EP2685565B1

EP2685565B1 - Electrical connectors

Info

Publication number: EP2685565B1
Application number: EP13158531.7A
Authority: EP
Inventors: Matthew Peter Fitt; David C Dowdell
Original assignee: Rolls Royce PLC
Current assignee: Rolls Royce PLC
Priority date: 2012-07-10
Filing date: 2013-03-11
Publication date: 2016-09-07
Anticipated expiration: 2033-03-11
Also published as: EP2685565A1

Description

The present invention relates to electrical connectors. In particular, aspects of the invention relate to electrical connectors in rigid electrical rafts used to distribute electrical signals around a gas turbine engine.
A typical gas turbine engine has a substantial number of electrical components which serve, for example, to sense operating parameters of the engine and/or to control actuators which operate devices in the engine. Such devices may, for example, control fuel flow, variable vanes and air bleed valves. The actuators may themselves be electrically powered, although some may be pneumatically or hydraulically powered, but controlled by electrical signals.
Electrical power, and signals to and from the individual electrical components, is commonly transmitted along conductors. Conventionally, such conductors may be in the form of wires and/or cables which are assembled together in a harness. In such a conventional harness, each wire may be surrounded by an insulating sleeve, which may be braided or have a braided cover.
By way of example, Figure 1 of the accompanying drawings shows a typical gas turbine engine including two conventional wiring harnesses 102, 104, each provided with a respective connector component 106, 108 for connection to circuitry, which may be for example accommodated within the airframe of an aircraft in which the engine is installed.
The harnesses 102, 104 are assembled from individual wires and cables which are held together over at least part of their lengths by suitable sleeving and/or braiding. Individual wires and cables, for example those indicated at 110, emerge from the sleeving or braiding to terminate at plug or socket connector components 112 for cooperation with complementary socket or plug connector components 114 on, or connected to, the respective electrical components.
Thus the conventional electrical harness has to be provided with plug or socket connector components 112 for connection to other electrical components, such as electrical units such as engine control units. These conventional plug or socket connector components add weight and complexity to the electrical harnesses. Furthermore, the conventional plug or socket connectors are exposed to the engine environment. Thus, the conventional plug or socket connectors may be exposed to, for example, high temperatures and/or vibrations.
The exposed connectors therefore need to be particularly robust in order to survive this environment. This means that the conventional exposed connectors are bulky and heavy. Even such bulky and heavy connectors may still be susceptible to damage and/or becoming loose, for example due to engine vibration.
Each conventional harness 102, 104 comprises a multitude of insulated wires and cables. This makes the conventional harness itself bulky, heavy and difficult to manipulate. The conventional harnesses occupy significant space within a gas turbine engine (for example within the nacelle of a gas turbine engine), and thus may compromise the design of the aircraft, for example the size and/or weight and/or shape of the nacelle.
Conventional harnesses comprise a large number of components, including various individual wires and/or bundles of wires, supporting components (such as brackets or cables) and electrical and/or mechanical connectors. This can make the assembly process complicated (and thus susceptible to errors) and/or time consuming. Disassembly of the conventional harnesses (for example removal of the conventional harnesses from a gas turbine engine during maintenance) may also be complicated and/or time consuming. Thus, in many maintenance (or repair or overhaul) procedures on a gas turbine engine, removal and subsequent refitting of the conventional electrical harness may account for a very significant portion of the operation time and/or account for a significant proportion of the potential assembly errors.
The electrical conductors in the conventional harnesses may be susceptible to mechanical damage. For example, mechanical damage may occur during installation (for example through accidental piercing of the protective sleeves/braiding) and/or during service (for example due to vibration). In order to reduce the likelihood of damage to the conductors in a conventional harness, the protective sleeves/braiding may need to be further reinforced, adding still further weight and reducing the ease with which they can be manipulated. Similarly, the exposed electrical connectors used to connect one conductor to another conductor or conductors to electrical units may be susceptible to damage and/or may add significant weight to the engine.
US2010/0261365 discloses a connector assembly having guide projections that project out from an outer peripheral surface of a wire-deriving tube of a wire-side housing. The guide projections guide a shielding tube of a shielding shell in position with respect to the wire-deriving tube. In fixing the shielding shell to a connector-mounting member, an inner peripheral surface of the shielding tube contacts the guide projections of the wire-side housing to fit the shielding shell on the wire-side housing without dislocation.
EP 1762714 discloses a connector for incorporation into a heater system for inlet struts that includes a body having a tapered forward end and an opposite rear end. A plurality of forward electrical terminals are formed on the outer surface of the tapered end. A plurality of rearward electrical terminals are formed on the rear end of the body. The rearward electrical terminals are in electrical connection with the forward electrical terminals. The forward electrical terminals on the tapered end are in electrical contact with a plurality of electrical contacts connected to heating elements formed in a heating mat. The heating mat entirely envelops the connector. The heater mat is formed within a substantially rigid outer shell.
US 6,752,632 discloses a pin connector including a housing having a central orifice and an annular skirt laterally projecting therefrom. The skirt is bondable over a structurally integrated pad with integral wiring array. An array of compliant pins are insertable within holes in the pad. The central orifice is adapted to receive a mating connector.
In a first aspect, the present invention provides a part of an electrical harness of a gas turbine engine (which may be referred to herein as an electrical raft) comprising:

a rigid material having multiple electrical conductors embedded therein so as to be surrounded by the rigid material and fixed in position by the rigid material, and
an electrical connector having a first set of electrical contacts connected to at least one of the electrical conductors, a second set of electrical contacts for electrical connection to another component, and a housing having a first end and a second end , the first set of electrical contacts being at the first end and the second set of electrical contacts being at the second end;
wherein:
- the first end of the housing is at least partly embedded in the rigid material, and the second end of the housing is accessible from outside the electrical raft, thereby allowing the electrical raft to be electrically connected to said other component, and
- the electrical connector further has a back-shell which sealingly encloses the first end of the housing and the first set of electrical contacts to prevent ingress of contaminants into the connector.

