发明名称 |
DIFFERENTIAL BRAKING OF AIRCRAFT LANDING GEAR WHEELS |
摘要 |
A method of braking left and right landing gear wheels on respective left and right sides of an aircraft. A desired left braking parameter (L) is received for the left wheel and a desired right braking parameter (R) is received for the right wheel. The left wheel is braked with a reduced left braking parameter (L′) which is less than the desired left braking parameter (L), and the right wheel is braked with a reduced right braking parameter (R′) which is less than the desired right braking parameter (R). A difference between the braking parameters is maintained so that L′−W=L−R. |
申请公布号 |
US2016016661(A1) |
申请公布日期 |
2016.01.21 |
申请号 |
US201514802268 |
申请日期 |
2015.07.17 |
申请人 |
AIRBUS OPERATIONS LIMITED ;AIRBUS OPERATIONS SAS |
发明人 |
HOWELL George;BEN Livier;ROMANA Louis-Emmanuel |
分类号 |
B64C25/48 |
主分类号 |
B64C25/48 |
代理机构 |
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代理人 |
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主权项 |
1. A method of braking left and right landing gear wheels on respective left and right sides of an aircraft, the method comprising: receiving a desired left braking parameter (L) for the left wheel; receiving a desired right braking parameter (R) for the right wheel; braking the left wheel with a reduced left braking parameter (L′) which is less than the desired left braking parameter (L); and braking the right wheel with a reduced right braking parameter (R′) which is less than the desired right braking parameter (R), wherein L′−R′=L−R. |
地址 |
Bristol GB |