Device for measuring deformations of a rotor blade and method for installing such a device

Patent metadata

Field	Value
Publication number	US-9534586-B2
Application number	US-201514854063-A
Country	US
Kind code	B2
Filing date	Sep 15, 2015
Priority date	Sep 16, 2014
Publication date	Jan 3, 2017
Grant date	Jan 3, 2017

Abstract

A device for measuring deformations of a rotor blade of a wind turbine generator system includes a position-measuring device having a first assembly and a second assembly. The first assembly is disposed so as to be movable relative to the second assembly. The position-measuring device is configured to measure a relative position between the first and second assemblies. An arm mechanically coupled to the first assembly has a first adhesive bonding surface configured to allow the arm to be permanently joined to the rotor blade. The second assembly has a second adhesive bonding surface configured to allow the second assembly to be permanently joined to the rotor blade. A first mounting element is fixed to at the second assembly and/or the arm. A second mounting element is adhesively attachable to the rotor blade. The first mounting element is detachably joinable to the second mounting element.

First claim

What is claimed is:

1. A device for measuring deformations of a rotor blade of a wind turbine generator system, the device comprising:
a position-measuring device having a first assembly and a second assembly, the first assembly being disposed so as to be rotatable relative to the second assembly about an axis, the position-measuring device being configured to measure a relative angular position between the first and second assemblies;
an arm mechanically coupled to the first assembly and having a first adhesive bonding surface configured to allow the arm to be permanently joined to the rotor blade at the first adhesive bonding surface, the second assembly having a second adhesive bonding surface configured to allow the second assembly to be permanently joined to the rotor blade, the first adhesive bonding surface being disposed at a distance (X) from the second adhesive bonding surface in a direction of extension of the arm, the arm being mechanically coupled to the first assembly at a radial distance such that a relative angular displacement is producible between the first and second assemblies in response to a change in the distance (X);
a first mounting element fixed to at least one of the second assembly and the arm; and
a second mounting element that is adhesively attachable to the rotor blade, the first mounting element being detachably joinable to the second mounting element.

2. The device as recited in claim 1 , wherein the second mounting element has an adhesive layer configured to adhesively attach the second mounting element to the rotor blade.

3. The device as recited in claim 1 , wherein the first mounting element is detachably joinable to the second mounting element by a hook and loop fastener.

4. The device as recited in claim 1 , wherein the first assembly is articulated to the arm via a flexible component.

5. The device as recited in claim 1 , wherein the position-measuring device has a measuring standard and an element configured to scan the measuring standard.

6. The device as recited in claim 5 , wherein the element configured to scan the measuring standard is photosensitive.

7. A method for installing a device for measuring deformations to a rotor blade, the method:
providing the device, the device comprising:
a position-measuring device having a first assembly and a second assembly, the first assembly being disposed so as to be movable relative to the second assembly, the position-measuring device being configured to measure a relative position between the first and second assemblies;
an arm mechanically coupled to the first assembly and having a first adhesive bonding surface configured to allow the arm to be permanently joined to the rotor blade at the first adhesive bonding surface, the second assembly having a second adhesive bonding surface configured to allow the second assembly to be permanently joined to the rotor blade;
a first mounting element fixed to at least one of the second assembly and the arm; and
a second mounting element that is adhesively attachable to the rotor blade, the first mounting element being detachably joinable to the second mounting element, attaching the second mounting element to the rotor blade; then

applying an adhesive to the first and second adhesive bonding surfaces; and then
attaching the device to the rotor blade by joining the first mounting element fixed on the device and the second mounting element attached to the rotor blade together, the adhesive being in contact with both the first and second adhesive bonding surfaces, as well as with the rotor blade.

8. The method as recited in claim 7 , wherein the second mounting element has an adhesive layer configured to adhesively attach the second mounting element to the rotor blade, the method, after providing the device and prior to applying the adhesive, further comprising:
detachably joining the second mounting element to the first mounting element prior to the second mounting element being attached to the rotor blade;
pressing the device onto the rotor blade such that the second mounting element adheres to the rotor blade, and
removing the device from the rotor blade for subsequent application of the adhesive.

9. The method as recited in claim 7 , wherein the first mounting element and the second mounting element are directly joined to each other.

Assignees

• Heidenhain Gmbh Dr Johannes

Inventors

• Meyer Hermann
• Sigl Thomas

Classifications

• Y02E10/72

  Wind turbines with rotation axis in wind direction · CPC title

• G01B5/30

  for measuring the deformation in a solid, e.g. mechanical strain gauge · CPC title

• G01M5/0058

  of elongated objects, e.g. pipes, masts, towers or railways · CPC title

• G01L1/04

  by measuring elastic deformation of gauges, e.g. of springs · CPC title

• G01M5/0016

  of aircraft wings or blades · CPC title