The electrical raft (and/or electrical raft assembly described below) may be a part of any electrical system. For example, an electrical raft/electrical raft assembly may form part of a gas turbine engine. In this case, the electrical raft/electrical raft assembly may form part of an electrical harness for a gas turbine engine, and thus may be referred to as an electrical harness raft. The electrical conductors embedded in the rigid material may be used to transfer electrical signals around a gas turbine engine. Transferring electrical signals using the embedded electrical system of the rigid raft can provide a number of advantages over transferring electrical signals using a conventional harness. For example, during assembly and in use, such rafts may provide greater protection to their electrical conductors than conventional harnesses. For example, the rigid material in which the conductors are embedded may provide greater protection (for example greater mechanical protection) to the embedded conductors, for example due to being resistant to breaking and/or snapping and/or piercing and/or puncturing. Purely by way of example, the use of electrical rafts may reduce, or substantially eliminate, the chance of foreign bodies coming into contact with the electrical conductors, for example through fluid ingress. The electrical raft(s) may provide improved protection to the electrical conductors during manufacture/assembly of the raft/gas turbine installation, and/or during service/operation/maintenance of the gas turbine engine. This may result in lower maintenance costs, for example due to fewer damaged components requiring replacement/repair and/or due to the possibility of extending time intervals (or service intervals) between inspecting the electrical system, for example compared with a system using only conventional harnesses. Further, the use of such rafts may significantly reduce the build and maintenance times of an engine, and/or reduce the possibility of errors occurring during such procedures. The rafts can also provide weight and size advantages over conventional harnesses.
In addition, by embedding the housing of the connector in the rigid material of the raft, it is possible to integrate the connector with the raft. The connector, an particularly the first set of electrical contacts, can be well protected by the rigid material of the raft, and thus may be more reliable and less susceptible to damage, for example than connectors in a conventional harness. Furthermore, because the connector may be assembled with the raft, its position can be determined accurately, reducing error during connection to other units. In particular, by embedding the housing, the first set of electrical contacts may thereby be contained within the electrical raft, and this may help to protect them from damage and/or degradation. The back-shell can advantageously prevent ingress of contaminants into the connector during manufacture or use of the raft. During manufacture, such contaminants can interfere with the positions of the electrical contacts, whereby the mated contacts may be unable to move sufficiently to ensure good electrical contact. During use, such contaminants can interfere with the proper electrical functioning of the connector, e.g. by preventing electrical contacts or producing short-circuits.
The housing may be a convenient arrangement for providing the second set of electrical contacts in a position that allows them to be connectable to another component, and the first set of electrical contacts at a position that allows them to be connected to one or more of the embedded electrical conductors. The housing may allow the connector to be easily handled and positioned, for example during assembly/manufacture, and/or may provide protection to the internal parts of the connector (which may, for example, include components for electrically connecting the first set of electrical contacts with the second set of electrical contacts).
In a second aspect, the present invention provides an electrical raft assembly comprising; an electrical raft according to the first aspect, and a further electrical component comprising a complimentary set of electrical contacts that correspond to the second set of electrical contacts, wherein the electrical raft and the further electrical component are in electrical connection through the second set of electrical contacts and the complimentary set of electrical contacts.
The complimentary set of electrical contacts may be in the form of a plug or socket. The second set of electrical contacts of the electrical raft may thus be in the form of the other of a plug and socket. The further electrical component may be any sort of electrical component, for example a set of electrical conductors that link the electrical raft to a still further electrical component. Such a set of electrical conductors may be, for example, in the form of one or more wires, which may be bundled together and/or which may be sheathed/braided, and/or in the form of an FPC. Additionally or alternatively, the further electrical component may be, for example, an electrical unit. Such an electrical unit may be mechanically fixed/mounted to the surface of the electrical raft, for example to the first major surface. The mechanical fixing may be independent of the electrical connection.
In a third aspect, the present invention provides a gas turbine engine or gas turbine engine installation, having the raft according to the first aspect or the raft assembly of the second aspect. For example, the electrical rigid raft or electrical raft assembly may be a first engine installation component, and the gas turbine engine or gas turbine engine installation may further comprise a second engine installation component having electrical conductors. At least one flexible cable can then connect between the electrical raft or electrical raft assembly and the second engine installation component so as to electrically connect electrical conductors of the electrical raft or electrical raft assembly with electrical conductors of the second engine installation component.
In a fourth aspect, the present invention provides a method of manufacturing (including assembling, repairing, reassembling and/or overhauling) a gas turbine engine comprising: attaching an electrical raft according to the first aspect (or an electrical raft assembly according to the second aspect) to the engine, and electrically connecting a further electrical component of the gas turbine engine to the electrical raft (or electrical raft assembly) by connecting the second set of contacts to a complimentary set of contacts of the further electrical component. The further electrical component may be as described elsewhere herein, for example a flexible cable (such as a FPC), or an ECU, such as en electronic engine controller (EEC), or Engine Health Monitoring Unit (EMU).
Further optional features of the invention will now be set out. These are applicable singly or in any combination with any aspect of the invention.
The rigid material may be any suitable material, examples of which are provided herein. For example, the rigid material may be a rigid polymer matrix composite material. The back-shell can then advantageously prevent ingress of the polymer as a fouling contaminant into the connector during manufacture of the raft.
The rigid material may contain layers of continuous reinforcing fibres, as discussed below.
The electrical connector may have an elastomeric seal between the housing and the back-shell. Such a seal can be particularly effective at preventing ingress of polymer during manufacture. Indeed, it is particularly desirable to prevent any such ingress when such a seal is used, as ingressing polymer can reduce compliance at the seal, reducing sealing effectiveness and allowing other contaminants (e.g. oil or fuel) to enter the connector during use.
The housing and the back-shell may be electrically conductive and may be in electrical contact with each other to provide electro-magnetic shielding of the connector. For example, the housing and the back-shell can be formed of metal. However another option is to form the housing and the back-shell of conductive or plated composite, plastic or ceramic, which may provide weight advantages.
At least some of the electrical conductors embedded in the electrical raft may be electrical wires. The electrical wires may be provided with a protective and/or insulating sheath/braiding. As such, individual wires may be laid into (or embedded in) the electrical raft, and each wire may be used to transfer one or more electrical signals through the raft and around an engine. The electrical conductors (which may be electrical wires) may be permanently fixed to (and thus permanently in electrical connection with) the first set of electrical contacts. This may mean that the embedded electrical conductors feed directly into the first set of electrical contacts. In that case, the first set of electrical contacts may be defined as being the portion(s) of the electrical connector into which the electrical wires feed.
At least some of the electrical conductors may be provided in a flexible printed circuit (FPC) in the form of electrical tracks formed in a flexible substrate. The flexible printed circuit may be flexible before being embedded in the rigid material. The electrical tracks may then terminate in openings in a flexible printed circuit connector, and the first set of electrical contacts can comprise pins that are received in respective openings so as to electrically connect the electrical tracks to the electrical connector. The FPC may be provided with a connector to connect the electrical tracks to the electrical connector. The electrical tracks may terminate in conductive openings in such a connector. Such a connector may be referred to as a lollipop connector, and may be generally planar. The first set of electrical contacts may comprise pins that are received in respective openings so as to electrically connect the electrical tracks to the electrical connector. This may be a particularly compact and/or lightweight and/or robust arrangement for connecting electrical tracks in an embedded flexible printed circuit to the electrical connector.
Providing the electrical conductors as tracks in a flexible printed circuit may allow the size of the resulting electrical raft to be reduced further and/or substantially minimized. For example, many different electrical conductors may be laid into a flexible printed circuit in close proximity, thereby providing a compact structure. The flexible substrate of a single flexible printed circuit may provide electrical and/or mechanical protection/isolation to a large number of electrical conductors.
Any given electrical raft may be provided with one or more electrical wires embedded therein (which may be sheathed) and/or one or more flexible printed circuits embedded therein. As such, a given electrical raft may have wires and flexible printed circuits laid therein.
It will be appreciated that the embedded electrical conductors (whether they are provided as embedded electrical wires or as conductive tracks in a flexible printed circuit embedded in the rigid material) may be described as being fixed in position by the rigid material, for example relative to the rest of the electrical harness raft. It will also be appreciated that the embedded electrical conductors may be said to be surrounded by the rigid material and/or buried in the rigid material and/or integral with (or integrated into) the rigid material.
The electrical raft may have a (first) major surface from which the second end of the housing is accessible. The electrical raft may have a second major surface which is separated by a thickness from the first major surface. The second major surface may be substantially parallel to the first major surface. The electrical conductors embedded in the raft may generally extend in a direction that is substantially parallel to the first and/or second major surface (except, for example, in the region of the first set of electrical contacts where they turn through angles as discussed below).
