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公开(公告)号:NO830945L
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
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:NO830944A
公开(公告)日:1983-10-03
申请号:NO830944
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 , F05B2260/96 , F05B2270/1033 , F05B2270/322 , F05B2270/334 , Y02E10/723 , Y02E10/728
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:DK136583A
公开(公告)日:1983-10-03
申请号:DK136583
申请日:1983-03-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: HARNER KERMIT IVAN , KOS JOSEPH MICHAEL , PATRICK JOHN PETER
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:IN151737B
公开(公告)日:1983-07-16
申请号:IN809CA1979
申请日:1979-08-03
Applicant: UNITED TECHNOLOGIES CORP , KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT JVAN
Inventor: UNITED TECHNOLOGIES CORPORATIO , KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT JVAN
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:IT8320367D0
公开(公告)日:1983-03-30
申请号:IT2036783
申请日:1983-03-30
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK 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:FI831031A0
公开(公告)日:1983-03-25
申请号:FI831031
申请日:1983-03-25
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK 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:DE3150824A1
公开(公告)日:1982-08-05
申请号:DE3150824
申请日:1981-12-22
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , KOS JOSEPH MICHAEL , HARNER KERMIT IVAN
Abstract: A blade pitch angle control for a wind turbine-generator establishing an optimum power or torque reference signal which, when operating conditions so warrant, is not limited by the nominal torque or power ratings of various turbine generator components. The reference signal is indicative of a maximum blade angle setting for safe operation of the wind turbine. An integral or lag compensation circuit for enhanced transient and steady-state operation may be employed.
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公开(公告)号:AU7883481A
公开(公告)日:1982-07-01
申请号:AU7883481
申请日:1981-12-23
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , KOS JOSEPH MICHAEL , HARNER KERMIT IVAN
Abstract: A blade pitch angle control for a wind turbine-generator establishing an optimum power or torque reference signal which, when operating conditions so warrant, is not limited by the nominal torque or power ratings of various turbine generator components. The reference signal is indicative of a maximum blade angle setting for safe operation of the wind turbine. An integral or lag compensation circuit for enhanced transient and steady-state operation may be employed.
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公开(公告)号:FR2470408A1
公开(公告)日:1981-05-29
申请号:FR8024727
申请日:1980-11-21
Applicant: UNITED TECHNOLOGIES CORP
Inventor: PATRICK JOHN PETER , GOODMAN ROBERT BERNARD
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公开(公告)号:NO792639L
公开(公告)日:1980-02-19
申请号:NO792639
申请日:1979-08-14
Applicant: UNITED TECHNOLOGIES CORP
Inventor: KOS JOSEPH MICHAEL , PATRICK JOHN PETER , HARNER KERMIT IVAN
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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