulting from the axial separation that the temperature is determined.
- the temperature and the angular deviation variation due to the torsional deformation are then sent to the computation unit which, from a prerecorded abacus, is able to calculate the value of the torque actually transmitted by the power shaft. .
- a series of teeth may comprise one or, preferably, several teeth.
- the first and second tone wheels are arranged so that the teeth of the first tone wheel alternate angularly with the teeth of the second tone wheel.
- the computing unit is advantageously programmed so as to know this particular sequence.
- the teeth of the first and third series are parallel to the axis of the power shaft.
- the teeth of the first and third series extend in an axial plane
- the teeth of the second and fourth series extend in a plane inclined relative to the first axial plane. Since the teeth of the first and third series are parallel to the axis of the power shaft, the first angular difference variation is representative only of the torsional deformation of the power shaft. Indeed, the axial spacing due to the expansion does not change the angular difference between two teeth parallel to the axis.
- the second angular difference variation is constituted by the angular variation resulting from the torsional deformation as well as by the angular modification due to the axial expansion.
- the temperature and the angular variation resulting from the torsional deformation are sent to the computation unit which then determines the value of the torque actually transmitted by the power shaft.
- the teeth of the first and third series are inclined with respect to a second axial plane containing the axis of the spindle. power of a predetermined angle, while the teeth of the second and fourth series are inclined relative to the first axial plane by an angle opposite said predetermined angle.
- the first and second angular deviation variations both contain information relating to the temperature and torsional deformation of the power shaft.
- the angles of inclination of the first and third series on the one hand, and second and fourth series on the other hand are opposite, the half-sum and the half-difference of the first and second series provide the temperature and the angular variation. sought.
- the reference shaft preferably extends axially inside the power shaft.
- the series of teeth are arranged angularly along a portion of the circumference of their respective tone wheels.
- the present invention finally relates to a turbomachine comprising a device for measuring the torque transmitted by a power shaft according to any one of the claims
- FIG. 1 shows a helicopter turbine engine equipped with a torque measuring device according to the invention
- FIG. 2 is a half-view in axial section of a measuring device according to the invention
- Fig. 2A is a detail of Fig. 1 showing an opening in the power shaft through which a tooth of the second tone wheel extends
- FIG. 2B is an axial half-view of a variant of the device of FIG. 2, in which the reference shaft extends outside the power shaft;
- FIG. 3 is a radial sectional view showing the relative position of the teeth of the first and second tone wheels
- FIG. 4A shows the relative position of the teeth of the first and second tone wheels of a first embodiment of the invention, considered in an orthoradial direction of the tone wheels, when the power shaft is at rest;
- FIG. 4B shows the relative position of the teeth of the first and second tone wheels of FIG. 4 when the power shaft transmits a torque
- - SA shows the relative position of the teeth of the first and second tone wheels of a second embodiment of the invention, considered in an orthoradial direction of the tone wheels, when the power shaft does not transmit torque
- - Figure SB shows the relative position of the teeth of the first and second sound wheels of Figure SA when the power shaft transmits a torque.
- the torque measuring device according to the present invention also called torsion torque meter, can be used in many situations where one seeks to know the torque transmitted by a shaft.
- the measuring device is described in the particular but non-exclusive example of the helicopter turbines, such as the gas turbine 9 shown in FIG. 1.
- the torque measuring device 10 according to FIG. The invention, shown in Figure 1, is in the general form of a shaft portion whose ends are intended to be coupled to other shafts or gears of the turbine engine.
- the torque measuring device 10 comprises a hollow power shaft 12 for transmitting the rotational torque about its axis A. It is this torque that one seeks to measure.
- the power shaft 12 comprises a pinion 14 at its first end 12a, and a drive member 16 disposed at its second end 12b opposite the first end.
- a pinion 14 at its first end 12a
- a drive member 16 disposed at its second end 12b opposite the first end.