The electrical connector may have a longitudinal axis which extends from the first end to the second end of the housing (for example, the housing may be an elongate housing having such a longitudinal axis). The connector can then be mounted in the rigid material such that the longitudinal axis forms a mounting angle in the range of from 20 degrees and 70 degrees with the first major surface. Such a mounting angle may allow the second set of electrical contacts to be readily accessible from the electrical raft (for example from the first major surface of the electrical raft), whilst ensuring that electrical conductors leading into the connector (for example the conductors embedded in the raft) and/or out of the connector (for example electrical conductors that may form part of a component connected to the connector) do not have to bend through a large angle and/or a tight corner (small bend radius). This may reduce the stress on the conductors and/or the connectors, for example mechanical stress that may otherwise be induced due to tight bending of the conductors. In turn, this may improve the reliability and/or service life of the conductors, and thus the electrical raft. The mounting angle may be in the range of from 30 degrees to 60 degrees, in the range of from 40 degrees to 50 degrees, or on the order of 45 degrees. This may help to further improve the reliability and/or service life of the conductors, and thus the electrical raft.
A mounting angle in the ranges set out herein may also provide the advantage of reducing the overall thickness of the electrical raft including the embedded connector. For example, such a mounting angle may enable the electrical connector to protrude less, or not at all, from the first major surface of the electrical raft, if desired.
The second set of electrical contacts may be aligned with the mounting angle of the electrical connector. This may facilitate reliable connection with complimentary electrical contacts of a further electrical component that may be attached to the electrical raft via the connector. Indeed, more generally, providing the electrical connector at the mounting angle means that electrical conductors that form a part of such a further electrical component may be manipulated so as to extend in a direction that is substantially parallel with the first major surface of the electrical raft without having to turn through a tight bend radius and/or large angle. This may help to reduce the stress that those conductors are subjected to, and thus may help to reduce failure rate and/or allow less robust (and thus potentially heavy/expensive) conductors/protection to be used.
Similarly, the first set of electrical contacts may be aligned with the mounting angle of the electrical connector. This may help to ensure that the electrical conductors embedded in the raft that are connected through the first set of electrical contacts do not have to turn through a tight bend radius, and thus may help to ensure reliability. In this regard, if, for example, the electrical conductors were forced to turn through a large angle (for example greater than that required by the mounting angle), this would also have to be achieved within the thickness of the electrical raft, thus requiring a smaller bend radius than that required for the conductors to turn through the mounting angles described herein.
The electrical conductors provided in the flexible printed circuit may turn through an angle equal to 90 degrees minus the mounting angle before being connected to the first set of electrical contacts. For example, the electrical conductors provided in the flexible printed circuit may turn through an angle equal to 90 degrees minus the mounting angle before terminating in the openings in the flexible printed circuit connector. Thus, the flexible printed circuit and the electrical conductors laid therein may not experience excessive mechanical stress as they turn to connect with the first set of electrical contacts.
The electrical raft may further have a location feature, such as a flange, so as to mount the electrical connector at the correct orientation relative to the first major surface. The location feature may be an integral part of the electrical connector. The location feature may be in contact with the rigid raft material (for example embedded in the rigid raft material). In other words, the location feature may ensure that the electrical connector is at the desired mounting angle in the electrical raft assembly.
The electrical raft may comprise an earthing (or grounding) mesh. The earthing mesh may be referred to as an electrically conductive screen layer, and may or may not take the form of a mesh. The earthing mesh may provide electrical screening to the electrical conductors embedded in the raft. For example, the earthing mesh may provide electrical screening against electrical interference and/or from electrical surges, for example from lightning strikes. The earthing mesh may be grounded, for example to a gas turbine engine to which the electrical raft may be provided. The earthing mesh may take any suitable form/arrangement. For example, it may be a mesh-type construction (meaning that it may be a surface with holes provided therein) and/or may be metallic. The earthing mesh may be embedded in the rigid material (for example it may be provided during manufacture). Alternatively or additionally, a fixture may be provided to hold the earthing mesh in position. The earthing mesh may be connected (electrically and/or mechanically) to the location feature, where both are present.
In general, the use of one or more electrical rafts/electrical raft assemblies may significantly reduce build time of an engine. For example, use of electrical rafts/electrical raft assemblies may significantly reduce the part count involved in engine assembly compared with a conventional harness arrangement. The number and/or complexity of the operations required to assemble an engine (for example to assemble/install the electrical system (or network) and/or other peripheral components, which may be referred to in general as engine dressing) may be reduced. For example, rather than having to install/assemble a great number of wires and/or wiring looms together on the engine installation, it may only be necessary to attach a relatively small number of electrical rafts/electrical raft assemblies, which themselves may be straightforward to handle, position, secure and connect. As described herein, electrical rafts may be conveniently and easily connected to each other and/or to other electrical components using flexible cable(s) (which may be FPCs). Thus, use of electrical raft assemblies in a gas turbine installation may reduce assembly time and/or reduce the possibility of errors occurring during assembly.
Use of electrical raft assemblies may provide significant advantages during maintenance, such as repair and overhaul. As discussed above, the electrical rafts may be particularly quick and straightforward to assemble. The same advantages discussed above in relation to assembly apply to disassembly/removal from the gas turbine engine. Thus, any repair/overhaul that requires removal of at least a part of the electrical harness may be simplified and/or speeded up through use of electrical rafts as at least a part of the electrical harness, for example compared with conventional harnesses. Use of electrical rafts (for example as part of one or more electrical raft assemblies) may allow maintenance procedures to be advantageously adapted. For example, some maintenance procedures may only require access to a certain portion of the gas turbine engine that only requires a part of the harness to be removed. It may be difficult and/or time consuming, or not even possible, to only remove the required part of a conventional harness from a gas turbine engine. However, it may be relatively straightforward to only remove the relevant electrical raft, for example by simply disconnecting it from the engine and any other electrical rafts/components to which it is connected. Decreasing maintenance times has the advantage of, for example, reducing out-of service times (for example off-wing times for engines that are used on aircraft).
The build/assembly times may be additionally or alternatively reduced by pre-assembling and/or pre-testing individual and/or combinations of electrical rafts and/or electrical raft assemblies prior to engine assembly. This may allow the electrical and/or mechanical operation of the electrical rafts to be proven before installation, thereby reducing/eliminating the testing required during engine installation.
The electrical rafts/electrical raft assemblies may be a particularly lightweight solution for transferring electrical signals around an engine. For example, an electrical raft may be lighter, for example significantly lighter, than a conventional harness required to transmit a given number of electrical signals. A plurality of conductors may be embedded in a single electrical raft, whereas in a conventional arrangement a large number of heavy, bulky wires, usually with insulating sleeves, would be required. The reduced weight may be particularly advantageous, for example, when used on gas turbine engines on aircraft.
Electrical rafts may be more easily packaged and/or more compact, for example than conventional harnesses. Providing an electrical connector with a back-shell as described herein may allow a still further reduction in the combined size of an electrical raft connected with other components. The electrical rafts can be made into a very wide range of shapes as desired. This may be achieved, for example, by manufacturing the electrical rafts using a mould conforming to the desired shape. As such, each electrical raft may be shaped, for example, to turn through a tighter corner (or smaller bend radius) than a conventional harness. The electrical rafts may thus provide a particularly compact solution for transferring electrical signals around a gas turbine engine. The electrical rafts may be readily shaped to conform to neighbouring components/regions of a gas turbine engine, for example components/regions to which the particular electrical raft assembly is attached, such as a fan casing or a core casing.
The electrical raft(s) may provide improved protection to the electrical conductors during manufacture/assembly of the raft/gas turbine installation, and/or during service/operation/maintenance of the gas turbine engine. This may result in lower maintenance costs, for example due to fewer damaged components requiring replacement/repair and/or due to the possibility of extending time intervals (or service intervals) between inspecting the electrical system, for example compared with a system using only conventional harnesses.
As mentioned above, any suitable material may be used for the rigid material of the electrical raft. For example, the rigid material may be a rigid composite material, for example an organic matrix composite. Such a rigid composite material may be particularly stiff and/or lightweight. Thus, a rigid composite raft may be used that has suitable mechanical properties, whilst being thin and lightweight, for example compared with some other materials. The rigid composite material may comprise any suitable combination of resin and fibre as desired for a particular application. For example, any of the resins and/or fibres described herein may be used to produce a rigid composite material for the electrical raft. Any suitable fibres may be used, for example carbon fibres, glass fibres, aramid fibres, and/or para-aramid fibres. The fibres may be of any type, such as woven and/or chopped. Any suitable resin may be used, for example epoxy, BMI (bismaleimide), PEEK (polyetheretherketone), PTFE (polytetraflouroethylene), PAEK (polyaryletherketone), polyurethane, and/or polyamides (such as nylon).
The electrical raft (or electrical raft assembly) may be at least a part of an electrical harness for a gas turbine engine, and thus may be referred to herein as an electrical harness raft (or electrical harness raft assembly).
An electrical raft (or electrical raft assembly) may comprise a fluid passage. Such a fluid passage may be embedded therein and/or otherwise provided thereto. The fluid passage may be part of a fluid system, such as a gas (for example pneumatic or cooling gas/air) and/or liquid (for example a fuel, hydraulic and/or lubricant liquid).
