Method for repairing an airfoil surface having an elastomeric protective coating

• US 9,770,791 B2
• Filed: 12/01/2011
• Issued: 09/26/2017
• Est. Priority Date: 12/14/2005
• Status: Active Grant

• Current Assignee: Hontek Corporation
• Original Assignee: Hontek Corporation
• Inventors: Hong, Shek C.
• Primary Examiner(s): Afzali, Sarang
• Application Number:
  US13/308,788
• Publication Number:
  US 20120094099A1
• Time in Patent Office: 2,126 Days
• Field of Search: 298891, 2940218, 29458, 29459, 29460, 427140, 427142, 427290, 427292, 4274071, 427409, 427355, 427356, 427368, 427429
• CPC Class Codes: B05D 1/42 by non-rotary members
• CPC Class Codes: B05D 5/005 Repairing damaged coatings
• CPC Class Codes: B05D 5/06 to obtain multicolour or other optical effects B05D5/02 takes precedence
• CPC Class Codes: B05D 7/56 Three layers or more
• CPC Class Codes: B05D 7/58 No clear coat specified
• CPC Class Codes: B23P 6/007 using only additive methods, e.g. build-up welding
• CPC Class Codes: B64F 5/40 Maintaining or repairing aircraft
• CPC Class Codes: F01D 5/005 Repairing methods or devices
• CPC Class Codes: F05D 2230/10 by removing material
• CPC Class Codes: F05D 2230/30 with deposition of material
• CPC Class Codes: F05D 2230/90 Coating; Surface treatment
• CPC Class Codes: F05D 2300/43 Synthetic polymers, e.g. plastics; Rubber
• CPC Class Codes: F05D 2300/611 Coating
• CPC Class Codes: Y02T 50/60 Efficient propulsion technologies, e.g. for aircraft
• CPC Class Codes: Y10T 29/49318 Repairing or disassembling
• CPC Class Codes: Y10T 29/49746 by applying fluent material, e.g., coating, casting
• CPC Class Codes: Y10T 428/24942 including components having same physical characteristic in differing degree
• CPC Class Codes: Y10T 428/2495 Thickness [relative or absolute]

Abstract

This invention relates to the repair and removal of erosion or impact damage with a liquid repair material using a flexible applicator capable of conforming to the surface of the leading edge of the airfoil while being drawn lengthwise along the airfoil surface of a helicopter or wind turbine rotor blade thereby restoring the aerodynamic contour with or without the addition of an optional topcoat layer.

Claims

1. A method of field repairing an airfoil surface having an elastomeric protective coating adhered to a portion of said airfoil surface having a plurality of irregular damage cavities caused by sand and water erosion or impact damage comprising:

filling said plurality of irregular damage cavities in said elastomeric protective coating with a liquid repair material having viscosity between a brushable coating and a flowable caulking compound using a flexible planar applicator having no handle capable of being manually conformed to a sharply curved, forward facing leading edge and contour surfaces directly adjacent to the leading edge of said airfoil surface while being drawn lengthwise along the airfoil surface, wherein said filling step comprises applying an elastomeric polyurethane, polyurea or fluoroelastomer to fill said plurality of irregular damage cavities to form filled cavities, restoring said airfoil surface to a smooth aerodynamic surface contour and providing protection against sand and water erosion; and

applying an optional topcoat layer over the filled cavities, wherein the airfoil surface is a part of a rotor blade of a helicopter or a windmill and the repair method is performed in a field environment.

2. The method of claim 1, wherein said optional topcoat layer is a polyurethane, polyurea or fluoroelastomer topcoat layer.

3. The method of claim 1, wherein said flexible planar applicator is a flat sheet of elastomeric or thermoplastic material of selected thickness to allow it to be deformable to conform to the airfoil surface and stiff enough to spread said liquid repair material smoothly.

4. The method of claim 1, wherein said flexible planar applicator is a flat sheet of high density polyethylene or polypropylene.

5. The method of claim 1, wherein contact between the airfoil surface and said flexible planar applicator is maintained by applying pressure in the direction of the airfoil surface to fill the plurality of irregular damage cavities with the liquid repair material.

6. The method of claim 1 further comprising applying a primer coat in at least one of the plurality of irregular damage cavities prior to filling step.

7. The method of claim 1 further comprising applying one or more layers of primer coat over any airfoil surface exposed within said plurality of irregular damage cavities prior to said filling step.

8. The method of claim 1, wherein the liquid repair material includes fillers selected from the group consisting of talc, clays, feldspar, mica, calcium silicate, calcium metasilicate, sodium aluminosilicate, sodium silicate, metal sulfates, calcium sulfate, barium sulfate, sodium sulfate, aluminum sodium sulfate, aluminum sulfate, gypsum, aluminum trihydrate, graphite, metal oxides, calcium oxide, lime, aluminum oxide, titanium dioxide, iron oxide, tin oxide, metal sulfites, metal powders, metal flakes, milled metal fibers, metal nitrides, graphite, carbon nanotubes, milled carbon fibers, silica, quartz, glass beads, glass bubbles, glass fibers, metal-coated glass spheres, metal-coated hollow spheres, buckyballs, electroactive polymers, antimony-doped tin oxide, carbon blacks, coke, micro-balloons and oxides, borides, carbides, nitrides and silicates from the group of compounds containing boron, aluminum, silicon, titanium, tungsten, and zirconium compounds and mixtures of any of the foregoing fillers.

9. The method of claim 1, wherein the liquid repair material includes fillers of organic based powders selected from the group consisting of polycarbonate, polyetherimide, polyester, polyethylene, polysulfone, polystyrene, acrylonitrile-butadiene-styrene block copolymer, Teflon, fluoropolymers, polypropylene, acetal polymers, polyvinyl chloride, polyurethanes, nylon and mixtures of any of the foregoing fillers.