# US 9,520,679 B2 · Earthing arrangement for electrical panel > Agents: this data is available as JSON from the patentgrep API and MCP server — see https://patentgrep.com/llms.txt - Number: US 9,520,679 B2 - Document ID: US9520679B2 - Status: Granted - Kind: B2 - Application number: 14/817,828 - Filed: 2015-08-04 - Published: 2016-02-25 - Granted: 2016-12-13 - Earliest claimed: 2014-08-22 - Assignees: ROLLS-ROYCE plc - Applicants: Rolls-Royce PLC - Inventors: Benjamin George Taylor - Web page: https://patentgrep.com/patent/US9520679B2 ## CPC - H01R 13/648: Protective earth or shield arrangements on coupling devices {, e.g. anti-static shielding} (coaxially arranged shields H01R24/38) - F01D 25/00: Component parts, details, or accessories, not provided for in, or of interest apart from, other groups - F02C 7/00: Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants (controlling F02C9/00) - H01R 13/6581: Shield structure - H01R 13/74: Means for mounting coupling parts in openings of a panel - H01R 43/20: for assembling or disassembling contact members with insulating base, case or sleeve - H01R 4/38: utilising a clamping member acted on by screw or nut (H01R4/50 takes precedence) - H01R 4/64: Connections between or with conductive parts having primarily a non-electric function, e.g. frame, casing, rail - H01R 9/18: Fastening by means of screw or nut - H01R 2201/26: for vehicles - Y02T 50/60: Efficient propulsion technologies, e.g. for aircraft - H01R: ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL ASSOCIATIONS OF A PLURALITY OF MUTUALLY-INSULATED ELECTRICAL CONNECTING ELEMENTS; COUPLING DEVICES; CURRENT COLLECTORS - F01D: NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES (machines or engines for liquids F03; non-positive displacement pumps F04D) - F02C: GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS (construction of turbines F01D; jet-propulsion plants F02K; construction of compressors or fans F04; generating combustion products of high pressure or high velocity F23R; using gas turbines in compression refrigeration plants F25B11/00) - Y02T: CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION ## Abstract A rigid electrical panel has both a flexible printed circuit and an electrically conductive grounding layer embedded therein. The electrically conductive grounding layer is electrically connected to a grounding insert which is also embedded in the rigid material. The grounding insert has a base portion and an exposed portion. The electrically conductive grounding layer is connected to the base portion, and the exposed portion allows the grounding insert, and thus the electrically conductive grounding layer, to be electrically connected to a grounding point, for example on a gas turbine engine. ## Claims ### Claim 1 A rigid electrical panel for an electrical harness comprising: a rigid material; at least one electrical conductor embedded in the rigid material, each electrical conductor being arranged to transfer at least one electrical signal; an electrically conductive grounding layer embedded in the rigid material; and a grounding insert electrically connected to the electrically conductive grounding layer, wherein the grounding insert comprises: a base portion which is embedded in the rigid material and permanently fixed in position by the rigid material; an exposed portion that is accessible from outside the panel to allow the grounding insert to be electrically connected to an external grounding element; an externally threaded portion that extends from the base portion; and the electrically conductive grounding layer is clamped between the base portion and a nut that is threaded onto the externally threaded portion. ### Claim 2 (depends on 1) A rigid electrical panel according to claim 1, wherein the electrically conductive grounding layer is in direct electrical contact with the base portion. ### Claim 3 (depends on 2) A rigid electrical panel according to claim 2, further comprising an electrically conductive washer between the nut and the electrically conductive grounding layer. ### Claim 4 (depends on 3) A rigid electrical panel according to claim 3, wherein: the washer is a thin member comprising a central through-hole having a shape that corresponds to the cross-sectional shape of the grounding insert at the position in which the washer is located; and the central through hole is not axisymmetric, thereby preventing rotation of the washer around the grounding insert. ### Claim 5 (depends on 1) A rigid electrical panel according to claim 1, wherein the base portion is not axisymmetric about an axis about which the threaded portion is formed, thereby preventing rotation of the grounding insert in the rigid material. ### Claim 6 (depends on 1) A rigid electrical panel according to claim 1, wherein the exposed portion comprises an internal thread that is accessible from outside the panel. ### Claim 7 (depends on 6) A rigid electrical panel according to claim 6, wherein the internal thread is formed by a replaceable insert that is provided in an opening of the grounding insert. ### Claim 8 (depends on 1) A rigid electrical panel according to claim 1, wherein: the rigid material comprises a first portion and a second portion; and the electrically conductive grounding layer and the base portion of the grounding insert are positioned between the first portion and the second portion. ### Claim 9 (depends on 8) A rigid electrical panel according to claim 8, wherein the first portion and/or the second portion comprise carbon fibre. ### Claim 10 (depends on 8) A rigid electrical panel according to claim 8, wherein: an electrically insulating layer is provided between the second portion and both the grounding insert and the electrically conductive grounding layer; and, optionally, the electrically insulating layer comprises glass fibre. ### Claim 11 (depends on 1) A gas turbine engine or vehicle having an electrical harness comprising an electrical panel according to claim 1, wherein: the exposed portion of the grounding insert is electrically and mechanically connected to a grounding element, and the grounding element is also electrically connected to a grounding point on the gas turbine engine or vehicle, thereby providing electrical connection between the electrically conductive grounding layer and the grounding point. ### Claim 12 (depends on 11) A gas turbine engine or vehicle according to claim 11, wherein: the grounding element is connected to the exposed portion using a bolt having an external thread (812) that engages an internal thread of the exposed portion; and/or the grounding element comprises a conductive strap. ### Claim 13 (depends on 1) A method of providing a grounded electrical panel to a gas turbine engine or vehicle comprising: mechanically attaching a rigid electrical panel according to claim 1 to the gas turbine engine or vehicle; and electrically connecting a conductive strap between the exposed portion of the grounding insert and a grounding point on the gas turbine engine or vehicle. ### Claim 14 A method of manufacturing a rigid electrical panel comprising: providing a first layer of material; providing an electrically conductive grounding layer and a grounding insert on top of the first layer of material, the electrically conductive grounding layer and the grounding insert being in electrical contact; and providing a second layer of material such that the electrically conductive grounding layer and a base portion of the grounding insert are embedded in or between the first layer and the second layer, wherein: the grounding insert comprises an exposed portion that extends from the base portion and is accessible from outside the panel to allow the grounding insert to be electrically connected to an external grounding element; the grounding insert comprises an externally threaded portion that extends from the base portion; the method further comprises embedding at least one electrical conductor in or between one or both of the first layer and the second layer of material; and the method further comprises clamping the electrically conductive grounding layer between the base portion and a nut that is threaded onto the externally threaded portion of the grounding insert. ### Claim 15 A method of providing a grounded electrical panel to a gas turbine engine or vehicle comprising: mechanically attaching a rigid electrical panel to the gas turbine engine or vehicle, the rigid electrical panel comprising: a rigid material; at least one electrical conductor embedded in the rigid material, each electrical conductor being arranged to transfer at least one electrical signal; an electrically conductive grounding layer embedded in the rigid material; and a grounding insert electrically connected to the electrically conductive grounding layer, wherein the grounding insert comprises: a base portion which is embedded in the rigid material and permanently fixed in position by the rigid material; an exposed portion that is accessible from outside the panel to allow the grounding insert to be electrically connected to an external grounding element, wherein the method further comprises electrically connecting a conductive strap between the exposed portion of the grounding insert and a grounding point on the gas turbine engine or vehicle.