There is also provided a method of assembling an electrical raft assembly and/or a gas turbine engine. The method comprises preparing an electrical raft assembly as described above and elsewhere herein. The method also comprises electrically and mechanically connecting the prepared electrical raft assembly to the rest of the apparatus/gas turbine engine.
Thus, there is provided a gas turbine engine or gas turbine engine installation (for example for an airframe) comprising an electrical raft and/or an electrical raft assembly as described above and elsewhere herein. For example, at least one electrical raft and/or electrical raft assembly may be used as part of an electrical harness for transferring electrical signals around the engine, in the form of electrical harness raft(s) and/or electrical harness raft assemblies.
The electrical raft may comprise one or more electrical connectors or sockets, which may be electrically connected to at least one of the embedded electrical conductors. The electrical connector or socket may allow electrical connection of the electrical raft to other electrical components, for example to other electrical rafts (either directly or indirectly, via an electrical cable or lead) or to electrical units (again, either directly or indirectly, via an electrical cable or lead). Such an electrical connector or socket may take any suitable form, and may be at least partially embedded in the rigid electrical raft as described herein.
The electrical raft assembly may be a first engine installation component of a gas turbine engine. The gas turbine engine may further comprise a second engine installation component having electrical conductors. The gas turbine engine may further comprise at least one flexible cable (which may be, for example, an FPC and/or at least one electrically conductive wire) connected between the electrical raft assembly and the second engine installation component so as to electrically connect electrical conductors of the electrical raft assembly with electrical conductors of the second engine installation component.
The second engine installation component may be, for example, another electrical raft/electrical raft assembly, or an ECU, such as an EMU or EEC. Additionally or alternatively, the second engine installation component may be a further electrical raft or electrical raft assembly.
The environment of a gas turbine engine during operation may be particularly severe, with, for example, high levels of vibration and/or differential expansion between components as the temperature changes through operation and as the components move relative to each other. Providing at least one flexible cable to connect an electrical raft assembly to another component may allow the electrical rafts and/or components to accommodate vibration and/or relative movement, for example of the component(s)/assemblies to which they are attached/mounted during use. For example, the flexible cable(s) (where present) used to electrically connect electrical raft assemblies to other component(s) may have sufficient length to accommodate such vibration and/or movement during use.
For example, providing separate (for example more than one) electrical raft assemblies and connecting at least some (for example at least two) of them together using at least one flexible cable may allow the electrical rafts to accommodate vibration and/or relative movement of the component(s)/assemblies to which they are attached/mounted during use.
The electrical signals transferred by the conductors in the electrical raft, and around the engine using the electrical rafts/raft assemblies may take any form. For example, the electrical signals may include, by way of non-limitative example, electrical power and/or electrical control/communication signals and/or any other type of transmission through an electrical conductor. Transmission of signals around the engine may mean transmission of signals between (to and/or from) any number of components/systems in the engine and/or components/system of a structure (such as an airframe) to which the gas turbine engine is (or is configured to be) connected/installed in. In other words, an electrical raft may be used to transfer/communicate any possible combination of electrical signals in any part of a gas turbine engine installation or a related (for example electrically and/or mechanically connected) structure/component/system.
An electrical raft or raft assembly may be provided in any suitable location/position of the gas turbine engine, for example to a mounting structure at any suitable location. For example, the gas turbine engine may comprise a bypass flow duct formed between an engine core and an engine fan casing (the gas turbine engine may be a turbofan engine, for example); and the electrical raft assembly may form at least a part of a radially extending splitter (which may be referred to as a bifurcation) that extends across the bypass flow duct. In this way, an electrical raft (which may be referred to as a splitter electrical raft) may provide an electrical connection between a fan casing and an engine core. By way of further example, electrical rafts or electrical raft assemblies may be mounted to, for example, the engine core (including the engine core casing) and/or the fan case/nacelle.
An electrical raft may be provided with (for example have embedded therein) at least one additional electrical socket, which may or may not be provided with a back-shell as described herein. The or each additional electrical socket may be in electrical contact with at least one of the respective electrical conductors embedded in the rigid material and may have terminals for connection with a complimentary connector. Such an additional electrical socket may take any suitable form, and may allow the electrical raft to be easily connected to other components, such as flexible cables and/or other electrical rafts.
An electrical raft assembly may comprise (for example have mounted thereon) other components/systems of the gas turbine engine, for example ancillary, auxiliary or control components. Such other components/systems may be provided to an electrical raft in any suitable manner. For example, such other components/systems may be mounted on one or more electrical rafts. Thus, a surface of an electrical raft may be used as a mounting surface for other gas turbine engine components/systems, such as ancillary/auxiliary components/systems.
For example, an electrical unit may be mounted on an electrical raft. The electrical unit may be any sort of electrical unit, for example one that may be provided to a gas turbine engine. For example, the electrical unit may be any type of electronic control unit (ECU), such as an Electronic Engine Controller (EEC) and an Engine Health Monitoring Unit (EMU). At least one (i.e. one or more) electrical unit may be attached to an electrical raft. Such an electrical raft assembly may be a particularly convenient, lightweight and/or compact way of providing (for example attaching, fixing or mounting) an electrical unit to a turbine engine. For example, the electrical unit and the electrical raft may be assembled together (mechanically and/or electrically) before being installed on the gas turbine engine, as described elsewhere herein.
An electrical raft may be provided with at least one mount on which other components (for example auxiliary/ancillary components/systems) of the gas turbine engine are (or may be) mounted. The mount may be a bracket, for example a bespoke bracket for the component/system mounted thereon or a conventional/standard bracket. The electrical raft may provide a stable, regular and convenient platform on which to mount the various systems/components. The combination of the installed electrical raft assembly with components/systems mounted thereon may be much more compact and/or straightforward to assemble and/or have a greatly reduced number of component parts, for example compared with the corresponding conventional electrical harness and separately mounted components/systems.
The mounts may be used to attach any component/system to an electrical raft (and thus to the engine) as required. For example, fluid pipes for transferring fluid around the engine may be mounted to the electrical rafts (for example mechanically mounted using a bracket), and thus to the engine. The fluid pipes may be arranged to carry any fluid as desired, including gas (such as cooling air, sealing air, and/or muscle air (for example for pneumatic systems)) and/or liquid (such as fuel, water, oil and/or hydraulic fluid). Of course, more than one set of fluid pipes, for example for carrying different or the same fluids, may be mounted on the same electrical raft.
Examples of other components/systems that may be at least in part mounted to an electrical raft include, by way of non-limitative example: fire detectors and/or fire detection elements; thermocouples for measuring air temperature (for example within a particular engine zone); vibration monitoring processing equipment (for example a signal processing component/box containing electronics used to process a vibration signal that may be measured elsewhere in the engine); equipment for measuring fluid quality (for example a probe for oil debris monitoring may be provided to one or more pipes mounted to the raft, and/or a signal processing box for processing the oil quality measurements may be mounted on the box); and pressure sensors and/or signal processing equipment, for example for fluid pipes mounted on the rafts. At least some of these components/systems may be electrically connected to the electrical conductors in the electrical raft using the electrical connector(s) of the electrical rafts. At least one other component/system may be at least partially embedded in an electrical raft. For example, at least one fluid passage may be at least partially embedded in an electrical raft. Such a fluid passage may take the form of a fluid pipe embedded in the electrical raft, or a conduit formed in the electrical raft during manufacture.
At least one electrical raft or raft assembly may be connected/attached/mounted to the gas turbine engine using at least one anti-vibration mount. Using an anti-vibration mount to attach an electrical raft/assembly to a gas turbine engine for example may reduce (or substantially eliminate) the amount (for example the amplitude and/or the number/range of frequencies) of vibration being passed to the electrical raft from the gas turbine engine, for example during use. This may help to prolong the life of the electrical raft. Furthermore, any other components that may be attached to the electrical raft (as discussed above and elsewhere herein) may also benefit from being mounted to the gas turbine engine via the anti-vibration mounts, through being mounted on the electrical raft. For an electrical raft assembly, the reduced vibration may help to preserve the electrical contact between the electrical raft and any electrical unit connected thereto. As such, any components (such as an electrical unit mounted to the electrical raft) that would conventionally be mounted directly to the gas turbine engine and require at least a degree of vibration isolation no longer require their own dedicated anti-vibration mount. Thus, the total number of anti-vibration mounts that are required to assemble an engine may be reduced. This may reduce the number of parts required and/or the time taken to assemble an engine or engine installation and/or reduce the total assembled weight and/or reduce the likelihood of errors occurring during assembly.
Furthermore, components that are conventionally mounted to an engine without anti-vibration mounts (for example because of the weight and/or cost penalty), but which are now mounted to an electrical raft (for example to a mounting surface of the electrical raft), may benefit from vibration isolation without any weight/cost/assembly time penalty. This may reduce the possibility of damage occurring to such components and/or increase their service life. Such components may include, for example, ignitor boxes (used to provide high voltage power to engine ignitors), and pressure sensors/switches, for example for fluid systems such as oil, air, fuel, pneumatics and/or hydraulics.
Further optional features of the invention are set out below.
Embodiments of the invention will now be described by way of example with reference to the accompanying drawings in which:

