Quick-repair patch and quick repair method for repairing external damage

Abstract

This invention relates to a rapid repair patch and a rapid repair method for repairing external damage. To improve the rapid repair of localized and mechanically unrelated damage (28) in an aircraft component (26), a rapid repair patch (36) is proposed. The rapid repair patch (36) has a layer structure (38) comprising a plastic foil (40) and an adhesive layer (48) on which a lightning protection layer (42) is applied, the adhesive layer being disposed at least on the plastic foil (40). The rapid repair patch (36) can be adhered to the damaged part (28), thereby placing the lightning protection layer (42) in electrical contact with the lightning protection layer of the component (26). The rapid repair patch (36) may have a QR code or RFID tag for storing or retrieving information about the rapid repair patch (36) or the rapid repair performed by means of the rapid repair patch (36).

Description

Technical Field

[0001] This invention relates to a rapid repair patch, preferably for use in aircraft, and a rapid repair method. The invention also relates to a repair assembly and the use of the rapid repair patch. Background Technology

[0002] Civil and military aircraft, helicopters and drones, as well as motor vehicles, ships, and wind turbines (or their rotor blades) are typically made of metal or composite materials. In the event of a lightning strike, repairs may be necessary. The most common type of damage during a lightning strike is merely surface damage, i.e., damage to the paint or possibly some deeper layers. Generally, no significant material damage that could affect the structure occurs here.

[0003] Following such incidents, due to time constraints and limited repair possibilities, these localized and mechanically unrelated damages (scratches, paint peeling, tufting, etc.) have so far been temporarily repaired using so-called high-speed adhesive tape (HST, self-adhesive aluminum foil). HST is inexpensive and available at many airports. Summary of the Invention

[0004] The purpose of this invention is to improve the rapid repair of localized and mechanically unrelated damage, thereby enabling not only operability but also functionality.

[0005] This invention provides a rapid repair patch for repairing localized and mechanically unrelated damage to components, preferably aircraft components, comprising a covering layer and a lightning strike surface protection layer located beneath the covering layer. The rapid repair patch has a layered structure, and the layered structure includes:

[0006] - A plastic foil layer that can be connected in conjunction with the cover material, and which faces away from the damaged area when the quick-repair patch is fastened to the component;

[0007] - A conductive lightning protection layer adapted for lightning protection or electromagnetic interference protection, the conductive lightning protection layer being disposed on the plastic foil layer, and making conductive contact with the lightning strike surface protection portion when the quick repair patch is fastened to the component.

[0008] - A fastening layer adapted to secure the quick-repair patch material to the component, and the fastening layer is disposed on the same side as the conductive lightning protection layer, at least on the plastic foil layer.

[0009] Preferably, the plastic foil layer comprises reinforcing fibers. Preferably, the plastic foil layer comprises a material that weakens radar radiation, preferably absorbing radar radiation. Preferably, the plastic foil layer comprises a conductive material. Preferably, the plastic foil layer comprises a material that weakens, preferably absorbs, UV light or ionizing radiation.

[0010] Preferably, the plastic foil layer is electrically insulated from the lightning protection layer.

[0011] Preferably, the plastic foil layer is designed to be larger in area than the lightning protection layer, wherein the edge region of the plastic foil layer is arranged between the outer contour of the plastic foil layer and the outer contour of the lightning protection layer.

[0012] Preferably, the fastening layer is applied to or disposed at the edge region.

[0013] Preferably, the layer structure has a functional layer. Preferably, the functional layer is arranged on the side of the plastic foil layer opposite to the lightning protection layer. Preferably, the functional layer has reinforcement function, camouflage function, electrostatic discharge protection function and / or protection against radiation (especially UV radiation and / or ionizing radiation).

