Wireless rotor track and balance system for rotorcraft
국가/구분 |
United States(US) Patent
등록
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국제특허분류(IPC7판) |
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출원번호 |
US-0924466
(2010-09-28)
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등록번호 |
US-8812255
(2014-08-19)
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발명자
/ 주소 |
- Lynch, Michael A.
- Sadok, Mokhtar
- Zakrzewski, Radoslaw R.
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출원인 / 주소 |
- Simmonds Precision Products, Inc.
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대리인 / 주소 |
Edwards Wildman Palmer LLP
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인용정보 |
피인용 횟수 :
2 인용 특허 :
10 |
초록
▼
Disclosed is a rotor track and balance system for rotorcraft that includes a data processing unit, a tachometer sensor and at least one accelerometer. The tachometer sensor is located remotely from the data processing unit and is mounted proximate to the rotating blades of the rotorcraft. The tachom
Disclosed is a rotor track and balance system for rotorcraft that includes a data processing unit, a tachometer sensor and at least one accelerometer. The tachometer sensor is located remotely from the data processing unit and is mounted proximate to the rotating blades of the rotorcraft. The tachometer sensor is adapted to measure the speed and position of the rotating blades and to wirelessly transmit speed and position data to the data processor. The at least one accelerometer is also located remotely from the data processing unit and is mounted proximate the rotating blades of the rotorcraft. Each accelerometer is adapted to measure vibration anomalies in the rotating blades and to wirelessly transmit vibration data to the data processor. The data processing unit synchronizes the wireless data transmitted from the tachometer sensor and the wireless accelerometer(s) and determines necessary adjustments to be made in order to reduce the vibration anomalies in the rotor blades.
대표청구항
▼
1. A rotor track and balance system for rotorcraft comprising: a) a data processing unit;b) a tachometer sensor located remotely from the data processing unit and mounted proximate to rotating blades of the rotorcraft, the tachometer sensor being adapted to measure the speed and position of the rota
1. A rotor track and balance system for rotorcraft comprising: a) a data processing unit;b) a tachometer sensor located remotely from the data processing unit and mounted proximate to rotating blades of the rotorcraft, the tachometer sensor being adapted to measure the speed and position of the rotating blades and wirelessly transmit speed and position data to the data processor:c) at least one accelerometer located remotely from the data processing unit on the rotorcraft, each accelerometer being adapted to measure vibration in the rotating blades and wirelessly transmit vibration data to the data processor;wherein the data processing unit synchronizes the wireless data transmitted from the tachometer sensor and the at least one wireless accelerometer and determines necessary adjustments to be made in order to reduce any vibration anomalies in the rotor blades,wherein the wireless data from the tachometer sensor and the at least one wireless accelerometer is synchronized prior to processing by the data processing unit. 2. The rotor track and balance system as recited in claim 1, wherein the data collected by the tachometer sensor and the at least one accelerometers is stored in a memory device for a period of time prior to being transmitted to the data processor. 3. The rotor track and balance system as recited in claim 1, wherein the tachometer sensor and each of the at least one accelerometers include an internal clock and each of the clocks are synchronized by the data processing unit. 4. The rotor track and balance system as recited in claim 1, wherein the tachometer sensor and each of the at least one accelerometers include an internal clock and wherein the data processor calculates relative correction times for all of the clocks in order to synchronize the wireless data transmitted from the tachometer sensor and the at least one wireless accelerometer. 5. The rotor track and balance system as recited in claim 1, further comprising a Health and Usage Management System for monitoring the state of the rotorcraft and wherein the data processor is part of the HUMS. 6. The rotor track and balance system as recited in claim 5, wherein at least a portion of the rotorcraft's HUMS in located onboard. 7. The rotor track and balance system as recited in claim 5, wherein the rotorcraft's HUMS includes a memory device for storing the data transmitted wirelessly by the tachometer sensor and the at least one accelerometer. 8. The rotor track and balance system as recited in claim 1, wherein the tachometer sensor and at least one of the accelerometers include an energy harvesting unit. 9. The rotor track and balance system as recited in claim 1, wherein the tachometer sensor and each of the at least one accelerometers include a radio utilizing a transmission protocol which is selected from the group of IEEE 802.11, 802.15.4 or 802.16. 10. The rotor track and balance system as recited in claim 1, further comprising a backup tachometer sensor located remotely from the data processing unit and mounted proximate to rotating blades of the rotorcraft, the tachometer sensor being adapted to measure the speed and position of the rotating blades and transmit speed and position data to the data processor. 