Figure 1 shows a gas turbine engine with a conventional harness;
Figure 2 shows a cross-section through a gas turbine engine having an electrical raft in accordance with the present invention;
Figure 3 shows (a) exploded, (b) perspective, and (c) elevation views of an electrical connector, and (d) a side view of the electrical connector embedded in an electrical raft;
Figure 4 shows a flexible printed circuit connector;
Figure 5 shows a perspective view of a flexible printed circuit;
Figure 6 shows a side view of the flexible printed circuit of Figure 5;
Figure 7 shows a schematic of an electrical raft prior to assembly; and
Figure 8 shows a cross-section normal to the axial direction through a gas turbine engine in accordance with the present invention.

With reference to Figure 2, a ducted fan gas turbine engine generally indicated at 10 has a principal and rotational axis X-X. The engine 10 comprises, in axial flow series, an air intake 11, a propulsive fan 12, an intermediate pressure compressor 13, a high-pressure compressor 14, combustion equipment 15, a high-pressure turbine 16, and intermediate pressure turbine 17, a low-pressure turbine 18 and a core engine exhaust nozzle 19. The engine also has a bypass duct 22 and a bypass exhaust nozzle 23.
The gas turbine engine 10 works in a conventional manner so that air entering the intake 11 is accelerated by the fan 12 to produce two air flows: a first air flow A into the intermediate pressure compressor 13 and a second air flow B which passes through the bypass duct 22 to provide propulsive thrust. The intermediate pressure compressor 13 compresses the air flow A directed into it before delivering that air to the high pressure compressor 14 where further compression takes place.
The compressed air exhausted from the high-pressure compressor 14 is directed into the combustion equipment 15 where it is mixed with fuel and the mixture combusted. The resultant hot combustion products then expand through, and thereby drive the high, intermediate and low- pressure turbines 16, 17, 18 before being exhausted through the nozzle 19 to provide additional propulsive thrust. The high, intermediate and low- pressure turbines 16, 17, 18 respectively drive the high and intermediate pressure compressors 14, 13 and the fan 12 by suitable interconnecting shafts.
The gas turbine engine 10 shown in Figure 2 comprises at least one electrical raft 200 according to the present invention. As such, the gas turbine engine 10 is in accordance with the present invention. The electrical raft 200 comprises an electrical connector 700. The electrical raft 200 may be used to transmit/transfer electrical signals (or electricity, including electrical power and/or electrical control signals) around the engine and/or to/from the engine 10 from other components, such as components of an airframe. The function and/or construction of the electrical raft 200 including the electrical connector 700 may be as described above and elsewhere herein.
In Figure 2, each electrical raft 200 (which may be referred to herein simply as a raft 200 or an electrical harness raft 200) comprises at least one electrical conductor 252 embedded in a rigid material 220, which may be a rigid composite material. In some embodiments, the electrical raft 200 may be provided with other gas turbine components/systems, such as fluid pipes or conduits forming at least a part of a fluid system. Such fluid pipes may be attached to the electrical raft 200 using mounting brackets. Additionally or alternatively, such fluid pipes may be embedded in the electrical raft 200.
In Figure 2, the electrical rafts 200 form part of respective electrical raft assemblies 600. Each electrical raft assembly 600 also comprises a further electrical component 760. The further electrical component 760 is electrically connected to a respective electrical raft 200 via the electrical connector 700 that is part of the electrical raft 200. The electrical raft 200 and the further electrical component are described in greater detail elsewhere herein.
The electrical raft(s) 200 may be attached to the rest of the gas turbine engine 10 using mounts 400, which may be anti-vibration (AV) mounts configured to reduce or substantially eliminate vibration from components of the gas turbine engine 10 being passed to the electrical raft 200, and thus to any components/systems mounted thereon/connected thereto.
Figure 3 shows (a) exploded, (b) perspective, and (c) elevation views of an electrical connector 700, and (d) a side view of the electrical connector 700 embedded in a rigid polymer matrix composite electrical raft 200. As shown in Figure 3(d), an electrical assembly 600 comprises the raft, the connector and a further electrical component 760 connected to the raft via the connector, as described in more detail below.
The electrical connector 700 comprises a first set of electrical contacts 710 through which the embedded electrical conductors 252 (e.g. in the form of FPCs 250) are electrically connected to the electrical connector 700. The first set of electrical contacts 710 may take any suitable form. For example, there may be an intermediate conductor plug or connector in which the electrical conductors terminate, which is then electrically connected to the first set of electrical contacts 710. An example of such an intermediate conductor plug or connector 260 is shown in Figure 3(a) and described in greater detail below.
The electrical connector 700 also comprises a second set of electrical contacts 720. Again, the second set of electrical contacts 720 may take any suitable form, such as male or female connectors, which may be in the form of a plug or socket. The second set of electrical contacts 720 electrically connects the electrical connector 700, and thus the conductors 252 in the electrical raft 200, to the further electrical component 760.
In the example of Figure 3, the second set of electrical contacts 720 are female pins divided between two side-by-side sockets 721 and the complimentary set of contacts are male pins (not shown) divided between two corresponding side-by-side plugs of the further electrical component 760. Separate mechanical connectors (not shown) may be provided to hold, or lock, the electrical connector 700 and the further electrical component 760 together.
The further electrical component 760 may take any suitable form. In Figure 3, for example, the further electrical component 760 comprises a set of electrical conductors 766, such as an FPC, and/or one or more wires, which may be sheathed and/or bundled together. Thus, the set of electrical conductors 766 may be flexible. The set of electrical conductors 766 may be used, for example, to connect the electrical raft 200 to another electrical component, which may be, for example, another electrical raft 200 or an ECU, such as an EEC or EMU. In Figure 3(d), the further electrical component 760 also comprises a body 764, the complimentary set of electrical contacts in their side-by-side plugs being provided at one end of the body 764, and electrical conductors 766 extending from the other end of the body 764.
Alternatively, as mentioned elsewhere herein, the further electrical component 760 may be any type of electrical component. For example, the further electrical component may be an electrical unit, or ECU, such as an EEC or an EMU. Thus, the further electrical component 760 may be an electrical unit, which may be connected to the electrical raft 200, for example directly connected to the second set of electrical contacts 720 using a set of complimentary electrical contacts.
The electrical connector 700 has a housing 706. The housing 706 may contain internal components of the electrical connector 706, such as internal electrical connections (not shown). The housing 706 has a first end 702 and a second end 704, which may be opposite to each other. The first set of electrical contacts 710 are formed at the first end 702. The second set of electrical contacts 720 are formed at the second end 704. The first end 702 is partially or, as shown in Figure 3(d), completely embedded in the rigid composite material 220.
The electrical connector 700 also has a back-shell 740 which encloses the first end 702 of the housing 706. As well as providing protection against resin movement during manufacture, the back-shell 740 can provide sealing against ingress of fluids (such as water, oil and fuel) during use. The back-shell can be held in place at the first end by mechanical fasteners such as screw-fittings 742. An elastomeric seal 744 may be provided between the housing and the back-shell to improve the sealing between these components.
As described in more detail below, to manufacture the raft 200, the electrical conductors 252 (e.g. in the form of FPCs 250) may be provided between fibre reinforcement layers 746 that are impregnated with and joined together by a polymer matrix (i.e. resin). Preferably, the first set of electrical contacts 710 are joined to the electrical conductors 252 and the back-shell 740 is connected to the housing 706 before the polymer matrix is cured or set, e.g. as part of a laying up process of the electrical conductors 252 and reinforcement layers 746, or before injection moulding of the composite material around the electrical conductors 252 and connector 700. In this way, the connector 700 can be integrated with the raft 230, 240. The back-shell prevents ingress of the polymer matrix into the connector during manufacture.
The electrical connector 700 can be mounted in the composite material of the electrical raft 200 at a mounting angle 730. The mounting angle 730 (shown in Figure 3(d)) is the acute angle formed between the longitudinal axis of the electrical connector 700 (i.e. the axis which extends from the first end 702 to the second end 704 of the housing 706) and a (first) major surface 222 of the raft 200 from which the second end 704 of the housing 706 is accessible. A second major surface 224 of the raft is parallel to and spaced from the first major surface 222.
The mounting angle 730 shown in Figure 3(d) is for illustrative purposes only. In general, the mounting angle 730 is in the range of from 20 degrees to 70 degrees, for example in the range of from 25 degrees to 65 degrees, for example in the range of from 30 degrees to 60 degrees, for example in the range of from 35 degrees to 55 degrees, for example in the range of from 40 degrees to 50 degrees, for example on the order of 45 degrees.
In order to achieve and/or facilitate achieving the desired mounting angle, the electrical raft 200 may comprise a location feature 750. In the Figure 3 example, the location feature 750 is a flange extending around the first end 702 of the housing 706. The location feature 750 may be aligned with the electrical raft 200, for example with the first and/or second major surfaces 222, 224 of the rigid material 220. In other words, during assembly, the location feature 750 may be aligned with the first and/or second major surfaces 222, 224 in order to ensure that the mounting angle 730 is as desired. However, it will be appreciated that a location feature could take any suitable form in order to facilitate correct mounting/location of the electrical connector 700 in the rigid material of the raft.
As shown in Figure 3(d) the electrical raft 200 also comprises an earthing mesh 770. The earthing mesh 770 may provide electrical screening to the electrical conductors embedded in the raft. The earthing mesh may be embedded in the composite structure (for example it may be provided during manufacture). In Figure 3(d), the screw-fittings 742 form an earthing mesh fixture which holds the earthing mesh 770 in position. However, such an earthing mesh fixture need not be required. For example, the earthing mesh 770 may be embedded and secured in position during manufacture.
