24-11-2022 дата публикации
Номер: WO2022245363A1
Methods, apparatus, systems and articles of manufacture are disclosed. An apparatus for mounting a gas turbine engine (100, 1100, 1200, 1300, 400) to a pylon (202, 402, 604, 608, 704), the gas turbine (400) including an upstream section and a downstream section (136), the gas turbine (400) defining a roll axis, a yaw axis, and a pitch axis, the apparatus including: a first mount (404) to couple the upstream section of the gas turbine engine (100, 1100, 1200, 1300, 400) to the pylon (202, 402, 604, 608 704); a second mount (404) to couple the upstream section of the gas turbine engine (100, 1100, 1200, 1300, 400) to the pylon (202, 402, 604, 608, 704), the second mount (404) downstream of the first mount (404); a thrust linkage (208, 408) to couple the upstream section to the pylon (202, 402, 604, 608, 704), wherein the downstream section (136) is decouplable from the upstream section without decoupling (1004, 904, 912) the first mount (404), the second mount (404), and the thrust linkage (208, 408).
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