- the power shaft 12 carries, near its second end 12b, a first wheel 18 in this case a coaxial voice wheel 18 comprising a plurality of angular references, in this case teeth 19.
- the measuring device further comprises a reference shaft 20 extending axially inside the power shaft 12 to which it is fixed by its first end 20a close to the first end. 12a of the power shaft 12, while its second end 20b is free.
- FIG. 2B shows an alternative configuration of the measuring device in which the reference shaft 20 'extends axially outside the power shaft 12' to which it is fixed by its first end 20a 1 adjacent to the first end 12a 'of the power shaft 12', while its second end 20b 'is free.
- the second end 20b of the reference shaft 20 opposite its first end 20a, carries a second wheel, in this case of the phonic type 22, which is concentric with the first phonic wheel 18.
- the second phonic wheel 22 carries a plurality of angular markers, in this case teeth 23 which, as best seen in FIG. 2A, extend radially through openings 24 formed in FIG. power shaft 20.
- a single magnetic sensor 26 Opposite the teeth of the first and second tone wheels 18, 22 is a single magnetic sensor 26 which is able to generate an electrical signal at each passage of a tooth in front of it, which signal is then sent to a computation unit 28 for determining the value of the torque transmitted by the power shaft 12.
- FIG. 3 illustrates the angular distribution of the teeth of the first and second tone wheels 18, 22.
- the white teeth belong to the first voice wheel 18, while the black teeth belong to the second voice wheel 22.
- the first voice wheel 18 comprises a first series of teeth D1 identical to each other and a second series of teeth D2 identical to each other, while the second voice wheel 22 comprises a third series of teeth D3 identical to each other and a fourth series of teeth D4 identical to each other.
- the first and second tone wheels are arranged so that the teeth D1, D2 of the first phonic wheel 18 alternate angularly with the teeth D3, D4 of the second phonic wheel 22.
- each series of teeth comprises two teeth. More precisely, considered according to the orthoradial direction OR of the power shaft 12, as represented in FIGS. 4A to 5B, follow successively, a tooth D1 of the first series, a tooth D3 of the third series, a tooth D2 of the second series and finally a tooth D4 of the fourth series.
- the teeth D1 and D3 belonging respectively to in the first and third series of teeth have a first known angular difference Xo
- the teeth D2 and D4 respectively belonging to the second and fourth series of teeth have a second angular difference y 0 also known.
- the power shaft 12 transmits a torque, it tends to deform in torsion, to a greater or lesser extent depending on the intensity of the torque transmitted on the one hand, and the temperature of the power shaft. 'somewhere else.
- FIGS. 4A and 4B a first embodiment of the invention will now be described. These figures are considered in a orthoradial OR direction of the tone wheels. They thus schematize the relative positions of the teeth as if the circumference of the phonic wheels was a straight line.
- the teeth D1 and D3 of the first and third series are parallel to each other, while the teeth D2 and D4 of the second and fourth series are parallel to each other while being inclined with respect to a first axial plane ( ) containing the axis A of the power shaft 12, the teeth D1 of the first series being inclined relative to the teeth D2 of the second series.
- the teeth D1 and D3 of the first and third series are parallel to the axis A of the power shaft 12, that is to say extend in two axial planes while the teeth D2 and D4 of the second and fourth series are inclined at an angle ⁇ relative to the first axial plane P1.
- each of the teeth D2 and D4 extends in a plane that makes an angle ⁇ relative to the first axial plane P1.
- FIG. 4A represents the relative position of the teeth D1, D2, D3 and D4 at rest, when no torque is transmitted by the power shaft 12.
- the first angular difference is then equal to X 0
- the second angular difference is yo.
- FIG. 4B represents the relative position of these same teeth when the power shaft transmits a torque, it being specified that at this moment, the power shaft 12 is at temperature T.
- the power shaft 12 has moved axially away from the reference shaft 20 due to the differential thermal expansion phenomenon due to the increase in the engine temperature and the respective expansion coefficients of the shafts.