[0014] Preferably, the layer structure includes a reinforcing layer comprising reinforcing fibers and disposed on a plastic foil layer. Preferably, the layer structure includes a camouflage layer comprising a material that attenuates radar radiation, preferably absorbing radar radiation. Preferably, the layer structure includes an electrostatic discharge (ESD) protection layer comprising a conductive material. Preferably, the layer structure has a connecting layer disposed between the plastic foil layer and the lightning protection layer, connecting the plastic foil layer and the lightning protection layer materials in a compliant manner. Preferably, the layer structure has a radiation protection layer comprising a material that attenuates, preferably absorbs, UV light or ionizing radiation.

[0015] Preferably, the reinforcing layer, camouflage layer, discharge protection layer, and / or radiation protection layer are combined in a common functional layer. Preferably, the reinforcing layer, camouflage layer, discharge protection layer, radiation protection layer, and / or functional layer are arranged on the side of the plastic foil layer opposite to the lightning protection layer.

[0016] Preferably, the layer structure is formed in the order of plastic foil layer, lightning protection layer, and fastening layer.

[0017] Preferably, the layer structure is formed in the following order: a reinforcing layer or camouflage layer or discharge protection layer or radiation protection layer, a plastic foil layer, a lightning protection layer, and a fastening layer. Preferably, the layer structure is formed in the following order: a reinforcing layer or camouflage layer or discharge protection layer or radiation protection layer, a plastic foil layer, a connecting layer, a lightning protection layer, and a fastening layer.

[0018] Preferably, the layer structure is formed in the order of functional layer, plastic foil layer, lightning protection layer, and fastening layer.

[0019] Preferably, the layer structure consists of only the aforementioned layers.

[0020] Preferably, the quick-repair patch includes an information device, preferably a QR code and / or an RFID tag, through which information can be stored or retrieved regarding the quick repair performed using the quick-repair patch. Preferably, this information is stored in or can be retrieved from an RFID tag. Preferably, this information can be stored or retrieved using a computer with the aid of a QR code.

[0021] Preferably, the information device is contained in or placed on a layer of plastic foil.

[0022] This invention provides a rapid repair patch for repairing localized and mechanically unrelated damage to components, preferably aircraft components, comprising a covering layer and a lightning strike surface protection layer located beneath the covering layer. The rapid repair patch has a layered structure, and the layered structure includes:

[0023] - A plastic foil layer that can be connected in conjunction with the cover material, and which faces away from the damaged area when the quick-repair patch is fastened to the component;

[0024] - A conductive lightning protection layer adapted for lightning protection or electromagnetic interference protection, the conductive lightning protection layer being disposed on the plastic foil layer, and making conductive contact with the lightning strike surface protection portion when the quick repair patch is fastened to the component.

[0025] - A fastening layer adapted to secure the quick-repair patch material to the component, and the fastening layer is disposed on the same side as the conductive lightning protection layer, at least on the plastic foil layer.

[0026] - (Optional) Connecting layer, which is disposed between the plastic foil layer and the lightning protection layer and connects the plastic foil layer and the lightning protection layer to each other in a materially compatible manner;

[0027] - (Optional) Functional layer, which is disposed on the side of the plastic foil layer opposite to the lightning protection layer.

[0028] Preferably, the functional layer includes: a reinforcing layer containing reinforcing fibers, and / or a camouflage layer containing a material that reduces radar radiation, preferably absorbing radar radiation, and / or an electrostatic discharge protection layer containing a conductive material.

[0029] Preferably, the plastic foil layer comprises reinforcing fibers. Preferably, the plastic foil layer comprises a material that reduces radar radiation, preferably absorbing radar radiation. Preferably, the plastic foil layer comprises a conductive material.

[0030] Preferably, the plastic foil layer is electrically insulated from the lightning protection layer.

[0031] The present invention provides a repair assembly comprising a component, preferably an aircraft component, and the aforementioned quick-repair patch, wherein the component has a cover layer and a lightning strike surface protection portion located beneath the cover layer, as well as a partial and mechanically unrelated damaged portion, wherein the quick-repair patch covers the damaged portion and is connected to the component material by means of a fastening layer, wherein a plastic foil layer is connected to the cover layer material and faces away from the damaged portion, and wherein a conductive lightning protection layer is disposed between the plastic foil layer and the lightning strike surface protection portion.