The housing 706 and the back-shell 740 may be electrically conductive and may be in electrical contact with each other (e.g. via the screw-fittings 742) to provide electro-magnetic shielding of the connector 700. For example, the housing and the back-shell can be formed of metal. However another option is to form the housing and the back-shell of conductive or plated composite, plastic or ceramic.
The electrical conductors 252 of the FPCs 250 terminate in two dedicated connectors 260, which are then connected to the first set of electrical contacts 710. As shown in greater detail in Figure 4, such a dedicated connector 260, which may be referred to as a lollipop connector 260 or a flexible printed circuit connector 260, comprises openings 265. An opening 265 is formed at the end of a respective electrical conductor (or track) 252 of the FPC 250, as in Figure 4. The openings 265 are configured to receive the first set of electrical contacts 710, for example the first set of electrical contacts may comprise pins (as shown in Figure 3), each of which is received in a respective opening 265. The dedicated connector 260 may be substantially rigid such that it maintains its shape under operating and/or manufacture loads. This may be achieved, for example, by reinforcing the dedicated connector with a rigid material.
In order for the embedded electrical conductors 252 to be connected to the electrical connector 700 in the manner shown in Figure 3, the electrical conductors must turn through an angle equal to 90 degrees minus the mounting angle 730. This may be referred to as a complimentary mounting angle 732 (shown in Figure 3(a). This complimentary mounting angle may be such that the conductors 252 can be bent into position without causing undue stress, and thus with a minimal risk of damage. In general, the complimentary mounting angle 732 is in the range of from 20 degrees to 70 degrees, for example in the range of from 25 degrees to 65 degrees, for example in the range of from 30 degrees to 60 degrees, for example in the range of from 35 degrees to 55 degrees, for example in the range of from 40 degrees to 50 degrees, for example on the order of 45 degrees.
Figure 3(d) shows a part of an electrical raft 200, including just one electrical connector 700. However, it will be appreciated that an electrical raft 200 or electrical raft assembly 600 may comprise any number of electrical connectors 700, any one or more of which may have a back-shell 740 as described herein. Further any or more may be mounted/embedded at the mountain angle 730 described herein. Some electrical rafts 200 or electrical raft assemblies 600 may have at least one electrical connector 700 mounted at a mounting angle as described herein, together with one or more electrical connectors mounted at different angles depending on, for example geometric and spatial constraints.
As mentioned elsewhere herein, the electrical conductors 252 in the electrical raft 200 may be provided in a harness 250, which may be a flexible printed circuit board (or FPC) 250. Additionally or alternatively, the further electrical component 760 may comprise electrical conductors 766, some or all of which may also be in the form of an FPC. An example of an FPC 250 in which the electrical conductors 252 may be provided is shown in greater detail in Figures 5 and 6. Figure 5 shows a perspective view of the FPC 250, and Figure 6 shows a side view.
Such an FPC 250 may comprise a flexible (for example elastically deformable) substrate 255 with conductive tracks 252 laid/formed therein. The FPC 250 may thus be deformable. The FPC 250 may be described as a thin, elongate member and/or as a sheet-like member. Such a thin, elongate member may have a major surface defined by a length and a width, and a thickness normal to the major surface. In the example shown in Figures 5 and 6, the FPC 250 may extend along a length in the x-direction, a width in the y-direction, and a thickness (or depth or height) in the z-direction. The x-direction may be defined as the axial direction of the FPC. Thus, the x-direction (and thus the z-direction) may change along the length of the FPC 250 as the FPC is deformed. This is illustrated in Figure 6. The x-y surface(s) (i.e. the surfaces formed by the x and y directions) may be said to be the major surface(s) of the FPC 250. In the example shown in Figures 5 and 6, the FPC 250 is deformable at least in the z direction, i.e. in a direction perpendicular to the major surface. FPCs may be additionally of alternatively deformable about any other direction, and/or may be twisted about any one or more of the x, y, or z directions.
The flexible substrate 255 may be a dielectric. The substrate material may be, by way of example only, polyamide. As will be readily apparent, other suitable substrate material could alternatively be used.
The conductive tracks 252, which may be surrounded by the substrate 255, may be formed using any suitable conductive material, such as, by way of example only, copper, copper alloy, tin-plated copper (or tin-plated copper alloy), silver-plated copper (or silver-plated copper alloy), nickel-plated copper (or nickel-plated copper alloy) although other materials could alternatively be used. The conductive tracks 252 may be used to conduct/transfer electrical signals (including electrical power and electrical control signals) through the rigid raft (or rafts) 200, for example around a gas turbine engine 10 and/or to/from components of a gas turbine engine and/or an airframe attached to a gas turbine engine.
The size (for example the cross-sectional area) and/or the shape of the conductive tracks 252 may depend on the signal(s) to be transmitted through the particular conductive track 252. Thus, the shape and/or size of the individual conductive tracks 252 may or may not be uniform in a FPC 250.
The example shown in Figures 5 and 6 has six conductive tracks 252 running through the substrate 255. However, the number of conductive tracks 252 running through a substrate 255 could be fewer than six, or greater than six, for example tens or hundreds of tracks, as required. As such, many electrical signals and/or power transmission lines may be incorporated into a single FPC 250.
A single FPC 250 may comprise one layer of tracks, or more than one layer of tracks, for example, 2, 3, 4, 5, 6, 7, 8, 9, 10 or more than 10 layers of tracks. An FPC may comprise significantly more than 10 layers of tracks, for example at least an order of magnitude more layers of tracks. In this regard, a layer of tracks may be defined as being a series of tracks that extend in the same x-y surface. Thus, the example shown in Figures 5 and 6 comprises 2 layers of tracks, with each layer comprising 3 tracks 252.
An electrical raft 200 may be manufactured using any suitable method. For example, the rigid material 220 may initially be provided as layers of flexible material, such as (by way of example only) layers of fibre and resin compound. This flexible material may be placed into a mould, for example having a desired shape. Other components (such as fluid pipes 210 and/or the electrical conductors 252, which may be embedded in a FPC 250) may also be placed into the mould, for example between layers of the flexible material from which the rigid material 220 is ultimately formed. Parts of the mould may have any suitable form and/or construction, for example that could be readily removed when the electrical raft 200 is formed into the desired shape.
Figure 7 shows components of an example of an electrical raft 200 prior to one method of construction. The electrical conductors 252 are provided between two layers of material 230, 240 that, after construction, form the rigid material 220. Some of the electrical conductors 252 are provided in an FPC 250. The material 230, 240 may be a fibre and resin compound, as described elsewhere herein. Such a fibre and resin compound may, after suitable treatment (for example heat treatment), produce the rigid composite material 220. In the example of Figure 7, the fibre and resin compound is formed of a sheet of interwoven fibres, or strands. The strands in Figure 7 extend in perpendicular directions, although the strands may extend in any one or more directions as required. The strands/fibres may be pre-impregnated (or "pre-pregged") with the resin.
Prior to any treatment, both the first and second layers 230, 240 and the electrical conductors 252 may be flexible, for example supple, pliable or malleable. As such, when the layers 230, 240 and the electrical conductors 252 are placed together, they may be moulded, or formed, into any desired shape. For example, the layers 230, 240 and the electrical conductors 252 may be placed into a mould (which may be of any suitable form, such as a glass or an aluminium mould) having the desired shape. The desired shape may be, for example, a shape that corresponds to (for example is offset from) a part of a gas turbine engine, such as, by way of example only, at least a part of a casing, such as an engine fan casing or engine core casing. This may enable the final raft to adopt shapes that are curved in two-dimensions or three-dimensions.
Any suitable method could be used to produce the electrical raft 200. For example, the strands/fibres need not be pre-impregnated with the resin. Instead, the fibres/strands could be put into position (for example relative to electrical conductors 252/FPC 250) in a dry state, and then the resin could be fed (or pumped) into the mould. Such a process may be referred to as a resin transfer method. In some constructions no fibre may be used at all in the rigid material 220.
After the treatment, the electrical raft 200 may be set in the desired shape. The electrical connectors 700 may be provided to the electrical raft 200 at any suitable time during manufacture. Preferably they are provided prior to a stiffening treatment of the rigid raft 200, such that their back-shells 740 can prevent ingress of contaminating resin into the connectors. However, this is not to exclude that they can be provided after such treatment, the back-shells still providing useful protection against ingress of other contaminants during use.
Thus, for example, the electrical connector(s) 700 (together with any associated components) may be embedded directly into the electrical raft 200 during the forming and setting of the electrical raft 200. As such, the rigid material 220 may set around the electrical connector(s) 700, thereby fixing them into position. In this case, the electrical conductors 252 may be in electrical contact with the electrical connector(s) 700 prior to the rigid material 220 being set around them.
Alternatively, the or each connector 700 (together with any associated components) may be fixed (for example bonded) into an appropriate recess in the electrical raft. Such a recess may be formed using a correspondingly shaped mould, or may be formed (for example by machining or boring) after the rigid electrical raft is set. The first set of electrical contacts 710 of the or each electrical connector 700 may be electrically connected to one or more embedded electrical conductors 252 at this stage.
Figure 8 is a schematic showing a cross-section perpendicular to the direction X-X of a gas turbine engine comprising electrical rafts 200A-200G. Figure 8 shows seven electrical rafts 200A-200G (which may collectively be referred to as electrical rafts 200).
Five of the electrical rafts 200A-200E comprise at least one electrical connector 700. These five electrical rafts 200A-200E may be in accordance with the electrical raft 200 described, for example, in relation to Figures 3 and 4, and the electrical connector(s) 700 may also be as described elsewhere herein, for example in relation to Figure 3. Each of the five electrical rafts 200A-200E has a further electrical component (which may include an electrical conductor 766) attached thereto, each electrical raft 200A-200E thereby forming an electrical raft assembly 600 (as labelled in relation to rafts 200A and 200C, but not the other rafts to aid clarity of the Figure).
