Effects on a cable at sea level compared to 35,000 feet

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SUMMARY

The discussion focuses on the effects of altitude on electrical cables, specifically generator cables used in a Boeing 747 at 35,000 feet compared to sea level. Key factors include a decrease in temperature, which affects resistance, and the breakdown voltage of air, which is significantly lower at high altitudes. The temperature coefficient of resistance for both copper and aluminum is noted as 3.9 x 10^-3. Additional considerations include reduced cooling efficiency and potential cable outgassing at altitude, which may impact performance.

PREREQUISITES
  • Understanding of electrical resistance and temperature coefficients
  • Familiarity with cable materials, specifically copper and aluminum
  • Knowledge of altitude effects on electrical systems
  • Basic principles of aircraft design and weight considerations
NEXT STEPS
  • Research the International Standard Atmosphere (ISA) for altitude-related design conditions
  • Investigate the Joint Airworthiness Regulations (JARs) relevant to aircraft electrical systems
  • Learn about the effects of altitude on breakdown voltage and corona discharge in cables
  • Explore cooling mechanisms for electrical cables in aviation environments
USEFUL FOR

Aerospace engineers, electrical engineers, and anyone involved in the design and maintenance of aircraft electrical systems will benefit from this discussion.

joe465
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Hi Guys,

Struggling to find any information on the changes to a cable at altitude compared to at sea level. The initial task was to calculate the resistance of generator wires and then change them from copper to aluminium cables to save weight. I have done this leading me onto describing the effects of the cable at 35,000 feet compared to at sea level.

All i can think of is a decrease in temperature causing a reduction in resistance but would ideally like to provide an example but struggling to find a formula to fit. I know copper has a temperature coefficient of resistance of 3.9 * 10^-3 and aluminium is the same.

Are there any other major effects to the cable at altitude?

Cheers,

Joe
 
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The temperature depends on the environment. 35000 feet above sea level is a typical altitude for an airplane, so temperature will depend on the position of the cable in the airplane.
You also get a bit more radiation, but that should be negligible for cables, and I don't see any effect of a changed air pressure.
 
Thanks, it is for an aircraft, it is generator cables for a 747. No environment stated so i could possibly just go with the 2 degree decrease every 1000 feet?. What would you recommend?
 
If temperature is important, I would recommend to check the design, and the expected temperature range for the cable.
 
I don't have any answers, but do have some questions.
At 35,000 feet the breakdown voltage of air is much less than at sea level.

Would there be a problem with cable terminations breaking down at 35,000 feet?
Would cable have corona at 35,000 feet? (Very short life)
Cooling of cables will be less at 35,000 feet. What is temperature rise?
Will cables outgas at 35,000 feet? Is this a problem?
 
It is impossible to answer those questions in general.
 
  • #10
joe465 said:
No environment stated so i could possibly just go with the 2 degree decrease every 1000 feet?. What would you recommend?

If this is a "homework" exercise, I think using the International Standard Atmosphere would be defensible set of design conditions. Or use ISA + or - 20C, whichever is the worst design conditions.

If it is "for real", you need to find the relevant section of the Joint Airworthiness Regulations (JARs) - sorry, I'm not an "electrical" guy so I can't tell you which section you want, but don't expect it to be easy bedtime reading!

Remember your generator probably has to work after sitting on the ground all day in the Middle East in air temperatures of +50C, as well as at -80C on a cold day at 35,000 ft!
 

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