[0032] Preferably, the lightning protection layer is electrically connected to the lightning strike surface protection part.

[0033] The present invention provides an aircraft comprising the above-mentioned quick repair patch and / or the above-mentioned repair components, wherein preferably, the components are selected from high-lift devices, flaps, canards, control surfaces, elevators, rudders, ailerons, fuselage components, rotor blades, wing surfaces, engine nacelles, horizontal tail and / or vertical tail.

[0034] This invention provides a rapid repair method for repairing localized and mechanically unrelated damage to components, preferably aircraft components, comprising a covering layer and a lightning strike surface protection layer located beneath the covering layer, wherein the method includes:

[0035] 1. A connection surface for quick repair of the patch is manufactured on the component, and the lightning strike surface protection portion is exposed if necessary;

[0036] 2. Position the aforementioned quick-repair patch at the damaged area; and

[0037] 3. The quick-repair patch is fastened to the connection surface manufactured in step 1 by pressing, thereby connecting the plastic foil layer to the cover material in a mating manner.

[0038] Preferably, the bonding surface and / or the lightning strike protection portion are manufactured by grinding in step 1.

[0039] Preferably, in step 1, the manufacturing process includes cleaning, drying, and / or degreasing the surface areas of the component to provide a connection surface.

[0040] Preferably, the quick-repair patch is positioned in step 2 such that the lightning protection layer can contact the lightning strike surface protection part.

[0041] Preferably, in step 3, the lightning protection layer makes conductive contact with the lightning strike surface protection part.

[0042] The present invention provides the use of the above-mentioned rapid repair patch for repairing localized and mechanically unrelated damaged parts of aircraft components.

[0043] Using the concept described herein, the typical lifespan of a quick repair can be increased to approximately two months. This extends the time until a full repair is required according to the repair manual. By adjusting the plastic foil accordingly, the patch can be fitted to the area to be repaired, making the overall quick repair less noticeable.

[0044] Military aircraft typically have coatings that reduce their radar signature. These coatings, known as hotspots, can be avoided by using quick-repair patches.

[0045] The smart quick surface repair patch (SQSRpatch) proposed here is a multi-layer patch with predefined dimensions and generally has three to four layers.

[0046] Layer 1 is a plastic foil layer. This layer can be colored. The plastic foil layer is, for example, polyurethane foil. The plastic foil can contain markings as information devices, such as in the form of QR codes or RFID tags. Various information about the patch or quick repair (e.g., type, manufacturing date, installation date, and individual identification number) can be stored in the information device. Optionally, the plastic foil layer can contain a reinforcement section made of reinforcing fibers (e.g., fiberglass, Kevlar). These reinforcing fibers are particularly suitable for repairing fuel tanks or combat damage. Optionally, the plastic foil can also have properties that improve camouflage (e.g., substances that absorb or attenuate suitable radar radiation). A colorless overlay can also be applied.

[0047] Layer 2 contains a conductive material. Examples of conductive materials include metal foil, perforated metal foil, extended metal mesh, and graphene. This layer serves as a lightning strike surface protection (LSSP) or electromagnetic interference shielding. Depending on the material, an additional adhesive layer may be provided between Layer 1 and Layer 2 as a connecting layer.

[0048] Layer 3 is, for example, a fastening layer made of an adhesive film. This layer may be applied only to layer 1. This layer may also be additionally disposed on layer 2, wherein a conductive adhesive is preferably used for this purpose.

[0049] In addition, a structure called Layer 1 can be arranged on Layer 1. + The layer can be optionally designed as a reinforcing layer with reinforcing fibers, a camouflage layer with improved camouflage materials, or an electrostatic discharge protection layer. This layer can also be referred to as a functional layer.

[0050] The order of these layers can be adapted to the corresponding application. The shaping of the patch can also be adapted to different situations. Therefore, patches can be designed as squares, rectangles, circles, or ellipses. The same applies to the shape of layer 2. The shape of layer 2 can differ from the overall shape.