- the second angular difference variation ⁇ y is equal to the first angular difference variation ⁇ x added to an angular expansion variation ⁇ z corresponding solely to the thermal expansion.
- This last value of variation is proportional to the axial expansion difference illustrated by reference d.
- the angular expansion variation ⁇ z is therefore a function of the temperature T of the power shaft, since the axial expansion d is itself a function of the temperature.
- the first variation of angular difference ⁇ x only measures the angular deformation between the two tone wheels 18, 22 insofar as the teeth of the first and third series are parallel to the direction of axial deformation by expansion, the expansion n ' not affecting the angular variation between teeth D1 and D3.
- the magnetic sensor 26 which generates signal trains sends this information to the computing unit 28 which is able to discriminate the different signals and to calculate the first and second angular difference variations.
- the angular expansion variation ⁇ z is obtained from which the temperature T. is deduced.
- the computing unit 28 determines the value of the torque transmitted by the power shaft 12 from the calculated temperature T and the first angular difference variation ⁇ x corresponding to the torsional deformation between the two tone wheels, using a previously recorded chart.
- Said abacus can take the form of a database containing torque values depending on the temperature and angular deviation variation. It can be done beforehand in a workshop.
- FIGS. 5A and 5B illustrate a second embodiment which differs from the first in that the teeth D1, D3 of the first and third series of teeth are not parallel to the axis A of the power shaft 12 but inclined by an angle ⁇ with respect to a second axial plane P2 which contains the axis A of the power shaft 12. The angle ⁇ is therefore opposite the inclination angle ⁇ 'of the teeth D2, D4 of the second and fourth series of teeth.
- FIG. 5A shows the relative position of the teeth D1, D2, D3 and D4 when no torque is transmitted by the power shaft 12.
- the first angular difference is then Xo, while the second angular difference is yo.
- FIG. 5B represents the relative position of these same teeth when the power shaft transmits a torque, it being specified that at this moment, the power shaft 12 is at the temperature T.
- the first and second angular difference variations ⁇ x and ⁇ y are each equal to the angular variation between the two tone wheels added with an angular difference component due to the expansion. Since the pairs of teeth D1, D3 and D2, D4 are inclined at opposite angles, it follows that the angular deviation components due to the expansion contained in the first and second angular difference variations are opposite, both so that by adding the first and second variations of angular difference one obtains twice the angular deformation between the two tone wheels, while by subtracting the first and second angular difference variations one obtains twice the component angular deviation due to the expansion from which the temperature is deduced T.
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- Physics & Mathematics (AREA)
- General Physics & Mathematics (AREA)
- Electromagnetism (AREA)
- Force Measurement Appropriate To Specific Purposes (AREA)
Abstract
Description
Claims
Priority Applications (7)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN200980118180.0A CN102037339B (zh) | 2008-05-21 | 2009-05-14 | 一种测量动力轴传递的扭矩的装置 |
