Patent · US Active

Failsafe multimode clutch assemblies for rotorcraft

US11174013B2 · kind B2 · utility

3Cited by
8References
19Claims
0Family size

Assignee

Inventors

Key dates

Filing dateSep 29, 2020
Grant dateNov 16, 2021
Priority date
Expiry dateSep 29, 2040

Classification

  • Technology area (CPC Y)Emerging Cross-Sectional Technologies
  • CPC primaryY02T50/60
  • WIPO fieldMechanical elements
  • WIPO sectorMechanical engineering

Abstract

A failsafe multimode clutch assembly is positioned in a powertrain of a rotorcraft. The clutch assembly includes a freewheeling unit having input and output races. The freewheeling unit has a driving mode in which torque applied to the input race is transferred to the output race and an overrunning mode in which torque applied to the output race is not transferred to the input race. A bypass assembly has an engaged position that couples the input and output races of the freewheeling unit. An actuator assembly must be energized to shift the bypass assembly from the engaged position to a disengaged position. In the disengaged position, the overrunning mode of the freewheeling unit is enabled such that the clutch assembly is configured for unidirectional torque transfer. In the engaged position, the overrunning mode of the freewheeling unit is disabled such that the clutch assembly is configured for bidirectional torque transfer.

Source: USPTO / EPO open patent data. Objective bibliographic and citation counts.