公开(公告)号：US09771149B2

公开(公告)日：2017-09-26

申请号：US14927873

申请日：2015-10-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： David Lazarovich ,  Nicolae Morcov ,  Marius Pleniceanu

IPC: G01C23/00 ,  G05D1/00 ,  G05D3/00 ,  B64C25/40 ,  B64C25/34 ,  B64C25/50 ,  B64D41/00

CPC classification number: B64C25/405 ,  B64C25/34 ,  B64C25/50 ,  B64D41/00 ,  B64D2221/00 ,  Y02T50/44 ,  Y02T50/823

Abstract: A gate departure system for an aircraft includes an electric traction motor for driving a wheel of a main landing gear assembly of the aircraft on only one side of the aircraft; and a controller selectively connected to a starter-generator of an auxiliary power unit (APU) and to the traction motor to control flow of electrical power to either the starter-generator for starting of the APU or the electric traction motor for driving the wheel.

公开(公告)号：US09787101B2

公开(公告)日：2017-10-10

申请号：US14480820

申请日：2014-09-09

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rocco DiVito ,  Hassan Ali Kojori ,  Nicolae Morcov ,  Wayne Pearson ,  Cristian Anghel

IPC: H02J4/00 ,  B60L7/16 ,  B64C25/40 ,  B64C25/42 ,  H02J7/00 ,  H02P3/14 ,  H02J1/00 ,  H02J7/14 ,  H02J7/34 ,  B60L7/10

CPC classification number: H02J4/00 ,  B60L7/10 ,  B60L7/16 ,  B60L11/1862 ,  B60L11/1868 ,  B60L2200/10 ,  B60L2210/10 ,  B60L2220/42 ,  B60L2240/547 ,  B64C25/405 ,  B64C25/42 ,  B64D2221/00 ,  H02J1/00 ,  H02J1/08 ,  H02J1/12 ,  H02J7/0055 ,  H02J7/14 ,  H02J7/345 ,  H02J2007/0059 ,  H02P3/14 ,  Y02T10/646 ,  Y02T10/7005 ,  Y02T10/7044 ,  Y02T10/7066 ,  Y02T10/7216 ,  Y02T50/823

Abstract: An electrical system for an aircraft with an electric taxi system (ETS), the electrical system may include at least one traction motor, a DC link and at least one traction-motor bidirectional DC-AC converter interposed between the at least one traction motor and the DC link. An engine-driven power source may be configured to provide DC power to the DC link or extract DC power from the DC link. A battery unit may be configured to provide DC power to the DC link or extract DC power from the DC link. An adaptive power controller may be interconnected with the power source, the battery unit and the at least one traction-motor bidirectional DC-AC converter and configured to regulate voltage of DC power delivered to the DC link.

公开(公告)号：US20170121012A1

公开(公告)日：2017-05-04

申请号：US14927873

申请日：2015-10-30

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： David Lazarovich ,  Nicolae Morcov ,  Marius Pleniceanu

IPC: B64C25/40 ,  B64C25/50 ,  B64D41/00 ,  B64C25/34

CPC classification number: B64C25/405 ,  B64C25/34 ,  B64C25/50 ,  B64D41/00 ,  B64D2221/00 ,  Y02T50/44 ,  Y02T50/823

Abstract: A gate departure system for an aircraft includes an electric traction motor for driving a wheel of a main landing gear assembly of the aircraft on only one side of the aircraft; and a controller selectively connected to a starter-generator of an auxiliary power unit (APU) and to the traction motor to control flow of electrical power to either the starter-generator for starting of the APU or the electric traction motor for driving the wheel.

公开(公告)号：US20160070266A1

公开(公告)日：2016-03-10

申请号：US14480820

申请日：2014-09-09

Applicant: HONEYWELL INTERNATIONAL INC.

Inventor： Rocco DiVito ,  Hassan Ali Kojori ,  Nicolae Morcov ,  Wayne Pearson ,  Cristian Anghel

IPC: G05D1/02 ,  H02J4/00 ,  H02J7/00

CPC classification number: H02J4/00 ,  B60L7/10 ,  B60L7/16 ,  B60L11/1862 ,  B60L11/1868 ,  B60L2200/10 ,  B60L2210/10 ,  B60L2220/42 ,  B60L2240/547 ,  B64C25/405 ,  B64C25/42 ,  B64D2221/00 ,  H02J1/00 ,  H02J1/08 ,  H02J1/12 ,  H02J7/0055 ,  H02J7/14 ,  H02J7/345 ,  H02J2007/0059 ,  H02P3/14 ,  Y02T10/646 ,  Y02T10/7005 ,  Y02T10/7044 ,  Y02T10/7066 ,  Y02T10/7216 ,  Y02T50/823

Abstract: An electrical system for an aircraft with an electric taxi system (ETS), the electrical system may include at least one traction motor, a DC link and at least one traction-motor bidirectional DC-AC converter interposed between the at least one traction motor and the DC link. An engine-driven power source may be configured to provide DC power to the DC link or extract DC power from the DC link. A battery unit may be configured to provide DC power to the DC link or extract DC power from the DC link. An adaptive power controller may be interconnected with the power source, the battery unit and the at least one traction-motor bidirectional DC-AC converter and configured to regulate voltage of DC power delivered to the DC link.

Abstract translation: 一种用于具有电动出租车系统（ETS）的飞机的电气系统，所述电气系统可以包括至少一个牵引电动机，DC链路和至少一个牵引电动机双向DC-AC转换器，其被插入在所述至少一个牵引电动机和 直流链路。 发动机驱动的电源可以被配置为向DC链路提供DC电力或从DC链路提取DC电力。 电池单元可以被配置为向DC链路提供DC电力或从DC链路提取DC电力。 自适应功率控制器可以与电源，电池单元和至少一个牵引电动机双向DC-AC转换器互连，并且被配置为调节传递到DC链路的DC功率的电压。