KR1020107026937A KR101604147B1 (ko) | 2008-05-21 | 2009-05-14 | 파워 샤프트에서 전달된 토크를 측정하기 위한 장치 |
JP2011509930A JP5579702B2 (ja) | 2008-05-21 | 2009-05-14 | パワーシャフトにより伝達されるトルクを測定する装置 |
US12/990,947 US8464598B2 (en) | 2008-05-21 | 2009-05-14 | Device for measuring the torque transmitted by a power shaft |
EP09749751A EP2288890A1 (fr) | 2008-05-21 | 2009-05-14 | Dispositif de mesure de couple transmis par un arbre de puissance |
CA2725101A CA2725101A1 (fr) | 2008-05-21 | 2009-05-14 | Dispositif de mesure de couple transmis par un arbre de puissance |
RU2010152245/28A RU2497087C2 (ru) | 2008-05-21 | 2009-05-14 | Устройство для измерения крутящего момента, передаваемого валом отбора мощности |
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0853295 | 2008-05-21 | ||
FR0853295A FR2931552B1 (fr) | 2008-05-21 | 2008-05-21 | Dispositif de mesure de couple transmis par un arbre de puissance |
Publications (1)
Publication Number | Publication Date |
---|---|
WO2009141261A1 true WO2009141261A1 (fr) | 2009-11-26 |
Family
ID=40225404
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2009/055818 WO2009141261A1 (fr) | 2008-05-21 | 2009-05-14 | Dispositif de mesure de couple transmis par un arbre de puissance |
Country Status (9)
Country | Link |
---|---|
US (1) | US8464598B2 (fr) |
EP (1) | EP2288890A1 (fr) |
JP (1) | JP5579702B2 (fr) |
KR (1) | KR101604147B1 (fr) |
CN (1) | CN102037339B (fr) |
CA (1) | CA2725101A1 (fr) |
FR (1) | FR2931552B1 (fr) |
RU (1) | RU2497087C2 (fr) |
WO (1) | WO2009141261A1 (fr) |
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2972256A1 (fr) * | 2011-03-02 | 2012-09-07 | Turbomeca | Procede de calibration d'un couplemetre a torsion |
JP2013530348A (ja) * | 2010-07-02 | 2013-07-25 | ターボメカ | トルク計を用いた測定によるフリータービンの過速度の検出 |
WO2014013160A1 (fr) | 2012-07-18 | 2014-01-23 | Centre Technique Des Industries Mecaniques | Dispositif de mesure d'un couple transmis par un arbre de transmission de puissance avec prise en compte des variations de température |
WO2015082835A1 (fr) | 2013-12-03 | 2015-06-11 | Snecma | Dispositif de mesure de couple pour arbre de turbomachine |
RU2766620C1 (ru) * | 2021-03-11 | 2022-03-15 | федеральное государственное автономное образовательное учреждение высшего образования "Казанский (Приволжский) федеральный университет" (ФГАОУ ВО КФУ) | Устройство мониторинга остаточной механической деформации в участке или звене механического силового агрегата |
FR3118486A1 (fr) * | 2020-12-30 | 2022-07-01 | Safran Helicopter Engines | Ensemble de transmission et de mesure de couple pour une turbomachine |
EP4290200A1 (fr) | 2022-06-08 | 2023-12-13 | Airbus Helicopters | Dispositif d'entraînement mécanique muni d'un couplemètre à roue phonique, boite de transmission de puissance muni d'un tel dispositif d'entraînement mécanique et aéronef |
Families Citing this family (14)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR3013390B1 (fr) | 2013-11-19 | 2019-01-25 | Safran Helicopter Engines | Turbomachine et procede de regulation |
US10436056B2 (en) | 2015-06-23 | 2019-10-08 | General Electric Company | Relative position measurement |
CN105300684B (zh) * | 2015-12-03 | 2018-12-14 | 中国南方航空工业(集团)有限公司 | 长轴组件扭矩标定装置及使用该装置的扭矩标定方法 |
FR3046841B1 (fr) * | 2016-01-20 | 2018-02-02 | Safran Helicopter Engines | Couplemetre a torsion |
US10975717B2 (en) * | 2016-12-19 | 2021-04-13 | General Electric Company | Torque monitoring device for a gas turbine engine |
