초록

The torque transmission system for an aircraft engine permits a starter-generator to drive the engine on starting at a speed reducing ratio. Once the engine is running, the engine then drives the starter-generator also at a speed reducing ratio.

대표청구항 ▼

1. An aircraft engine comprising a starter-generator drivingly connected to a drive shaft through a transmission, the transmission having a first speed reducing transmission ratio when driven by the starter-generator and having a second speed reducing transmission ratio when driven by the drive shaf

1. An aircraft engine comprising a starter-generator drivingly connected to a drive shaft through a transmission, the transmission having a first speed reducing transmission ratio when driven by the starter-generator and having a second speed reducing transmission ratio when driven by the drive shaft; the starter-generator being drivingly connected to the drive shaft at the first ratio through a first unidirectional clutch and the drive shaft being drivingly connected to the starter-generator at the second ratio through a second unidirectional clutch; wherein at least one of the first ratio and the second ratio is constant at all rotation speeds. 2. The engine as defined in claim 1, wherein the transmission includes a first set of meshed gears corresponding to the first ratio, and a second set of meshed gears corresponding to the second ratio. 3. The engine as defined in claim 2, wherein each of the first and second clutches includes a sprag. 4. The engine as defined in claim 1, wherein the first ratio is less than the second ratio, such that the second ratio reduces an output speed of the transmission more than the first ratio. 5. The engine as defined in claim 2, wherein the other of the first ratio and the second ratio is variable. 6. The engine as defined in claim 1, wherein the first ratio and the second ratio are each constant at all rotation speeds.