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公开(公告)号:ZA831632B
公开(公告)日:1983-11-30
申请号:ZA831632
申请日:1983-03-09
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRIC JOHN PETER , HARNER KERMIT IVAN
Abstract: Damping of the primary bending mode of a tower (12) mounting a wind turbine having a control (36) for providing a pitch blade angle reference signal (40) to modulate the pitch of the turbine blades (1) through a pitch change mechanism (38) for constant power is provided by generating the pitch blade angle reference signal as the integral (104) of the summation (266) of a torque/power controlling blade pitch angle reference rate signal (98) with an estimated acceleration signal (255) generated by filtering (250, 252, 254) the blade pitch angle reference signal (40) with the following transfer function
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公开(公告)号:DE3308566A1
公开(公告)日:1983-10-13
申请号:DE3308566
申请日:1983-03-10
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
Abstract: An accelerometer (1) disposed on the support tower (12) of a wind turbine electric generating system in the vicinity of the rotor (10, 16) thereof provides a signal (1) indicative of acceleration of the tower in the direction of the rotor rotational axis. The signal (2) is passed through a band-pass filter (4) for summation (9) with a torque/power controlled (100) blade pitch angle reference rate signal (98), the integral (104) of which provides a blade pitch angle reference signal (40) to control the pitch angle of the rotor blades (10) through a pitch change mechanism (38), thereby to provide additional, positive aerodynamic damping to the tower while modulating blade angle for constant torque/power in response to wind turbulence.
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公开(公告)号:NO830945A
公开(公告)日:1983-10-03
申请号:NO830945
申请日:1983-03-17
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
CPC classification number: F03D7/043 , F03D7/0224 , F03D7/0292 , F03D9/25 , F03D80/00 , F05B2240/912 , F05B2260/821 , F05B2260/96 , F05B2270/1033 , F05B2270/322 , F05B2270/335 , Y02E10/723 , Y02E10/728
Abstract: Damping of the primary bending mode of a tower (12) mounting a wind turbine having a control (36) for providing a pitch blade angle reference signal (40) to modulate the pitch of the turbine blades (1) through a pitch change mechanism (38) for constant power is provided by generating the pitch blade angle reference signal as the integral (104) of the summation (266) of a torque/power controlling blade pitch angle reference rate signal (98) with an estimated acceleration signal (255) generated by filtering (250, 252, 254) the blade pitch angle reference signal (40) with the following transfer function
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公开(公告)号:DK136683D0
公开(公告)日:1983-03-25
申请号:DK136683
申请日:1983-03-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HARNER KERMIT IVAN , KOS JOSEPH MICHAEL , PATRICK JOHN PETER
Abstract: Damping of the primary bending mode of a tower (12) mounting a wind turbine having a control (36) for providing a pitch blade angle reference signal (40) to modulate the pitch of the turbine blades (1) through a pitch change mechanism (38) for constant power is provided by generating the pitch blade angle reference signal as the integral (104) of the summation (266) of a torque/power controlling blade pitch angle reference rate signal (98) with an estimated acceleration signal (255) generated by filtering (250, 252, 254) the blade pitch angle reference signal (40) with the following transfer function
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公开(公告)号:DE2961688D1
公开(公告)日:1982-02-18
申请号:DE2961688
申请日:1979-08-02
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , HARNER KERMIT IVAN , PATRICK JOHN PETER
Abstract: A multi-mode electronic wind turbine control system establishes a reference blade angle BR for a two-bladed, horizontal axis, variable pitch wind turbine rotor, the blade angle being regulated by a hydraulic pitch change mechanism (38). The rotor (10), via appropriate shafts and a gearbox (20), is coupled to a synchronous generator (24) to produce electrical energy which is fed to a power utility grid. The control system (36) provides closed loop pitch control for rotor acceleration rate during start-up, for rotor deceleration rate during shut-down, for speed control when the synchronous generator is off-line, and for power control when the synchronous generator is on-line. A single control integrator is used for all closed loop operating modes, with a rate limiter circuit in front of the control integrator to prevent integrator overtravel. The integrator has maximum and minimum blade angle stops, the minimum stop being variable as a function of rotor speed and wind speed. When on-line, power control is provided by a unique shaft torque control using proportional plus integral plus derivative controls in combination.
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公开(公告)号:DE2922972A1
公开(公告)日:1980-01-03
申请号:DE2922972
申请日:1979-06-06
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HARNER KERMIT IVAN , KOS JOSEPH MICHAEL , PATRICK JOHN PETER
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公开(公告)号:AU601410B2
公开(公告)日:1990-09-13
申请号:AU7221487
申请日:1987-04-28
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , RAPP ALLEN FLOYD
Abstract: A variable speed wind turbine is controlled in a way which avoids the turbine lingering at a critical speed which would otherwise tend to cause excessive vibration. The disclosed method and apparatus increases speed at a selected rate with respect to generator output power except in the vicinity of the critical speed. The selected rate is changed in the vicinity of the critical speed to a different rate which is selected slower in the selected embodiment, to avoid commanding the critical speed. After the output power increases or decreases beyond the critical point, a deliberate discontinuity in the speed command signal is induced. A rapid speed change through the critical speed is accompanied by a corresponding power output change. If the speed is increasing at a selected slower rate below the critical speed, and the speed command signal is stepped to a higher level just before reaching the critical speed, the speed will rapidly increase and quickly pass through the critical speed while the power output decreases. Similarly, if the speed is decreasing at a selected slower rate above the critical speed, and the speed command signal is stepped to a lower level just before reaching the critical speed, the speed will rapidly decrease and quickly pass through the critical speed while the power output increases.
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公开(公告)号:FI77091C
公开(公告)日:1989-01-10
申请号:FI831030
申请日:1983-03-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
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公开(公告)号:FI76627C
公开(公告)日:1988-11-10
申请号:FI792440
申请日:1979-08-06
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
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公开(公告)号:FI77091B
公开(公告)日:1988-09-30
申请号:FI831030
申请日:1983-03-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
Abstract: An accelerometer (1) disposed on the support tower (12) of a wind turbine electric generating system in the vicinity of the rotor (10, 16) thereof provides a signal (1) indicative of acceleration of the tower in the direction of the rotor rotational axis. The signal (2) is passed through a band-pass filter (4) for summation (9) with a torque/power controlled (100) blade pitch angle reference rate signal (98), the integral (104) of which provides a blade pitch angle reference signal (40) to control the pitch angle of the rotor blades (10) through a pitch change mechanism (38), thereby to provide additional, positive aerodynamic damping to the tower while modulating blade angle for constant torque/power in response to wind turbulence.
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