Designing power cables that provide high power and low system mass is one of the major goals in achieving the future all-electric wide-body aircraft. Radiative and convective heat transfers from a cable's surface to the surrounding air determine how much current is permitted to flow through it. At a cruising altitude of 12.2 km (18.8 kPa) for wide-body aircraft, the limited heat transfer by convection poses thermal issues for the design of aircraft cables. These thermal challenges are exacerbated for bipolar electric power systems (EPS), which are usually made up of two power lines next to each other. The cable's surface area affects both convective and radiative heat transfers. Changing the shape of the cable is one technique to improve heat transfers and compensate for the reduced convective heat transfer caused by low air pressure. In comparison to cylindrical and cuboid cables, the rectangular geometry design gives a bigger contact area with the surrounding atmosphere for the same cross-section area, hence it is anticipated that the heat transfer would rise and as a result, the cable's maximum power-carrying capability will be higher. The purpose of this paper is to design ±5 kV bipolar MVDC power cables with rectangular geometry to raise the maximum current carrying capacity of the cable and analyze its performance with bipolar cylindrical and cuboid geometries.
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Optimized Design of ±5 kV, 1 kA Rectangular Power Cable for a Low Pressure of 18.8 kPa for Envisioned All-Electric Wide-Body Aircraft
Power cables, one of the key components of electric power systems (EPS) in future wide-body all-electric aircraft (AEA), have a lot of room for improvement in achieving low system mass leading to high power density designs. The limited heat transfer by convection at a cruising altitude of 12.2 km (18.8 kPa) presents thermal issues for the design of aircraft power cables. The surface area of the cable influences both convective and radiative heat transfers. One way to improve radiative heat transfers and make up for the lower convective heat transfer caused by the low air pressure is to change the shape of the cable. The rectangular geometry design of cables offers a larger contact area with the surrounding atmosphere compared to cylindrical and cuboid cables of the same cross-sectional area. This paper presents the design and analysis of rectangular bipolar MVDC power cables in addition to cuboid, coaxial, and conventional cylindrical bipolar cables to determine the optimized bipolar MVDC power cable system for future wide-body AEA. To compare these designs, a parameter J is introduced that quantifies the product of the overall mass per unit length of the cables and their cross-sectional area. According to the findings, the rectangular bipolar cable systems demonstrated superior performance compared to other bipolar cable systems in terms of J and would be a solution for future wide-body AEA.
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- Award ID(s):
- 2306093
- PAR ID:
- 10492455
- Publisher / Repository:
- IEEE
- Date Published:
- Journal Name:
- IEEE Access
- ISSN:
- 2169-3536
- Page Range / eLocation ID:
- 1 to 1
- Subject(s) / Keyword(s):
- all-electric aircraft (AEA), coaxial cable, cuboid geometry, low pressure, MVDC power cables, multilayer insulation, rectangular geometry, thermal analysis
- Format(s):
- Medium: X
- Sponsoring Org:
- National Science Foundation
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