公开(公告)号：US20220245063A1

公开(公告)日：2022-08-04

申请号：US17586913

申请日：2022-01-28

Applicant: AIRBUS OPERATIONS LIMITED ,  AIRBUS OPERATIONS (S.A.S.)

Inventor： Louis-Emmanuel ROMANA ,  George HOWELL

IPC: G06F11/36

Abstract: A method of testing a system model is disclosed. The system model includes a system parameter and three or more equipment models, each equipment model includes an equipment parameter which models a parameter of a respective equipment. The method includes (a) making a series of changes of the equipment parameter of one of the equipment models so that the equipment parameter of the one of the equipment models adopts a series of test values of the equipment parameter; (b) operating the system model to determine a series of test values of the system parameter, each test value of the system parameter is determined in accordance with a respective one of the test values of the equipment parameter; (c) determining a weight of the selected one of the equipment models, the weight of the one of the equipment models indicates a sensitivity of the system parameter to the series of changes in the equipment parameter of the one of the equipment models; and (d) outputting the weight of the one of the equipment models.

公开(公告)号：US20140209739A1

公开(公告)日：2014-07-31

申请号：US14167095

申请日：2014-01-29

Applicant: AIRBUS OPERATIONS S.A.S.

Inventor： Matthieu MAYOLLE ,  Caroline ACANFORA ,  Louis-Emmanuel ROMANA ,  Julien FONTAN

IPC: B64C25/48

CPC classification number: B64C25/48 ,  B60T8/1703 ,  B60T2201/16 ,  B64C25/50

Abstract: The device includes, but is not limited to a calculating unite for automatically applying, if conditions for turning of the aircraft are met, a symmetrical braking value at a brake assembly, then in the course of the turn automatically distributing this symmetrical braking value in differential braking between braking device of the left main landing gear and braking device of the right main landing gear of the aircraft, as a function of current directional command orders, in such a way as to maintain a constant overall braking level, at least for directional command orders below a predetermined threshold.

Abstract translation: 该装置包括但不限于如果满足飞行器转动条件的自动应用的计算联合，在制动组件处的对称制动值，则在转向过程中自动将该对称制动值分配在差速器 至少对于方向指令，左主起落架的制动装置与飞机的右主起落架的制动装置之间的制动作为当前方向指令命令的函数，以保持恒定的总制动水平 低于预定阈值。