[0051] Advantageously, a method similar to HST can be used to place the quick-repair patch. The patch is designed to better prevent peeling. Unlike HST, the patch is watertight, thus improving corrosion resistance. Even if markings or markings on the aircraft are damaged, they can be repaired at a lower cost.

[0052] Compared to HST, patches allow maintenance of minor damage to be postponed until a scheduled D-Check. In individual cases, patches may even be permitted as permanent repairs.

[0053] Correspondingly, the concept presented here allows operators to perform simpler, more durable, and safer repairs to surface damage. The repair patch provides long-lasting protection, reducing, mitigating, or even preventing surface damage associated with lightning strikes. Attached Figure Description

[0054] The embodiments are illustrated in more detail with the aid of schematic drawings. In the drawings:

[0055] Figure 1 An embodiment of the aircraft is shown;

[0056] Figure 2 An example of a rapid repair patch is shown;

[0057] Figure 3A top view of the quick-repair patch is shown;

[0058] Figure 4 It shows having Figure 2 Examples of repair components for rapid repair patches; and

[0059] Figure 5 An example of a patch strip is shown. Detailed Implementation

[0060] First refer to Figure 1 The figure shows an aircraft 10. The aircraft 10 includes a fuselage 12 in a manner known per se, on which a pair of wings 14 are arranged. A vertical tail 16 and a horizontal tail 18 are arranged at the rear of the fuselage 12. Each wing 14 includes a wing surface 20 and a high-lift device 22. Furthermore, the wings 14, the vertical tail 16, and the horizontal tail 18 all have control surfaces 24.

[0061] The aforementioned component 26 may have, for example, a localized and mechanically unrelated damaged portion 28 caused by a lightning strike. Component 26 includes a substrate 30. The substrate 30 may be made of metal or fiber-reinforced plastic. Furthermore, component 26 includes a lightning strike surface protection portion 32. The lightning strike surface protection portion 32 may also be formed by the substrate 30 itself. Additionally, component 26 includes a covering layer 34 disposed on the lightning strike surface protection portion 32.

[0062] Figures 2 to 4 The quick-repair patch 36 is schematically shown, which can be integrated into the repair assembly 37. Figure 4 ) is used to repair damaged parts 28. The thickness of the quick repair patch is approximately 0.1mm to 0.2mm.

[0063] The quick-repair patch 36 includes a layer structure 38. The layer structure 38 has a plastic foil layer 40. The plastic foil layer 40 is preferably made of polyurethane foil. The plastic foil layer 40 may be colored. The plastic foil layer 40 is designed herein to be rectangular. However, the plastic foil layer 40 may also have other shapes, such as circular, elliptical, or square.

[0064] Layer structure 38 includes a conductive lightning protection layer 42 disposed on one side of the plastic foil layer 40. The lightning protection layer 42 comprises a conductive material made of metal or graphene. Accordingly, the lightning protection layer 42 may include stretched metal, perforated metal foil, etc. Here, the lightning protection layer 42 is elliptical. However, the lightning protection layer 42 may also have other shapes, such as circular, rectangular, or square. The lightning protection layer 42 has a smaller area than the plastic foil layer 40. (Viewed in top view...) Figure 3 The plastic foil layer 40 has an edge region 44 disposed between the outline of the plastic foil layer 40 and the lightning protection layer 42.

[0065] A thin connecting layer 46 is arranged along the thickness direction between the plastic foil layer 40 and the lightning protection layer 42, which connects the two layers together.

[0066] Furthermore, the layer structure 38 includes a fastening layer 48 disposed on the plastic foil layer 40. The fastening layer 48 contains an adhesive to securely bond the quick-repair patch 36 to the component 26 material. In a variant, the fastening layer 48 may be bonded to the component 26 material by welding. Preferably, the fastening layer 48 is applied only to or disposed at the edge region 44. Additionally, the fastening layer 48 may also be applied to the lightning protection layer 42. In the region of the lightning protection layer 42, the adhesive is preferably designed to be conductive. Alternatively, a region of the lightning protection layer 42 may be exposed to allow electrical contact between the lightning protection layer 42 and the lightning strike surface protection portion 32.

