Detecting a pitch angle adjustment fault
US-2015176570-A1 · Jun 25, 2015 · US
US9976539B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9976539-B2 |
| Application number | US-201514732862-A |
| Country | US |
| Kind code | B2 |
| Filing date | Jun 8, 2015 |
| Priority date | Jun 11, 2014 |
| Publication date | May 22, 2018 |
| Grant date | May 22, 2018 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
A control method and a control system for a wind turbine are disclosed. The control method comprises measuring wind turbine blade pitch angles; obtaining a wind turbine rotor acceleration value; determining whether a blade pitch runaway fault condition is occurring; and during the blade pitch runaway fault condition, adjusting a pitch angle command based at least in part on the rotor acceleration value, a pitch angle of at least one faulted blade and a pitch angle of a healthy blade; and controlling wind turbine blades based at least in part on the adjusted pitch angle command.
Opening claim text (preview).
What is claimed is: 1. A control method comprising: measuring wind turbine blade pitch angles; obtaining a wind turbine rotor acceleration value; determining whether a blade pitch runaway fault condition is occurring; and during the blade pitch runaway fault condition, adjusting a pitch angle command based at least in part on the wind turbine rotor acceleration value, a pitch angle of at least one faulted blade and a pitch angle of a healthy blade, wherein adjusting the pitch angle command comprises: generating a first pitch angle rate command based at least in part on a difference between the pitch angle of the at least one faulted blade and the pitch angle of the healthy blade; generating a second pitch angle rate command based at least in part on the wind turbine rotor acceleration value; summing the first pitch angle rate command and the second pitch angle rate command; and integrating the summed pitch angle rate command; and controlling wind turbine blades based at least in part on the adjusted pitch angle command. 2. The control method of claim 1 , wherein the pitch angle of the healthy blade comprises a pitch angle command for normal operation or a pitch angle measurement of the healthy blade. 3. The control method of claim 1 , wherein the first pitch angle rate command is calculated by the following equation, {dot over (θ)} sync [n ]=max{(θ c [n− 1]−θ f [n ])÷Δ T, 0} wherein: {dot over (θ)} sync represents the first pitch angle rate command, θ c represents the pitch angle of the healthy blade, θ f represents the pitch angle of the at least one faulted blade, n represents a sampling time, and ΔT represents a sampling time interval. 4. The control method of claim 3 , wherein when at least two blades comprise faulted blades, the pitch angle of the at least one faulted blade comprises an average pitch angle of the faulted blades. 5. The control method of claim 1 , further comprising: generating the second pitch angle rate command based on the wind turbine rotor acceleration value in conjunction with a saturation arithmetic with a rotor acceleration upper limit and no lower limit. 6. The control method of claim 5 , wherein the second pitch angle rate command is calculated by the following equation, θ . ω . r = ( ∂ Mz aero ∂ θ 1 + … + ∂ Mz aero ∂ θ m ) - 1 ( - ∂ Mz aero ∂ ω r ω . r + K 1 ( ω . r , ref - ω . r ) ) ω . r , ref = [ ω . r , max , - ∞ ) wherein: {dot over (θ)} {dot over (ω)} r represents the second pitch angle rate command, ∂ Mz aero ∂ θ m represents a partial derivative of rotational moment on the blade pitch angle, m represents a number of the blades, ω r represents an angular velocity of the rotor, ∂ Mz aero ∂ ω r represents a partial derivative of rotational moment on the angular
Onshore wind turbines · CPC title
Cross-Sectional Technologies · mapped topic
Arrangements for mounting or supporting wind motors; Masts or towers for wind motors · CPC title
Adjusting blade pitch · CPC title
Monitoring or testing of wind motors, e.g. diagnostics (testing during commissioning of wind motors F03D13/30) · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.