| 摘要 |
An accessory apparatus (76) for a gas turbine engine (10) having a first shaft (48, 50) that rotates when the gas turbine engine (10) is energized. The accessory apparatus (76) includes a mount rail (78) attached to the gas turbine engine (10) and extending parallel to the first shaft (48, 50) of the gas turbine engine (10) a first accessory (80) having a first mounting block (88), to mount the first accessory (80) to the mount rail (78), and an first accessory shaft (90) to power the first accessory (80) and a second accessory (82) having a second mounting block (88), to mount the second accessory (82) to the mount rail (78), and a second accessory shaft (92) to power the second accessory (82). |