[0067] In addition, the layer structure 38 may have a functional layer 50. The functional layer 50 is disposed on the surface of the plastic foil layer 40 facing away from the lightning protection layer 42.

[0068] The functional layer 50 may have a reinforcing layer 52 containing reinforcing fibers. Glass fiber or Kevlar may be used as the reinforcing fibers.

[0069] Functional layer 50 may have camouflage layer 54, which contains one or more radar absorption or attenuation additives.

[0070] The functional layer 50 may include an electrostatic discharge protection layer 56, which contains a conductive material.

[0071] The functional layer 50 is preferably designed as a single layer, which integrates a reinforcement layer 52, a camouflage layer 54 and a discharge protection layer 56.

[0072] Alternatively, the functions of the reinforcing layer 52, the camouflage layer 54, or the discharge protection layer 56 can be achieved in any combination within the plastic foil layer.

[0073] The quick-repair patch 36 may also have an information device 58 by means of which information about the quick-repair patch 36 and / or the quick repair performed thereon can be stored or retrieved. This information includes the type and manufacturing date of the quick-repair patch 36, the repair date, the repair location, and any other information (especially the type of technology associated with the quick-repair patch 36 or the repair itself). For example, the information device 58 may be a QR code or an RFID tag. QR codes and RFID tags can be used as references to corresponding information stored in a computer system or computer network, respectively. RFID tags may also be designed to directly contain this information.

[0074] The following will refer to Figure 4The rapid repair process is described in more detail. First, the damaged portion 28 is treated (e.g., by grinding) to provide a smooth, clean, dry, and grease-free bonding surface 60 for the rapid repair patch 36.

[0075] Next, a suitable quick-repair patch 36 is selected and placed on the damaged area 28, ensuring complete coverage. The quick-repair patch 36 is then pressed onto the component 26. Here, the plastic foil layer 40, especially the edge region 44, is pressed against the covering layer 34 and connected to it via the fastening layer 48. Furthermore, the lightning protection layer 42 is pressed against the lightning strike surface protection portion 32, creating electrical contact. If the lightning protection layer 42 is also coated with adhesive, it is also connected to the lightning strike surface protection portion 32 via the same material.

[0076] The following is for reference. Figure 5 The figure illustrates the quick-repair patch 36 as a presentation form of patch strip 62. Here, multiple quick-repair patches 36 are interconnected at separable edge regions 64 (e.g., by means of perforations). Patch strip 62 can be rolled up. The desired quick-repair patch 36 is separated from patch strip 62 before use.

[0077] To improve the rapid repair of localized and mechanically unrelated damage to components 26 of an aircraft, a rapid repair patch 36 is proposed. The rapid repair patch 36 has a layer structure 38 comprising a plastic foil 40 and an adhesive layer, on which a lightning protection layer 42 is applied, and the adhesive layer is disposed at least on the plastic foil 40. The rapid repair patch 36 can be adhered to the damaged portion 28, thereby placing the lightning protection layer 42 in electrical contact with the lightning protection layer of component 26. The rapid repair patch 36 may have a QR code or RFID tag for storing or retrieving information about the rapid repair patch 36 or the rapid repair performed by means of the rapid repair patch 36.

