The XIX International Conference on Electrical Machines - ICEM 2010 2010
DOI: 10.1109/icelmach.2010.5607893
|View full text |Cite
|
Sign up to set email alerts
|

A combined electromagnetic and thermal optimisation of an aerospace electric motor

Help me understand this report

Search citation statements

Order By: Relevance

Paper Sections

Select...
3
1
1

Citation Types

0
6
0

Year Published

2011
2011
2020
2020

Publication Types

Select...
5
3

Relationship

1
7

Authors

Journals

citations
Cited by 16 publications
(7 citation statements)
references
References 18 publications
0
6
0
Order By: Relevance
“…The optimization of the fin extension , fin pitch and the number of fins which are illustrated in Fig. 1, are the main ways to increase the natural cooling performance [24][25][26][27][28][29]. The key design objective must be to maximize the rate of the heat dissipation, while minimizing the weight and volume of the cooling fins.…”
Section: A Natural Passive Coolingmentioning
confidence: 99%
See 1 more Smart Citation
“…The optimization of the fin extension , fin pitch and the number of fins which are illustrated in Fig. 1, are the main ways to increase the natural cooling performance [24][25][26][27][28][29]. The key design objective must be to maximize the rate of the heat dissipation, while minimizing the weight and volume of the cooling fins.…”
Section: A Natural Passive Coolingmentioning
confidence: 99%
“…In this paper, a detailed analysis of the active type cooling: the natural [21][22][23][24][25][26][27][28], forced air [29][30][31][32][33][34][35][36][37][38][39][40][41][42], forced liquid and phase change types [18,[66][67][68], are reviewed in Section II. On this basis, a comprehensive summary of the convection methods as applicable to the automotive traction motors cooling contexts have been provided with the advantages and disadvantages of each method being compared.…”
Section: Introductionmentioning
confidence: 99%
“…Empirical relationships are limited to the specific geometries of a given machine [6]. Flow resistance networks in conjunction with correlations [7][8][9][10][11][12] provide an improved modelling technique, but are not able to provide the detail required to accurately predict the important surface heat transfer which dictates the conduction paths within the important solid windings and laminations [6,13]. Experimental testing of surface heat transfer is expensive and discrete so does not allow a full understanding of the heat transfer at the surfaces [14].…”
Section: Introductionmentioning
confidence: 99%
“…where, , N, d, k and ∆ are maximum flux-density, the number of minor loops, thickness of the lamination material, a constant which will be chosen between k = 0.6-0.7, and the flux reversal associated with a given minor loop, respectively [13,14]. Rotor eddy-current loss becomes the dominant loss mechanism, contributing 83% of the total loss [15].…”
Section: Losses Calculation Of the Arwmmentioning
confidence: 99%