Abstract:
A disclosed lubrication system for turbofan engine includes a primary lubricant circuit, a primary pump driving lubricant through the primary circuit, an auxiliary lubricant circuit in communication with the primary lubricant circuit and an auxiliary lubricant pump driving lubricant through the auxiliary lubricant circuit. A first valve downstream of an outlet of auxiliary lubricant pump separates the auxiliary lubricant circuit from the primary lubricant circuit. A sensor is disposed within the auxiliary lubricant circuit for sensing pressure within the auxiliary lubricant circuit separate from a pressure within the primary lubricant circuit.
Abstract:
A lubrication system includes a shaft rotatable about an axis, a lubrication pump configured to supply a lubricant flow to a gear system, and a gear train coupled to the shaft and configured to drive the lubrication pump in a first direction responsive to rotation of the shaft in both the first direction and a second direction. A gas turbine engine and method are also disclosed.
Abstract:
What is described is a system for pumping lubricant to a component of a gas turbine engine (20). The system includes a fan gear (200; 600) coupled to a fan shaft (98) of the gas turbine engine (20) and configured to rotate in a forward direction and in a reverse direction based at least partially on a direction of wind relative to a fan (42) of the gas turbine engine (20). The system also includes a first pump (206; 606) coupled to the fan gear (200; 600) and configured to pump lubricant to the component in response to the fan (42) rotating in the forward direction. The system also includes a second pump (208; 604) coupled to the fan gear (200; 600) and configured to pump lubricant to the component in response to the fan (42) rotating in the reverse direction.
Abstract:
A pump assembly includes a first stage including a first inlet in communication with a first cavity, and a first pumping means disposed within the first cavity. A second stage includes a second inlet in communication with a second cavity, an outlet in communication with both the first and the second cavity, and a second pumping means disposed within the second cavity. A transfer plate is disposed between the first stage and the second stage. The transfer plate includes a transfer window. The entire transfer window is disposed horizontally above the first pumping means and the second pumping means.
Abstract:
A lubrication system includes a shaft rotatable about an axis, a lubrication pump configured to supply a lubricant flow to a gear system, and a gear train coupled to the shaft and configured to drive the lubrication pump in a first direction responsive to rotation of the shaft in both the first direction and a second direction. A gas turbine engine and method are also disclosed.
Abstract:
A disclosed lubrication system for turbofan engine includes a primary lubricant circuit, a primary pump driving lubricant through the primary circuit, an auxiliary lubricant circuit in communication with the primary lubricant circuit and an auxiliary lubricant pump driving lubricant through the auxiliary lubricant circuit. A first valve downstream of an outlet of auxiliary lubricant pump separates the auxiliary lubricant circuit from the primary lubricant circuit. A sensor is disposed within the auxiliary lubricant circuit for sensing pressure within the auxiliary lubricant circuit separate from a pressure within the primary lubricant circuit.
Abstract:
A debris discourager for a gas turbine engine is rotatable about an engine axis and extends between a fore end and an aft end. A portion of the debris discourager includes a non-uniform surface that generates a wind flow to prevent debris from entering a sealed interface.