Gearbox mounted force generator
AssigneeSikorsky Aircraft Corporation
InventorsWilliam A. Welsh, Erez Eller, Robert K. Goodman
Life of this patent
Estimating the term…
Abstract
An active vibration control (AVC) system includes a shaft-driven gearbox mounted force generator (GMFG) mounted to a main rotor transmission. The GMFGs receive shaft power from an output shaft driven by the main rotor transmission and/or engine-to-transmission gearbox to avoid separate drive motors.
Claims26
An active vibration control system comprising:
- a first shaft defined along a first axis;
- a first gear mounted to said first shaft;
- an input shaft engaged with said first gear;
- a second gear mounted to said first shaft;
- a first mass mounted to said second gear;
- a third gear mounted to said first shaft;
- a second mass mounted to said third gear;
- a fourth gear engaged with said second gear and said third gear such that said third gear and said second gear counter-rotate;
- and
- a first differential assembly engaged with said first gear and said second gear to selectively adjust rotation of said first mass and said second mass relative said first gear to generate a first vibratory force output.
An active vibration control system comprising:
- a first shaft defined along a first axis;
- a first gear mounted to said first shaft;
- a second gear mounted to said first shaft;
- a first mass mounted to said second gear;
- a third gear mounted to said first shaft;
- a second mass mounted to said third gear;
- a fourth gear engaged with said second gear and said third gear such that said third gear and said second gear counter-rotate;
- and
- a first differential assembly engaged with said first gear and said second gear to selectively adjust rotation of said first mass and said second mass relative said first gear to generate a first vibratory force output wherein said first differential assembly comprises a clutch.
An active vibration control system comprising:
- a first shaft defined along a first axis;
- a first gear mounted to said first shaft;
- a second gear mounted to said first shaft;
- a first mass mounted to said second gear;
- a third gear mounted to said first shaft;
- a second mass mounted to said third gear;
- a fourth gear engaged with said second gear and said third gear such that said third gear and said second gear counter-rotate;
- and
- a first differential assembly engaged with said first gear and said second gear to selectively adjust rotation or said first mass and said second mass relative said first gear to generate a first vibratory force output wherein said first differential assembly comprises a magnetorheological fluid clutch.
An active vibration control system comprising:
- a helicopter transmission;
- an engine-to-transmission gearbox which drives said helicopter transmission;
- and
- a force generator mounted to said engine-to-transmission gearbox, said force generator mechanically driven by an input shaft rotated by said engine-to-transmission gearbox.
An active vibration control system comprising:
- a helicopter transmission;
- an engine-to-transmission gearbox which drives said helicopter transmission;
- and
- a force generator mounted to said engine-to-transmission gearbox, said force generator driven by an input shaft rotated by said engine-to-transmission gearbox;
- a first shaft defined along a first axis;
- a first gear mounted to said first shaft, said first gear driven by said input shaft;
- a second gear mounted to said first shaft;
- a first mass mounted to said second gear,
- a third gear mounted to said first shaft;
- a second mass mounted to said third gear;
- a fourth gear engaged with said second gear and said third gear such that said third gear and said second gear counter-rotate;
- and
- a first differential assembly engaged with said first gear and said second gear to selectively adjust rotation of said first mass and said second mass relative said first gear to generate a first vibratory force output.
An active vibration control system comprising:
- a helicopter transmission;
- an engine-to-transmission gearbox which drives said helicopter transmission;
- and
- a force generator mounted to said engine-to-transmission gearbox, said force generator driven by an input shaft rotated by said engine-to-transmission gearbox;
- and
- a second force generator mounted to said helicopter transmission, said second force generator driven by an output to a helicopter tail rotor.
An active vibration control system comprising:
- a helicopter transmission;
- and
- a force generator mounted to and mechanically driven by said helicopter transmission.
An active vibration control system comprising:
- a helicopter transmission;
- and
- a force generator mechanically driven by said helicopter transmission.
Dependencies are inferred from the claim text.