Aircraft cable routing harness
US-9040821-B2 · May 26, 2015 · US
US9426844B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-9426844-B2 |
| Application number | US-201213716516-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 17, 2012 |
| Priority date | Dec 22, 2011 |
| Publication date | Aug 23, 2016 |
| Grant date | Aug 23, 2016 |
A practical reading order for non-experts. Skip the full description unless you need deep technical detail.
What the patent document calls the invention.
A short plain-language summary of the technical disclosure.
Who owns or filed the patent and who is credited as inventor.
Filing, priority, publication, and grant dates set the timeline.
The legal scope of protection — read this for what is actually claimed.
Technology tags used to group this patent with similar filings.
Prior art links and similar publications in this corpus.
Official abstract text for this publication.
An electrical raft 200 is provided that has electrical conductors 252 embedded in a rigid material 220 . The electrical raft 200 may have other embedded components, such as embedded fluid pipes 210 . The electrical raft 200 is provided with a raft map 400 that indicates the location and/or path of components embedded in the electrical raft 200 . The raft map 400 can be used to identify the positions of the embedded components, and may also be provided with active elements, such as LEDs, which may be used to indicate an operating state of the systems/components embedded in the electrical raft 200 . The raft map 400 may be useful in assembly, repair and fault diagnosis, for example.
Opening claim text (preview).
We claim: 1. A gas turbine engine having an electrical raft, the electrical raft comprising: components embedded in a rigid material, the components including embedded electrical conductors that form at least a part of an electrical system of the gas turbine engine, the electrical conductors configured to carry electrical signals for the gas turbine engine; and a raft map comprising lines indicating paths of at least some of the embedded electrical conductors within the electrical raft, the raft map being visible from outside the electrical raft, wherein the electrical raft has at least one outer surface, on which the raft map is provided. 2. The gas turbine engine according to claim 1 , wherein the rigid material is a rigid composite material. 3. The gas turbine engine according to claim 1 , wherein: the embedded components further comprise at least one fluid passage embedded in the rigid material; and the raft map also comprises a further line that shows a path of the or each embedded fluid passage. 4. The gas turbine engine according to claim 3 , wherein the raft map also includes an arrow indicating a direction in which fluid is configured to flow through the fluid passage in use. 5. The gas turbine engine according to claim 3 , wherein: the raft map comprises an active indicator that has at least two state outputs, each state output indicating a different state of the fluid passage in use. 6. The gas turbine engine according to claim 1 , wherein: the raft map comprises an active indicator that has at least two state outputs, each state output indicating a different state of an electrical component. 7. The gas turbine engine according to claim 5 , wherein the active indicator comprises a light emitting device. 8. The gas turbine engine according to claim 1 wherein: the raft map shows a projection of an actual position of at least some of the embedded components. 9. The gas turbine engine according to claim 1 , wherein the raft map is a substantially full scale representation of the embedded components. 10. The gas turbine engine of claim 1 , wherein the electrical raft forms a first engine installation component; and a second engine installation component comprising electrical conductors; and at least one flexible cable electrically connected between the electrical raft and the second engine installation component. 11. The gas turbine engine according to claim 5 , wherein the state indicated by the active indicator corresponds to at least one of a flow rate and a flow pressure through the fluid passage in use. 12. The gas turbine engine according to claim 6 , wherein the state indicated by the active indicator corresponds to at least one of a voltage across and a current through an electrical component in use. 13. The gas turbine engine according to claim 8 , wherein the projection is a projection onto a surface of the electrical raft. 14. A method of servicing a gas turbine engine according to claim 1 , the method comprising: removing the electrical raft from the gas turbine engine; and installing a second, pre-prepared, electrical raft onto the gas turbine engine in place of the removed electrical raft.
Flexible materials (H05K1/038 takes precedence; specific organic compositions are classified in H05K1/0313 and subgroups) · CPC title
Retaining components in desired mutual position · CPC title
Repairing, converting, servicing or salvaging · CPC title
Methods or apparatus specially adapted for installing, maintaining, repairing or dismantling electric cables or lines · CPC title
Electrical device making · CPC title
Related publications grouped by family.
Answers are generated from the same data shown on this page.