Aircraft electric motor
Abstract
Aircraft electric motors are described. The aircraft electric motors include a motor unit having a rotor and a stator, wherein the stator includes a plurality of windings and cooling channels arranged to provide cooling to the plurality of windings, a drive unit configured to drive operation of the motor unit, and a cooling system having at least one directional feature forming a portion of at least one cooling channel, the at least one directional feature configured to prevent backflow of a cooling fluid that passes through the at least one cooling channel.
- Inventors:
- Issue Date:
- Research Org.:
- Hamilton Sundstrand Corporation, Charlotte, NC (United States)
- Sponsoring Org.:
- USDOE
- OSTI Identifier:
- 2293872
- Patent Number(s):
- 11817761
- Application Number:
- 17/519,749
- Assignee:
- Hamilton Sundstrand Corporation (Charlotte, NC)
- DOE Contract Number:
- AR0001351
- Resource Type:
- Patent
- Resource Relation:
- Patent File Date: 11/05/2021
- Country of Publication:
- United States
- Language:
- English
Citation Formats
Alahyari, Abbas A., Turney, Joseph, Tangudu, Jagadeesh Kumar, and Saviers, Kimberly Rae. Aircraft electric motor. United States: N. p., 2023.
Web.
Alahyari, Abbas A., Turney, Joseph, Tangudu, Jagadeesh Kumar, & Saviers, Kimberly Rae. Aircraft electric motor. United States.
Alahyari, Abbas A., Turney, Joseph, Tangudu, Jagadeesh Kumar, and Saviers, Kimberly Rae. Tue .
"Aircraft electric motor". United States. https://www.osti.gov/servlets/purl/2293872.
@article{osti_2293872,
title = {Aircraft electric motor},
author = {Alahyari, Abbas A. and Turney, Joseph and Tangudu, Jagadeesh Kumar and Saviers, Kimberly Rae},
abstractNote = {Aircraft electric motors are described. The aircraft electric motors include a motor unit having a rotor and a stator, wherein the stator includes a plurality of windings and cooling channels arranged to provide cooling to the plurality of windings, a drive unit configured to drive operation of the motor unit, and a cooling system having at least one directional feature forming a portion of at least one cooling channel, the at least one directional feature configured to prevent backflow of a cooling fluid that passes through the at least one cooling channel.},
doi = {},
journal = {},
number = ,
volume = ,
place = {United States},
year = {2023},
month = {11}
}
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