[0078] List of reference numerals in the attached diagram:

[0079] 10 Aircraft

[0080] 12. Fuselage

[0081] 14 Wings

[0082] 16 Vertical tail fin

[0083] 18 Horizontal tail fin

[0084] 20 wing surfaces

[0085] 22 High-lift device

[0086] 24 Control Surfaces

[0087] 26 components

[0088] 28 Damaged parts

[0089] 30 matrix

[0090] 32 Lightning Surface Protection

[0091] 34 Covering layer

[0092] 36 Quick Repair Patch

[0093] 37 Repair Components

[0094] 38-layer structure

[0095] 40 layers of plastic foil

[0096] 42 Lightning Protection Layer

[0097] 44 Edge Area

[0098] 46 Connection Layer

[0099] 48 Fastening layer

[0100] 50 Functional Layer

[0101] 52 Reinforcement Layer

[0102] 54 Camouflage Layer

[0103] 56 Discharge protection layer

[0104] 58 Information Devices

[0105] 60 Connecting surface

[0106] 62 patch strips

[0107] 64. Edge region

Claims

1. A quick-repair patch (36) for repairing a localized and mechanically unrelated damaged portion (28) of a component (26), the component comprising a cover layer (34) and a lightning strike surface protection portion (32) located beneath the cover layer, wherein the quick-repair patch (36) has a layer structure (38), and the layer structure (38) comprises: - A plastic foil layer (40) that can be connected in a way that fits with the material of the cover layer (34), and when the quick repair patch (36) is fastened to the component, the plastic foil layer is away from the damaged part (28); - A conductive lightning protection layer (42) adapted for lightning protection or electromagnetic interference protection, the conductive lightning protection layer being disposed on the plastic foil layer (40), and making conductive contact with the lightning strike surface protection part (32) when the quick repair patch (36) is fastened to the member (26). - Connecting layer (46), which is disposed between the plastic foil layer (40) and the lightning protection layer (42) and connects the plastic foil layer and the lightning protection layer to each other in a material-coordinated manner; - A fastening layer (48) adapted to secure the quick-repair patch (36) material to the component by compression, and the fastening layer is disposed at least on the plastic foil layer (40) and on the same side of the plastic foil layer (40) as the conductive lightning protection layer (42).

2. The rapid repair patch (36) according to claim 1, characterized in that, The component (26) is an aircraft component.

3. The rapid repair patch (36) according to claim 1, characterized in that, The plastic foil layer (40) comprises at least one of the following materials: Reinforcing fibers, Materials that reduce radar radiation The conductive material, wherein the plastic foil layer (40) is electrically insulated from the lightning protection layer (42); Materials that reduce UV light or ionizing radiation.

4. The rapid repair patch (36) according to claim 3, characterized in that, The material that reduces radar radiation is a material that absorbs radar radiation, and / or the material that reduces UV light or ionizing radiation is a material that absorbs UV light or ionizing radiation.

5. The rapid repair patch (36) according to any one of claims 1 to 4, characterized in that, The layer structure (38) has: - A reinforcing layer (52), which comprises reinforcing fibers and is disposed on the plastic foil layer (40); and / or - Camouflage layer (54), said camouflage layer comprising materials that reduce radar radiation; and / or - Electrostatic discharge protection layer (56), the electrostatic discharge protection layer comprising a conductive material; and / or - A radiation protection layer comprising a material that reduces UV light or ionizing radiation.

6. The rapid repair patch (36) according to claim 5, characterized in that, The material that reduces radar radiation is a material that absorbs radar radiation, and / or the material that reduces UV light or ionizing radiation is a material that absorbs UV light or ionizing radiation.

7. The rapid repair patch (36) according to claim 5, characterized in that, At least two of the following layers are combined in a common functional layer (50): the hardening layer (52), the camouflage layer (54), the electrostatic discharge protection layer (56), and the radiation protection layer.

8. The rapid repair patch (36) according to claim 5, characterized in that, The reinforcing layer (52), the camouflage layer (54), the electrostatic discharge protection layer (56), and / or the radiation protection layer are arranged on the side of the plastic foil layer (40) opposite to the lightning protection layer (42).

9. The rapid repair patch (36) according to claim 7, characterized in that, The functional layer (50) is arranged on the side of the plastic foil layer (40) opposite to the lightning protection layer (42).

