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Blade pitch

About: Blade pitch is a research topic. Over the lifetime, 5321 publications have been published within this topic receiving 63134 citations.


Papers
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Patent
23 Jul 1990
TL;DR: In this article, a pitch change mechanism for an aircraft propeller is described, in which a common ring gear changes pitch of all propeller blades on a given rotor simultaneously and a large deceleration occurs, driving the blades to a safe, feathered position.
Abstract: The invention concerns a pitch change mechanism for an aircraft propeller in which a common ring gear (51) changes pitch of all propeller blades on a given rotor simultaneously Motion of the ring gear (51) is induced by a planet (40)-and-carrier (101) system driven by a pinion (110) Acceleration of the pinion causes a change toward flat pitch Deceleration of the pinion causes change toward feathered pitch If the motor driving the pinion fails, a large deceleration occurs, driving the blades to a safe, feathered position

43 citations

Patent
17 Mar 1980
TL;DR: In this paper, a pitch control system for a multibladed variable pitch wind turbine is described, where the actuators are supplied with hydraulic fluid from second sources thereof under conditions of normal pitch change adjustment.
Abstract: A pitch control system for a multibladed variable pitch wind turbine. Each of the turbine blades is pivotally driven about the longitudinal axis thereof independently of the other blades by at least a pair of hydraulic actuators. The actuators are supplied with pressurized hydraulic fluid from a first source thereof under conditions of normal pitch change adjustment. Under conditions wherein feathering of the blades is required, the actuators are supplied with hydraulic fluid from second sources thereof such that one of the actuators associated with each of the blades is supplied with fluid from one second source and a second actuator is provided with fluid from a redundant second source whereby blade feathering may be effected despite a malfunction of one of the redundant sources or one of the actuators. In one of the two preferred embodiments disclosed, the first and second fluid sources are maintained in mutual communication whereby fluid from the second sources thereof may supplement fluid from the first source under conditions of normal blade pitch adjustment.

43 citations

Journal ArticleDOI
28 Jan 2020-Energy
TL;DR: In this article, the effect of dimpled surface blades on the performance of a V47-660kW horizontal axis wind turbine is numerically investigated using an incompressible Reynolds-Averaged Navier-Stokes solver and k − ω Shear-Stress Transport turbulent model.

43 citations

Patent
25 Sep 1999
TL;DR: In this paper, a management system is designed to regulate the rotational speed of the rotor within a predetermined wind speed range by adjusting the rotor blade angle, and which can shut down the operation of the system when a shut-down speed is exceeded.
Abstract: The invention relates to wind energy system comprising a rotor (3) which can be wind-driven and which comprises adjustable rotor blades (4). The wind energy system also comprises a generator which is directly or indirectly connected to the rotor and which is provided for generating electrical energy. The generator can output power with a variable rotational speed of the rotor. A management system is also provided which is designed to regulate the rotational speed of the rotor within a predetermined wind speed range by adjusting the rotor blade angle, and which can shut down the operation of the system when a shut-down speed is exceeded. According to the invention, a wind energy system can be economically manufactured in an advantageous manner while using fewer materials and accruing lower energy costs if the management system is designed to regulate downward the rotational speed of the rotor and the power output by adjusting the rotor blade angle within a range between a predetermined limiting speed and the shut-down speed.

43 citations

Patent
29 Apr 1999
TL;DR: In this paper, a system for controlling the pitch of a propeller blade using a transfer bearing and a pitch change actuator is presented. But the mechanism is fluidically connected to and translatable relative to the transfer tube.
Abstract: A system (10) for controlling propeller blade pitch is disclosed. The system (10) comprises a transfer tube (18), wherein the transfer tube (18) defines an element of the rotatable portion (12) and wherein the transfer tube (18) is non-translating relative the rotatable (12) and non-rotatable portions (26). A transfer bearing (16) for providing hydraulic fluid to and interfacing with the transfer tube (18) is also used, wherein the transfer bearing (16) is located on the non-rotatable portion (26). The system further includes a pitch change actuator (22) and a mechanism form (74) for actuating the pitch change actuator (22), wherein the mechanism (74) is fluidically connected to and translatable relative to the transfer tube (18). A device for measuring blade angle of the propeller blade (120) is also provided, wherein the device is separate and distinct from the transfer tube (18).

43 citations


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Performance
Metrics
No. of papers in the topic in previous years
YearPapers
202377
2022163
202184
2020110
2019105
2018109