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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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01 Jan 1979
TL;DR: In this paper, wind-tunnel tests of an aeroelastically designed helicopter rotor model were carried out to determine the effects on dynamic response and aerodynamic performance of varying the design of the outboard 8 percent of the blade length.
Abstract: Wind-tunnel tests of an aeroelastically designed helicopter rotor model were carried out to determine the effects on dynamic response and aerodynamic performance of varying the design of the outboard 8 percent of the blade lengths. Four different blade tip geometries or shapes having different amounts of planform sweep, thickness and chordwise taper, and anhedral angle were studied. Each configuration was tested at several shaft angles of attack for advance ratios of 0.20, 0.30, 0.35, and 0.40. For each combination of shaft angle and advance ratio, rotor lift was varied over a wide range to include high lift conditions.

21 citations

Patent
15 Apr 2009
TL;DR: In this article, a vertical axis wind turbine that can be actively controlled is provided, which includes mechanisms and methods for enabling high-efficiency wind energy extraction using active pitch and camber control of individual blades.
Abstract: A vertical axis wind turbine that can be actively controlled is provided. This invention includes mechanisms and methods for enabling high-efficiency wind energy extraction by a vertical axis wind turbine using active pitch and camber control of individual blades. Blade control is further integrated with generator control and power electronics. Integrated control algorithms are systematically constructed, and transmitted to the wind turbine through a wireless communications interface. The interface also allows the user to continuously monitor the state of the wind turbine system. This invention includes sensors and procedures for periodic self-calibration of wind turbine parameters for preserving the long-term efficiency of wind energy extraction. Furthermore, a capability to intelligently interact with other wind turbine systems in a wind-farm setting is incorporated.

21 citations

Patent
07 Nov 1969
TL;DR: In this article, a variable-pitch bladed rotor, a hydraulic actuator for effecting pitch variation of the blading of the rotor, and a pump driven by the rotor to supply fluid for operation of the actuator are arranged coaxially.
Abstract: A ram-air turbine comprises a variable-pitch bladed rotor, a hydraulic actuator for effecting pitch variation of the blading of the rotor, and a pump driven by the rotor to supply fluid for operation of the actuator. A rotary speed-sensitive flyweight governor is provided to control the supply of fluid to the actuator whereby to cause the rotor automatically to rotate at constant speed, and the arrangement includes a machine driven by the rotor. The rotor, hydraulic actuator, pump, governor and driven machine are all coaxially arranged.

21 citations

Patent
23 Feb 2001
TL;DR: In this paper, the rotation field of the rotation current generated in the permanent magnet generator is connected to the short-circuit rotors, so that they rotate the rotor blades in their feathered pitch.
Abstract: The device uses electric motors (14) to adjust the rotor blade angle. The rotor blades (4) can be rotated in their feathered pitch by connection with a contactor (15) arranged in an emergency current circuit (7,12,14) with an independent energy source. At least one permanent magnet generator (7) assigned to the rotor shaft (2) is arranged in the emergency current circuit as the energy source. The electric motors are formed as short-circuit rotors, where the rotation field of the rotation current generated in the permanent magnet generator is connected to the short-circuit rotors, so that they rotate the rotor blades in their feathered pitch.

21 citations

Patent
21 Apr 2009
TL;DR: In this paper, a self-contained electrical generator comprising a first hub and second hub with respective generator parts is proposed to generate electrical power in coils opposed by permanent magnets for controllable turbo prop arrangements.
Abstract: In some circumstances such as with regard to contra-rotating turbo prop arrangements in aircraft it is desirable to vary the pitch of the blades and/or provide de-icing facilities. Advantageously, these blade pitch and de-icing facilities could be provided through electrical actuators. Unfortunately, provision of electrical power to such rotating components traditionally requires utilisation of slip rings which are subject to wear. By providing a self-contained electrical generator comprising a first hub and second hub with respective generator parts it is possible to utilise the contra-rotating nature in order to create relative motion and therefore electrical power generation in coils opposed by permanent magnets. Slide contacts for electrical connection are avoided whilst electrical power can be generated within the rotating reference frame defined by the hubs.

21 citations


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