11. A method for tracking and balancing rotating blades of a rotorcraft, the method comprising the steps of: a) providing a data processing unit;b) positioning a tachometer sensor onboard the rotorcraft remotely from the data processing unit and proximate to the rotating blades of the rotorcraft;c) measuring with the tachometer sensor the speed and position of the rotating blades;d) transmitting wirelessly speed and position data from the tachometer sensor to the data processor;e) positioning at least one accelerometer onboard the rotorcraft remotely from the data processing unit;f) measuring using each accelerometer vibrations in the rotating blades;g) transmitting wirelessly for each accelerometer vibration data to the data processor;h) synchronizing using the data processor the wireless data transmitted from the tachometer sensor and each of the at least one wireless accelerometers; andi) determining using the data processor necessary adjustments to be made in order to reduce any vibration anomalies in the rotor blades,wherein the synchronizing the wireless data transmitted from the tachometer sensor and each of the at least one wireless accelerometers is done prior to wirelessly transmitting the data to the data processing unit. 12. The method for tracking and balancing rotating blades of a rotorcraft as recited in claim 11, further comprising the step of storing in a sensor memory device the data collected by the tachometer sensor and the at least one accelerometer for a period of time prior to transmitting the date to the data processor. 13. The method for tracking and balancing rotating blades of a rotorcraft as recited in claim 11, further comprising the steps of: i) providing the tachometer sensor and each of the at least one accelerometers with a clock; andii) synchronizing the clock using the data processing unit. 14. The method for tracking and balancing rotating blades of a rotorcraft as recited in claim 11, further comprising the steps of: i) providing the tachometer sensor and each of the at least one accelerometers with a clock; andii) calculating using the data processor relative correction times for all of the clocks in order to synchronize the wireless data transmitted from the tachometer sensor and the at least one wireless accelerometer. 15. The method for tracking and balancing rotating blades of a rotorcraft as recited in claim 11, further comprising the step of providing a Health and Usage Management System for monitoring vibration anomalies in the rotorcraft's airframe and wherein the data processor is part of the HUMS. 16. The method for tracking and balancing rotating blades of a rotorcraft as recited in claim 15, wherein at least a portion of the rotorcraft's HUMS in provided onboard. 17. The method for tracking and balancing rotating blades of a rotorcraft as recited in claim 16, wherein the speed and position data and vibration data is transmitted wirelessly from the rotorcraft's onboard HUMS to a HUMS ground station computer for analysis. 18. A track and balance system for rotating blades of a rotorcraft comprising: a) a tachometer sensor mounted proximate to the rotating blades of the rotorcraft, the tachometer sensor being adapted to measure the speed and position of the rotating blades and wirelessly transmit speed and position data;b) a plurality of vibration sensors mounted on the rotorcraft, each vibration sensor being adapted to measure vibrations in the rotating blades and wirelessly transmit vibration data; andc) a data processor associated with an onboard Heath and Usage Management System which is adapted and configured to receive the speed and position data transmitted by the tachometer sensor and the vibration data transmitted by the plurality of vibration sensors; andwherein the Health and Usage Management system commands the sensors as to when data is to be acquired, when data is to be transmitted, and determines necessary adjustments to be made in order to reduce any vibration anomalies in the rotor blades,wherein the data processor synchronizes the acquired data prior to transmitting the data to the data processor. 19. The track and balance system for rotating blades of a rotorcraft as recited in claim 18, wherein the data collected by the tachometer sensor and the vibration sensors is stored in a memory device for a period of time prior to being transmitted to the data processor. 20. The track and balance system for rotating blades of a rotorcraft as recited in claim 18, wherein the tachometer sensor and the vibration sensors include a clock and each of the clocks are synchronized by the data processing unit.
이 특허에 인용된 특허 (10)
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Grieb Paul (Huntsville AL) Deaton Donald (Madison AL) Collison Harry (New Smyrna Beach FL), Air-driven, turbine tow reel machine controlled according to towline velocity and vent door position.
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Chadwick ; James R., Aircraft rotor out-of-track correction method and apparatus.
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Chadwick James R. (Bradbury CA) Johnson Lloyd N. (Glendora CA), Control of rotor blade stroboscopic display.
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Dennis K. Kennedy ; Friedrich K. Straub ; Ahmed A. Hassan, Helicopter in-flight rotor tracking system, method, and smart actuator therefor.
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Wright Dale M. (Folsom CA) Kiraly Robert L. (Mesa AZ), In-flight monitoring of composite structural components such as helicopter rotor blades.
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Curtis George C. (Marietta GA) McInturff Joe A. (Marietta GA) Rubel Herbert J. (Atlanta GA) Wall William F. (Marietta GA), Means for balancing rotors of a machine.
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Chadwick James R. (Bradbury CA), Method and apparatus to determine need for rotor blade pitch adjustment and/or blade substitution.
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C. Samuel Ventres, Method for determining a minimal set of rotor blade adjustments.
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Yeung, King-Wah Walter; Yeung, Wei-Wei Vivian, Post data-collection synchronization for approximation of simultaneous data.
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McBrien,Gary M.; Gottwald,James, Vibration monitoring system for gas turbine engines.
이 특허를 인용한 특허 (2)
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Wirth, Richard Brian; Winchcomb, Robert; Calvert, Bruce; Wigny, Robert, Propeller balancing using inflight data.
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Dempsey, Patrick J.; White, Matthew A.; Kellner, Aaron; King, Joshua, Relative acceleration blade position measurement.
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