WO2019217636A1 (fr) | 2018-05-09 | 2019-11-14 | Abb Schweiz Ag | Diagnostic de turbine |
RU2684444C1 (ru) * | 2018-06-14 | 2019-04-09 | федеральное государственное бюджетное образовательное учреждение высшего образования "Волгоградский государственный аграрный университет" (ФГБОУ ВО Волгоградский ГАУ) | Способ определения крутящего момента на вращающемся валу |
US10801360B2 (en) | 2018-06-29 | 2020-10-13 | Pratt & Whitney Canada Corp. | Phonic wheel with output voltage tuning |
US10745110B2 (en) * | 2018-06-29 | 2020-08-18 | Pratt & Whitney Canada Corp. | Propeller blade synchrophasing using phonic wheel |
GB201901113D0 (en) * | 2019-01-28 | 2019-03-13 | Rolls Royce Plc | Shaft monitoring system |
US11286038B2 (en) | 2019-09-03 | 2022-03-29 | Pratt & Whitney Canada Corp. | Pitch control assembly for an aircraft-bladed rotor |
CN113959722B (zh) * | 2021-10-28 | 2023-06-09 | 南京航空航天大学 | 基于音轮的扭矩-桨距-相角-转速集成测量装置及方法 |
CN116164959B (zh) * | 2022-12-30 | 2023-10-17 | 上海尚实航空发动机股份有限公司 | 扭转试验台及使用方法 |
US11906017B1 (en) | 2023-06-02 | 2024-02-20 | Pratt & Whitney Canada Corp. | Drive assembly and method of assembly |
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US4602515A (en) * | 1984-12-03 | 1986-07-29 | Simmonds Precision Products, Inc. | Torque measurement apparatus containing embedded data structure and related method |
FR2595821A1 (fr) | 1986-03-12 | 1987-09-18 | Turbomeca | Procede et dispositif pour mesurer le couple transmis par un arbre soumis a des variations de temperature |
GB2213275A (en) * | 1987-12-26 | 1989-08-09 | Nissan Motor | Magnetostriction type torque sensor with feature of temperature dependent error compensation |
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DE19817886A1 (de) * | 1998-04-22 | 1999-10-28 | Bosch Gmbh Robert | Vorrichtung zur Erfassung des auf eine Welle wirkenden Drehmoments |
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RU1795312C (ru) * | 1991-02-20 | 1993-02-15 | Омский политехнический институт | Устройство дл измерени угла закручивани вращающегос вала |
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JP7054273B2 (ja) | 2021-02-24 | 2022-04-13 | ローレル機械株式会社 | 売上金回収システム |
-
2008
- 2008-05-21 FR FR0853295A patent/FR2931552B1/fr active Active
-
2009
- 2009-05-14 EP EP09749751A patent/EP2288890A1/fr not_active Withdrawn
- 2009-05-14 KR KR1020107026937A patent/KR101604147B1/ko not_active IP Right Cessation
- 2009-05-14 RU RU2010152245/28A patent/RU2497087C2/ru not_active IP Right Cessation
- 2009-05-14 WO PCT/EP2009/055818 patent/WO2009141261A1/fr active Application Filing
- 2009-05-14 JP JP2011509930A patent/JP5579702B2/ja not_active Expired - Fee Related
- 2009-05-14 CN CN200980118180.0A patent/CN102037339B/zh not_active Expired - Fee Related
- 2009-05-14 CA CA2725101A patent/CA2725101A1/fr not_active Abandoned
- 2009-05-14 US US12/990,947 patent/US8464598B2/en not_active Expired - Fee Related
Patent Citations (5)
Publication number | Priority date | Publication date | Assignee | Title |
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US4602515A (en) * | 1984-12-03 | 1986-07-29 | Simmonds Precision Products, Inc. | Torque measurement apparatus containing embedded data structure and related method |
FR2595821A1 (fr) | 1986-03-12 | 1987-09-18 | Turbomeca | Procede et dispositif pour mesurer le couple transmis par un arbre soumis a des variations de temperature |
