US 12,278,523 B2
Electrical machine
Nadhem Boubaker, Buckinghamshire (GB)
Assigned to SAFRAN ELECTRICAL & POWER UK LTD., Buckinghamshire (GB)
Appl. No. 17/913,993
Filed by SAFRAN ELECTRICAL & POWER UK LTD., Buckinghamshire (GB)
PCT Filed Apr. 1, 2021, PCT No. PCT/EP2021/058700
§ 371(c)(1), (2) Date Sep. 23, 2022,
PCT Pub. No. WO2021/204693, PCT Pub. Date Oct. 14, 2021.
Claims priority of application No. 2005018 (GB), filed on Apr. 6, 2020.
Prior Publication US 2023/0126330 A1, Apr. 27, 2023
Int. Cl. H02K 11/00 (2016.01); H02K 1/16 (2006.01); H02K 1/27 (2022.01); H02K 11/225 (2016.01); H02K 11/25 (2016.01); H02K 11/33 (2016.01)
CPC H02K 11/225 (2016.01) [H02K 1/165 (2013.01); H02K 1/27 (2013.01); H02K 11/25 (2016.01); H02K 11/33 (2016.01)] 19 Claims
OG exemplary drawing
 
1. An electrical machine for use in an aircraft, comprising:
a rotor that includes a plurality of rotor poles; and
a stator that includes a plurality of phases, wherein each respective phase of the plurality of phases occupies at least one elementary block, the at least one elementary block of each phase comprising a set of conductors of the respective phase wound around a plurality of slots of the respective elementary block in a concentrated winding configuration;
wherein the stator further comprises at least one sensor located between two elementary blocks, the at least one sensor being configured to measure at least one parameter of the rotor, and wherein the at least one sensor comprises at least one sensor coil wound around a pair of adjacent slots.