10. The rapid repair patch (36) according to claim 5, characterized in that, The layer structure (38) is formed in one of the following orders: - Plastic foil layer (40), connecting layer (46), lightning protection layer (42), fastening layer (48); or - Reinforcing layer (52) or camouflage layer (54) or electrostatic discharge protection layer (56) or radiation protection layer, plastic foil layer (40), connecting layer (46), lightning protection layer (42), fastening layer (48).

11. The rapid repair patch (36) according to claim 7, characterized in that, The layer structure (38) is formed in the following order: - Functional layer (50), plastic foil layer (40), connecting layer (46), lightning protection layer (42), fastening layer (48).

12. The rapid repair patch (36) according to any one of claims 1 to 4, characterized in that, The layer structure (38) consists only of the layers mentioned.

13. The rapid repair patch (36) according to any one of claims 1 to 4, characterized in that, The quick-repair patch (36) includes an information device (58) through which information can be stored or retrieved regarding the quick-repair patch (36) and / or the quick repair performed by means of the quick-repair patch (36).

14. The rapid repair patch (36) according to claim 13, characterized in that, The information device (58) is a QR code and / or an RFID tag.

15. A patch strip (62) comprising a plurality of quick-repair patches (36) according to any one of claims 1 to 14, wherein the quick-repair patches (36) are interconnected in a manner that allows them to be individually separable from each other at an edge region (64).

16. The patch strip (62) according to claim 15, characterized in that, The edge region (64) is designed to be perforated for separation.

17. The patch strip (62) according to claim 15 or 16, characterized in that, The patch strip (62) is designed in a rolled shape.

18. A repair component (37), the repair component comprising: The component (26), and the quick-repair patch (36) according to any one of claims 1 to 14, wherein the component (26) has a cover layer (34) and a lightning strike surface protection portion (32) located below the cover layer and a partial and mechanically unrelated damaged portion (28), wherein the quick-repair patch (36) covers the damaged portion (28) and is materially connected to the component (26) by means of the fastening layer (48), wherein the plastic foil layer (40) is materially connected to the cover layer (34) and faces away from the damaged portion (28), wherein the conductive lightning protection layer (42) is disposed between the plastic foil layer (40) and the lightning strike surface protection portion (32).

19. The repair component (37) according to claim 18, characterized in that, The component (26) is an aircraft component.

20. An aircraft (10) comprising a quick-repair patch (36) according to any one of claims 1 to 14 and / or a repair assembly (37) according to claim 18 or 19.

21. The aircraft (10) according to claim 20, characterized in that, The component (26) is selected from high lift devices, flaps, canards, control surfaces, elevators, rudders, ailerons, fuselage components, rotor blades, wing surfaces, engine nacelles, horizontal tail and / or vertical tail.

22. A rapid repair method for repairing localized and mechanically unrelated damage (28) of a component (26), the component comprising a covering layer (34) and a lightning strike surface protection portion (32) located beneath the covering layer, wherein the method comprises: 13.1 A connection surface (60) for quick repair patch (36) is formed on the component (26) and the lightning strike surface protection part (32) is exposed if necessary; 13.2 Positioning the quick-repair patch (36) according to any one of claims 1 to 14 at the damaged portion (28); and 13.3 The quick repair patch (36) is fastened to the connecting surface (60) manufactured in step 13.1 by compression, thereby connecting the plastic foil layer (40) with the cover layer (34) material and bringing the lightning protection layer (42) into contact with the lightning strike surface protection part (32).

23. The rapid repair method according to claim 22, characterized in that, The component (26) is an aircraft component.

24. The rapid repair method according to claim 22, characterized in that, In step 13.3, the lightning protection layer (42) is brought into conductive contact with the lightning strike surface protection part (32).

25. The rapid repair method according to claim 22, characterized in that, In step 13.1, the connection surface (60) is manufactured and / or the lightning strike surface protection part (32) is exposed by grinding.

26. Use of the quick-repair patch (36) according to any one of claims 1 to 14 for repairing localized and mechanically unrelated damage (28) of an aircraft component.

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