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270VDC AIRCRAFT CIRCUIT WIRING

faresos

Senior Member
Hello Everyone,

Can we use THHN/THWN-2 wires for 270VDC circuit (used to power an outlet for aircraft power plug)? Is there anything I need to be concern of as far sizing this circuits (100A), other than voltage drop? Thanks,
 

Geber

Member
Location
Vermont
Occupation
PE, retired electronics engineer
I saw an FAA-recommended training video which warned against using solid wire on aircraft. The video claimed solid wire tended to break of at connections because of vibration.
 

faresos

Senior Member
I saw an FAA-recommended training video which warned against using solid wire on aircraft. The video claimed solid wire tended to break of at connections because of vibration.
it will be stranded type (for 100A circuit)
 

tortuga

Code Historian
Location
Oregon
Occupation
Electrical Design
Is this wiring in the plane itself? Or wiring in say a maintenance hanger to supply power to an aircraft?
 

winnie

Senior Member
Location
Springfield, MA, USA
Occupation
Electric motor research

tom baker

First Chief Moderator & NEC Expert
Staff member
Location
Bremerton, Washington
Occupation
Master Electrician
This is premise wiring for a receptacle in a hanger? Then you would follow the rules for wiring in Chapter 3. Note: some hangers can be a classified location per chapter 5
 

drcampbell

Senior Member
Location
The Motor City, Michigan USA
Occupation
Registered Professional Engineer
I saw an FAA-recommended training video which warned against using solid wire on aircraft. The video claimed solid wire tended to break of at connections because of vibration.
Even 7-strand wire isn't really suitable for vehicles.

Do you know what types of aircraft use 270 VDC, and what they use it for?
 

synchro

Senior Member
Location
Chicago, IL
Occupation
EE
F-22 and 787 and others use 270 Vdc. BAC13-70 wire typical, or 13-78

And according to the article at the link below, on the 787 +-270VDC buses supply substantial loads from VFDs:

"The ±270 VDC system supports a handful of large-rated adjustable speed motors required for the no-bleed architecture. These include cabin pressurization compressor motors, ram air fan motors, the nitrogen-generation-system compressor used for fuel-tank inerting, and large hydraulic pump motors."

The primary power is generated at 235 VAC 380-800Hz, and from which 115 VAC, +-270VDC, and 28 VDC are derived and distributed.

http://www.boeing.ch/commercial/aeromagazine/articles/qtr_4_07/article_02_3.html
 

junkhound

Senior Member
Location
Renton, WA
Occupation
EE, power electronics specialty
235 VAC 380-800Hz

Many vendors sent existing 400 Hz designs for use on the test flight aircraft.

More than a few forgot to analyze for the 380-800 Hz part. The 19 pulse ATRUS used to generate the 270 Vdc produce a lot of 17th and 19th harmonics, those would hit the resonance of the EMI filters as engine speed changed and blowup power supply capacitors.
 
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