Each of the electrical rafts 200A-200G shown in Figure 8 comprises one or more electrical conductors 252 as described elsewhere herein. However, any one or more of the electrical rafts 200A-200G may be replaced with a raft that does not comprise electrical conductors 252 (but not all of the electrical rafts 200A-200E). Such a raft would not be an electrical raft 200, but may otherwise be as described elsewhere herein, for example it may be a rigid raft that may have components/systems (such as, by way of example only, fluid systems, such as pipes) mounted thereon and/or embedded therein. Thus, for example, a gas turbine engine 10 in accordance with the present invention may have a combination of electrical rafts 200 and non-electrical rafts.
The arrangement of electrical rafts 200A-200G shown in Figure 8 is by way of example only. Alternative arrangements, for example in terms of number, size, shape and/or positioning, of electrical rafts 200A-200G may be used. For example, there need not be seven electrical rafts, the rafts may or may not be connected together, and the rafts could be provided to (for example mounted on) any one or more components of the gas turbine engine. Purely by way of example only, connection between electrical rafts 200A, 200B, 200C, 200F mounted on the fan casing 24 to the electrical rafts 200D, 200E mounted on the core casing 28 may be provided at least in part by means other than an additional electrical raft 200G, for example using wire conductors with insulating sleeves. By way of further example, one or more electrical rafts 200 may additionally or alternatively be provided to the nose cone, structural frames or elements within the engine (such as "A-frames"), the nacelle, the fan cowl doors, and/or any connector or mount between the gas turbine engine 10 and a connected structure (which may be at least a part of a structure in which the gas turbine engine 10 is installed), such as the pylon 500 between the gas turbine engine 10 and an airframe (not shown).
Any one or more of the electrical rafts 200A-200G may have a fluid passage 210 embedded therein. The fluid passage 210 may be part of a fluid system, such as a gas (for example pneumatic or cooling gas/air) and/or liquid (for example a fuel, hydraulic and/or lubricant liquid). In the Figure 8 example, three of the electrical rafts 200A, 200C, 200F comprise a fluid passage 210 at least partially embedded therein. The electrical raft 200C also has a fluid passage 285 (which may be for any fluid, such as those listed above in relation to embedded passage 210) mounted thereon. Such a mounted fluid passage 285 may be provided to any electrical raft, such as those of electrical rafts 200A-200G shown in Figure 8. The fluid passages 210, 285 shown in Figure 8 may be oriented in an axial direction of the engine 10. However, fluid passages may be oriented in any direction, for example axial, radial, circumferential or a combination thereof.
Two of the electrical rafts 200A, 200C in the Figure 8 arrangement have electronic units 300 mounted thereon. The electronic control units 300 are electrically connected to the electrical rafts 200A, 200C via connections 800. At least a part of each connection 800 may be an electrical connection 700 with a back-shell as described elsewhere herein. Alternatively, the connections between the electronic units 300 and the electrical raft 200A, 200C may take any other suitable form. It will be appreciated that electrical units 300 may be provided to any one or more electrical raft provided to an engine 10, such as the electrical rafts 200A-200G shown in Figure 8.
In general, any electrical raft 200 may be provided with and/or may comprise (for example may have mounted on and/or have at least partially embedded therein) at least a part of any component and/or system of a gas turbine engine. Components/systems provided to different rafts 200 may be connected to each other, for example a component mounted on one raft 200 may be connected (for example directly electrically, mechanically and/or fluidly connected) to one or more components mounted on another raft 200.
The electrical rafts 200A-200G may be attached to the rest of the gas turbine engine 10 in any suitable manner. For example, as labelled explicitly in relation to electrical raft 200B, mounts 400, which may be anti-vibration mounts, may be used. Using anti-vibration mounts 400 may, for example, allow all components of the electrical raft 200 and/or electrical raft assembly 600 to be isolated from vibrations. Thus, components of at least two gas turbine engine systems may be vibration isolated using a single set of anti-vibration mounts 400.
The electrical rafts 200A, 200B, 200C, 200F are mounted to a fan case 24 in the example of Figure 8. However, electrical rafts 200 such as those described by way of example herein may be provided/mounted anywhere on the engine 10. For example, one or more electrical raft 200D, 200E may be mounted between an engine core casing 28 and an engine core fairing 26. Also by way of example, one or more electrical raft 200G may be provided as at least a part of (for example in) a passage across the bypass duct 22, such as a bifurcation or splitter. In other respects, the electrical rafts mounted anywhere on the engine may be as described elsewhere herein, or otherwise in accordance with the invention. Although only five of the electrical rafts 200A-200E are shown as comprising an electrical connector 700 having a back-shell as described herein, any one of the electrical rafts 200A-200G shown in Figure 8 may comprise such an electrical connector 700, and thus may be in accordance with the invention.
Any of the electrical rafts 200A-200G (or non-electrical rafts in an arrangement where at least one the of rafts does not have electrical conductors 252) may have any combination of mechanical, electrical and/or fluid connections to one or more (for example 2, 3, 4, 5 or more than 5) other components/systems of the gas turbine engine 10 and/or the rest of the gas turbine engine 10. Examples of such connections are shown in Figure 8, and described below, but it will be appreciated that a gas turbine engine 10 including electrical rafts 200 may have connections that are different to those shown in Figure 8, although at least one of the electrical rafts 200 has an electrical connector 700 provided with a back-shell as described herein. For example, electrical rafts 200 (and/or non-electrical rafts) may be connected together (or to other components) using any combination of electrical, fluid and/or mechanical connectors. Thus, any of the connections 290A/290B, 766 shown in Figure 8 may be any combination of electrical, fluid and/or mechanical connection. Alternatively, electrical rafts (and/or non-electrical rafts) may be standalone, and thus may have no connection to other rafts or components.
A connection 766 is shown between the electrical rafts 200A and 200B. The connection 766 may comprise an electrical connection. Such an electrical connection may be flexible and may, for example, take the form of a flexible printed circuit such as the flexible printed circuit 250 shown in Figures 5 and 6. The electrical connection 766 may be part of a further electrical component 760 that is electrically connected to the second set of electrical contacts 720 of the electrical connector 700, for example as described herein in relation to Figure 3 in particular. Such a flexible electrical connection766 may be used to electrically connect any electrical raft 200 to any other component, such as another electrical raft 200 Further, similar, electrical connections 766 are provided between the electrical rafts 200A, 200C and a part of an airframe, or airframe installation 500, which may, for example, be a pylon. Similarly, an electrical connection 766 (extending from a respective electrical connector 700) is provided between each of the rafts 200D, 200E mounted between the engine core casing 28 and the engine core fairing 26 and the electrical raft 200G provided in the engine bifurcation or splitter.
Each of the rafts 200A-200E in Figure 8 that is provided with an electrical connector 700 having a back-shell as described herein, and is thus in accordance with the invention, is connected to a further electrical component in the form of one or more electrical conductors 766. However, the further electrical component that is connected to the electrical connector 700 may be of any type, for example any type of ECU, as described elsewhere herein.
Thus, it will be appreciated that the further electrical components attached to the electrical connectors 700 of the electrical rafts 200A-200E are by way of example only.
A direct connection 290A, 290B is provided between the electrical rafts 200B and 200C in the Figure 8 arrangement. Such a direct connection 290A, 290B may comprise a connector 290A provided on (for example embedded in) one electrical raft 200C connected to a complimentary connector 290B provided on (for example embedded in) another electrical raft 200B. Such a direct connection 290A, 290B may, for example, provide fluid and/or electrical connection between the two electrical rafts 200B, 200C.
Where reference is made herein to a gas turbine engine, it will be appreciated that this term may include a gas turbine engine/gas turbine engine installation and optionally any peripheral components to which the gas turbine engine may be connected to or interact with and/or any connections/interfaces with surrounding components, which may include, for example, an airframe and/or components thereof. Such connections with an airframe, which are encompassed by the term "gas turbine engine" as used herein, include, but are not limited to, pylons and mountings and their respective connections. The gas turbine engine itself may be any type of gas turbine engine, including, but not limited to, a turbofan (bypass) gas turbine engine, turbojet, turboprop, ramjet, scramjet or open rotor gas turbine engine, and for any application, for example aircraft, industrial, and marine application. Electrical raft 200 such as any of those described and/or claimed herein may be used as part of any apparatus, such as any vehicle, including land, sea, air and space vehicles, such as motor vehicles (including cars and busses), trains, boats, submarines, aircraft (including aeroplanes and helicopters) and spacecraft (including satellites and launch vehicles).
It will be appreciated that many alternative configurations and/or arrangements of electrical rafts 200 and gas turbine engines 10 comprising electrical rafts 200 other than those described herein may fall within the scope of the invention. For example, alternative arrangements of electrical rafts 200 (for example in terms of the arrangement, including number/shape/positioning/constructions, of mounting fixtures, the arrangement/shape/positioning/construction of the electrical rafts 200, the type and/or positioning of components (if any) mounted to/embedded in the electrical rafts 200, the rigid material 220 and the electrical conductors 252) may fall within the scope of the invention and may be readily apparent to the skilled person from the disclosure provided herein. Alternative arrangements of connections (for example mechanical, electrical and/or fluid) between the electrical (or non-electrical) rafts and between the electrical (or non-electrical) rafts and other components may fall within the scope of the invention and may be readily apparent to the skilled person from the disclosure provided herein. Furthermore, any feature described and/or claimed herein may be combined with any other compatible feature described in relation to the same or another embodiment.

