Heated rigid electrical harness for a gas turbine engine
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United States of America Patent
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Nov 7, 2017
Issued Date -
N/A
app pub date -
Dec 9, 2013
filing date -
Dec 22, 2011
priority date (Note) -
In Force
status (Latency Note)
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Abstract
A rigid electrical raft has electrical conductors embedded in a rigid material. The electrical conductors transmit electrical signals through the rigid electrical raft, which may form part of an electrical system of a gas turbine engine. The rigid electrical raft also has electrical heating elements embedded therein. The electrical heating elements provide heat which may be used, for example, to prevent condensation and/or ice build-up and/or to raise the temperature of electrical components to be within a desired range.
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International Classification(s)
- F24H:FLUID HEATERS, e.g. WATER OR AIR HEATERS, HAVING H....
- B23P:OTHER WORKING OF METAL; COMBINED OPERATIONS; UNIVE....
- H05B:ELECTRIC HEATING; ELECTRIC LIGHTING NOT OTHERWISE ....
- H01R:ELECTRICALLY-CONDUCTIVE CONNECTIONS; STRUCTURAL AS....
- B60R:VEHICLES, VEHICLE FITTINGS, OR VEHICLE PARTS, NOT ....
- B64D:EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLYING SU....
- F02C:GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION....
- H02G:INSTALLATION OF ELECTRIC CABLES OR LINES, OR OF CO....
- B64C:AEROPLANES; HELICOPTERS
- H05K:PRINTED CIRCUITS; CASINGS OR CONSTRUCTIONAL DETAIL....
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