Propeller assembly including a rigging free beta tube
AssigneeGE Aviation Systems LLC
InventorNicholas Bown
Life of this patent
Estimating the term…
Abstract
An example apparatus includes a propeller assembly including a blade and a propeller shaft, the propeller shaft including a first gallery and a second gallery; and a beta tube rotationally fixed to the propeller shaft, the beta tube axially translating with respect to the propeller shaft, the beta tube including a first connection, the first connection to provide hydraulic fluid to a pitch chamber to adjust a pitch of the blade to a first pitch angle, the first connection fluidly coupled to the first gallery of the propeller shaft based on a position of the beta tube.
Claims20
An apparatus comprising:
- a propeller assembly including a blade and a propeller shaft, the propeller shaft including a first gallery;
- and
- a beta tube rotationally fixed to the propeller shaft, the beta tube axially translating with respect to the propeller shaft, the beta tube including a first connection, the first connection to provide hydraulic fluid to a pitch chamber to adjust a pitch of the blade to a first pitch angle, the first connection fluidly coupled to the first gallery of the propeller shaft based on a position of the beta tube.
An apparatus comprising:
- a blade;
- a propeller shaft coupled to the blade, the propeller shaft including a first gallery and a second gallery, the first and second galleries fluidly coupled to a pump via one or more control valves;
- and
- a beta tube rotationally fixed to the propeller shaft, the beta tube axially translating with respect to the propeller shaft, the beta tube including a first connection and a second connection, the first connection to provide hydraulic fluid to a first pitch chamber to adjust a pitch of the blade to a first pitch angle, the second connection to provide hydraulic fluid to a second pitch chamber to adjust the pitch of the blade to a second pitch angle, the first connection fluidly coupled to the first gallery of the propeller shaft based on a position of the beta tube, the second connection fluidly coupled to the second gallery of the propeller shaft.
An engine comprising:
- a low pressure shaft;
- a propeller assembly including a blade and a propeller shaft, the propeller shaft including a first gallery and a second gallery;
- a gearbox to translate a first rotation of the low pressure shaft into a second rotation of the propeller shaft, the blade to rotate with the second rotation;
- and
- a beta tube rotationally fixed to the propeller shaft, the beta tube axially translating with respect to the propeller shaft, the beta tube including a first connection and a second connection, the first connection to provide hydraulic fluid to a first pitch chamber to adjust a pitch of the blade to a first pitch angle, the second connection to provide hydraulic fluid to a second pitch chamber to adjust the pitch of the blade to a second pitch angle, the first connection fluidly coupled to the first gallery of the propeller shaft based on a position of the beta tube, the second connection fluidly coupled to the second gallery of the propeller shaft.
Dependencies are inferred from the claim text.