Claims

A part of an electrical harness for a gas turbine engine (200) comprising:
a rigid material (220) having multiple electrical conductors (252) embedded therein so as to be surrounded by the rigid material and fixed in position by the rigid material, and

an electrical connector (700) having a first set of electrical contacts (710) connected to at least one of the electrical conductors, a second set of electrical contacts (720) for electrical connection to another component, and a housing (706) having a first end (702) and a second end (704), the first set of electrical contacts being at the first end and the second set of electrical contacts being at the second end;

wherein:
the first end of the housing is at least partly embedded in the rigid material, and the second end of the housing is accessible from outside the electrical raft, thereby allowing the electrical raft to be electrically connected to said other component, and

the electrical connector further has a back-shell (740) which sealingly encloses the first end of the housing and the first set of electrical contacts to prevent ingress of contaminants into the connector.
A part of an electrical harness for a gas turbine engine according to claim 1, wherein the rigid material is a rigid polymer matrix composite material.
A part of an electrical harness for a gas turbine engine according to claim 1 or 2, wherein the electrical connector has an elastomeric seal (744) between the housing and the back-shell.
A part of an electrical harness for a gas turbine engine according to any one of the preceding claims, wherein the housing and the back-shell are electrically conductive and are in electrical contact with each other to provide electro-magnetic shielding of the connector.
A part of an electrical harness for a gas turbine engine according to any one of the preceding claims, wherein:
at least some of the electrical conductors are provided in a flexible printed circuit (250) in the form of electrical tracks formed in a flexible substrate (255),

the electrical tracks terminate in openings (265) in a flexible printed circuit connector (260), and

the first set of electrical contacts comprise pins that are received in respective openings (265) so as to electrically connect the electrical tracks to the electrical connector.
A part of an electrical harness for a gas turbine engine according to any one of the preceding claims, wherein the electrical raft has a major surface (222) from which the second end of the housing is accessible, and the electrical connector has a longitudinal axis which extends from the first end to the second end of the housing;
the connector being mounted in the rigid material such that the longitudinal axis forms a mounting angle (730) in the range of from 20 degrees and 70 degrees with the major surface.
A part of an electrical harness for a gas turbine engine according to claim 6, wherein the second set of electrical contacts are aligned with the electrical connector so as to be at the mounting angle relative to the major surface.
A part of an electrical harness for a gas turbine engine according to any one of claims 6 or 7, wherein the first set of electrical contacts are aligned with the electrical connector so as to be at the mounting angle relative to the major surface.
A part of an electrical harness for a gas turbine engine according to any one of claims 6 to 8 as dependent on claim 5, wherein the electrical conductors provided in the flexible printed circuit turn through an angle (732) equal to 90 degrees minus the mounting angle before terminating in the openings in the flexible printed circuit connector.
A part of an electrical harness for a gas turbine engine according to any one of the preceding claims, further comprising an electrically conductive screen layer (770).
An assembly (600) comprising:
a part of an electrical harness for a gas turbine engine according to any one of the preceding claims, and

a further electrical component (760) comprising a complimentary set of electrical contacts (762) that correspond to the second set of electrical contacts, wherein

the part of an electrical harness for a gas turbine engine and the further electrical component are in electrical connection through the second set of electrical contacts and the complimentary set of electrical contacts.
A gas turbine engine or gas turbine engine installation, having the part of an electrical harness for a gas turbine engine or the assembly according to any one of the previous claims.
A gas turbine engine or gas turbine engine installation according to claim 12, wherein:
the part of an electrical harness for a gas turbine engine or the assembly is a first engine installation component (200A),

the gas turbine engine or gas turbine engine installation further comprises a second engine installation component (200B) having electrical conductors, and

at least one flexible cable (766) connects between the part of an electrical harness for a gas turbine engine or the assembly and the second engine installation component so as to electrically connect electrical conductors of the part of an electrical harness for a gas turbine engine or the assembly with electrical conductors of the second engine installation component.
A method of manufacturing a gas turbine engine (10) comprising:
attaching a part of an electrical harness according to any one of claims 1 to 10 to the engine, and

electrically connecting a further electrical component (766) of the gas turbine engine to the part of the electrical harness by connecting the second set of contacts to a complimentary set of contacts (762) of the further electrical component.