公开(公告)号：US10604240B2

公开(公告)日：2020-03-31

申请号：US15853408

申请日：2017-12-22

申请人： Brian Goyez ,  Dominique Onfroy ,  Olivier Frey

发明人： Brian Goyez ,  Dominique Onfroy ,  Olivier Frey

IPC分类号： B64C25/44 ,  B60T8/17 ,  B60T13/74 ,  B60T8/172 ,  B60T8/32 ,  F16D65/18 ,  F16D121/24

摘要： A braking system architecture for aircraft, the architecture comprising: a brake including friction members and electromechanical actuators for exerting a braking torque on the wheel; a computer situated in the fuselage of the aircraft and arranged to produce first control signals; and a junction box situated on the undercarriage, the junction box being connected to the computer and to the electromechanical actuators, the junction box being configured to receive the first control signals and to use the first control signals to produce second control signals for application to the electromechanical actuators in order to control the electromechanical actuators.

公开(公告)号：US20180178905A1

公开(公告)日：2018-06-28

申请号：US15853408

申请日：2017-12-22

申请人： Brian Goyez ,  Dominique Onfroy ,  Olivier Frey

发明人： Brian Goyez ,  Dominique Onfroy ,  Olivier Frey

IPC分类号： B64C25/44 ,  B60T8/17 ,  B60T8/32 ,  B60T8/172 ,  F16D65/18

CPC分类号： B64C25/44 ,  B60T8/1703 ,  B60T8/172 ,  B60T8/325 ,  B60T13/741 ,  F16D65/18 ,  F16D2121/24

摘要： A braking system architecture for aircraft, the architecture comprising: a brake including friction members and electromechanical actuators for exerting a braking torque on the wheel; a computer situated in the fuselage of the aircraft and arranged to produce first control signals; and a junction box situated on the undercarriage, the junction box being connected to the computer and to the electromechanical actuators, the junction box being configured to receive the first control signals and to use the first control signals to produce second control signals for application to the electromechanical actuators in order to control the electromechanical actuators.