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公开(公告)号:US20200318552A1
公开(公告)日:2020-10-08
申请号:US16377351
申请日:2019-04-08
Applicant: Hamilton Sundstrand Corporation
Inventor: Eric A. Brust , Paul Henry Verstrate , Anthony L. Biermann , Derek R. Hochstetler , Jose Rafael Relampagos Ridao
Abstract: A bracket assembly for supporting terminal leads in an auxiliary generator of an aircraft, which includes a first bracket adapted and configured to be fastened to a stator housing of the generator to retain a main stator within the stator housing, and a second bracket adapted and configured to be fastened to a top surface of the first bracket to support a plurality of terminal leads in such a manner so that they are not susceptible to damage from resonance and vibration.
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公开(公告)号:US11378013B2
公开(公告)日:2022-07-05
申请号:US16377351
申请日:2019-04-08
Applicant: Hamilton Sundstrand Corporation
Inventor: Eric A. Brust , Paul Henry Verstrate , Anthony L. Biermann , Derek R. Hochstetler , Jose Rafael Relampagos Ridao
IPC: H02K3/52 , H02K5/22 , H02K3/50 , H02K5/24 , F16M13/00 , F02C7/32 , B23K37/04 , B64D41/00 , F16M13/02 , H02K1/18
Abstract: A bracket assembly for supporting terminal leads in an auxiliary generator of an aircraft, which includes a first bracket adapted and configured to be fastened to a stator housing of the generator to retain a main stator within the stator housing, and a second bracket adapted and configured to be fastened to a top surface of the first bracket to support a plurality of terminal leads in such a manner so that they are not susceptible to damage from resonance and vibration.
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