GB2213275A (en) * | 1987-12-26 | 1989-08-09 | Nissan Motor | Magnetostriction type torque sensor with feature of temperature dependent error compensation |
US5182953A (en) * | 1990-07-13 | 1993-02-02 | Simmonds Precision Products, Inc. | Method and apparatus for shaft torque measurement with temperature compensation |
DE19817886A1 (de) * | 1998-04-22 | 1999-10-28 | Bosch Gmbh Robert | Vorrichtung zur Erfassung des auf eine Welle wirkenden Drehmoments |
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JP2013530348A (ja) * | 2010-07-02 | 2013-07-25 | ターボメカ | トルク計を用いた測定によるフリータービンの過速度の検出 |
KR101948945B1 (ko) | 2011-03-02 | 2019-02-15 | 사프란 헬리콥터 엔진스 | 비틀림 토오크 측정기를 조정하기 위한 방법 |
WO2012117187A1 (fr) * | 2011-03-02 | 2012-09-07 | Turbomeca | Procede de calibration d'un couplemetre a torsion |
CN103403514A (zh) * | 2011-03-02 | 2013-11-20 | 涡轮梅坎公司 | 用于校准扭矩测量仪的方法 |
JP2014507004A (ja) * | 2011-03-02 | 2014-03-20 | ターボメカ | ねじりトルク計を較正する方法 |
US9032776B2 (en) | 2011-03-02 | 2015-05-19 | Turbomeca | Method for calibrating a torsion torquemeter |
FR2972256A1 (fr) * | 2011-03-02 | 2012-09-07 | Turbomeca | Procede de calibration d'un couplemetre a torsion |
RU2596178C2 (ru) * | 2011-03-02 | 2016-08-27 | Турбомека | Способ калибровки измерителя крутящего момента |
WO2014013160A1 (fr) | 2012-07-18 | 2014-01-23 | Centre Technique Des Industries Mecaniques | Dispositif de mesure d'un couple transmis par un arbre de transmission de puissance avec prise en compte des variations de température |
FR2993657A1 (fr) * | 2012-07-18 | 2014-01-24 | Ct Tech Des Ind Mecaniques | Dispositif de mesure d'un couple transmis par un arbre de transmission de puissance avec prise en compte des variations de temperature |
WO2015082835A1 (fr) | 2013-12-03 | 2015-06-11 | Snecma | Dispositif de mesure de couple pour arbre de turbomachine |
FR3118486A1 (fr) * | 2020-12-30 | 2022-07-01 | Safran Helicopter Engines | Ensemble de transmission et de mesure de couple pour une turbomachine |
WO2022144530A1 (fr) * | 2020-12-30 | 2022-07-07 | Safran Helicopter Engines | Ensemble de transmission et de mesure de couple pour une turbomachine |
RU2766620C1 (ru) * | 2021-03-11 | 2022-03-15 | федеральное государственное автономное образовательное учреждение высшего образования "Казанский (Приволжский) федеральный университет" (ФГАОУ ВО КФУ) | Устройство мониторинга остаточной механической деформации в участке или звене механического силового агрегата |
EP4290200A1 (fr) | 2022-06-08 | 2023-12-13 | Airbus Helicopters | Dispositif d'entraînement mécanique muni d'un couplemètre à roue phonique, boite de transmission de puissance muni d'un tel dispositif d'entraînement mécanique et aéronef |
FR3136449A1 (fr) * | 2022-06-08 | 2023-12-15 | Airbus Helicopters | dispositif d’entraînement mécanique muni d’un couplemètre à roue phonique, boîte de transmission de puissance muni d’un tel dispositif d’entraînement mécanique et aéronef |
Also Published As
Publication number | Publication date |
---|---|
EP2288890A1 (fr) | 2011-03-02 |
RU2497087C2 (ru) | 2013-10-27 |
JP5579702B2 (ja) | 2014-08-27 |
FR2931552A1 (fr) | 2009-11-27 |
CA2725101A1 (fr) | 2009-11-26 |
FR2931552B1 (fr) | 2010-07-30 |
RU2010152245A (ru) | 2012-06-27 |
KR20110048489A (ko) | 2011-05-11 |
CN102037339A (zh) | 2011-04-27 |
KR101604147B1 (ko) | 2016-03-16 |
US20110056309A1 (en) | 2011-03-10 |
JP2011521242A (ja) | 2011-07-21 |
US8464598B2 (en) | 2013-06-18 |
CN102037339B (zh) | 2013-06-05 |
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