초록 ▼

A method for inspecting at least one rotor blade of a wind turbine for damage, such as subsurface blade cracks, includes the steps of: attaching at least one acoustic emission sensor to a surface of a rotor blade to be inspected, exciting oscillations in the rotor blade for a time period, measuring

A method for inspecting at least one rotor blade of a wind turbine for damage, such as subsurface blade cracks, includes the steps of: attaching at least one acoustic emission sensor to a surface of a rotor blade to be inspected, exciting oscillations in the rotor blade for a time period, measuring activity signals of the oscillations in the rotor blade with the at least one acoustic emission sensor, and detaching the at least one acoustic emission sensor from the surface of the rotor blade after the inspection. An inspection system for a rotor blade of a wind turbine is also contemplated.

대표청구항 ▼

1. A method for inspecting at least one rotor blade of a wind turbine, comprising: while the rotor blade is oscillating, measuring activity signals of the oscillations in the rotor blade with an acoustic emission sensor that is attached to at least one of (i) an outer rotor blade surface within a th

1. A method for inspecting at least one rotor blade of a wind turbine, comprising: while the rotor blade is oscillating, measuring activity signals of the oscillations in the rotor blade with an acoustic emission sensor that is attached to at least one of (i) an outer rotor blade surface within a third of a rotor blade length of the rotor blade as measured from a rotor blade tip and (ii) an internal rotor blade surface within half of a rotor blade length of the rotor blade as measured from a rotor blade hub; anddetermining damage to the rotor blade based on the measured activity signals. 2. The method according to claim 1, wherein the oscillations are caused by manually introducing at least one of flap and edge wise oscillations. 3. The method according to claim 1, wherein the activity signals are measured with the acoustic emission sensor in surface contact with structural means of the rotor blade. 4. The method according to claim 1, further comprising: positioning the acoustic emission sensor such that a contact surface of the acoustic emission sensor faces the surface of the rotor blade or a surface of an element within the rotor blade; andbefore positioning the acoustic emission sensor, applying an acoustic coupling agent between the contact surface and the surface of the rotor blade or the surface of the element. 5. The method according to claim 1, where at least two acoustic sensors are positioned opposite each other on leeward and windward sides of the rotor blade. 6. The method according to claim 1, wherein the acoustic sensor is attached to at least one of an outer rotor blade surface in a centre position in relation to leading and trailing edges of the rotor blade and a spar beam of the rotor blade. 7. The method according to claim 1, wherein the acoustic sensor is attached to the outer rotor blade surface or to the internal rotor blade surface or to the outer and the internal rotor blade surfaces in combination. 8. The method according to claim 1, wherein the measured activity signals are transferred from the acoustic emission sensor to a portable acoustic emission unit to be at least one of stored, investigated and displayed. 9. The method according to claim 8, wherein the transfer of the activity signals from the acoustic emission sensor to the portable acoustic emission unit is performed by cables or by wireless communication. 10. The method according to claim 1, wherein measuring the activity signals is performed while the rotor blade is at a standstill and locked. 11. The method according to claim 1, wherein the activity signals detected by the acoustic emission sensor are compared with pre-established reference level values. 12. The method according to claim 1, wherein activity signals detected by at least two acoustic emission sensors in proximity of each other are used for directional damage detection. 13. An inspection system for measuring oscillations in at least one rotor blade of a wind turbine, said system comprising an acoustic emission sensor attached to at least one of (i) an outer rotor blade surface within a third of a rotor blade length of the rotor blade as measured from a rotor blade tip and (ii) an internal rotor blade surface within half of a rotor blade length of the rotor blade as measured from a rotor blade hub, the acoustic emission sensor configured to produce a signal based on the oscillations of the rotor blade; anda portable acoustic emission unit configured to at least one of store, investigate and display the signal, wherein the signal is transferred from the one acoustic emission sensor via at least one of cable and wireless connection means. 14. The inspection system according to claim 13, further comprising attachment means for attaching the acoustic emission sensor, wherein the attachment means comprise one or more mounting brackets and an acoustic coupling agent. 15. The inspection system according to claim 13, wherein at least two acoustic emission sensors are attached to the rotor blade. 16. A method for inspecting at least one rotor blade of a wind turbine, comprising: while the rotor blade is oscillating, measuring activity signals of the oscillations in the rotor blade with an acoustic emission sensor that is located on a surface of the rotor blade or within the rotor blade; anddetermining damage to the rotor blade based on the measured activity signals, wherein the activity signals are measured for a time period of at least 5 seconds. 17. A method for inspecting at least one rotor blade of a wind turbine, comprising: while the rotor blade is oscillating, measuring activity signals of the oscillations in the rotor blade with an acoustic emission sensor that is located on a surface of the rotor blade or within the rotor blade, wherein the activity signals are measured while a rotor comprising the rotor blade is rotating using a rotor hub, and wherein the activity signals are measured while the rotor is performing an emergency stop sequence; anddetermining damage to the rotor blade based on the measured activity signals. 18. The method of claim 17, wherein the acoustic emission sensor is associated with a different acoustic emission sensor, wherein the two acoustic emission sensors are located on the surface of the rotor blade and are positioned substantially opposite each other on a leeward side and a windward side of the rotor blade.