A gas turbine engine propulsion system includes a gas turbine engine, a fuel storage tank and a pump unit. The gas turbine engine provides propulsive forces to move a vehicle. The fuel storage tank stores a fuel that can be used to power the gas turbine engine. The pump unit displaces a fuel flow from the fuel storage tank and delivers the fuel flow to the gas turbine engine.

A gas turbine engine propulsion system includes a gas turbine engine, a fuel storage tank and a pump unit. The gas turbine engine provides propulsive forces to move a vehicle. The fuel storage tank stores a fuel that can be used to power the gas turbine engine. The pump unit displaces a fuel flow from the fuel storage tank and delivers the fuel flow to the gas turbine engine.

A probe adapter includes an adapter body including a probe aperture and a slot. The probe adapter further includes a driver slidably mounted within the slot and slidable between a first position and a second position. The driver includes a first end and a second end opposite the first end. The first end includes a ramped recess extending in a direction from the first end toward the second end. The probe adapter further includes a threaded fastener configured to contact the second end of the driver so as to retain the driver in the first position.

A probe adapter includes an adapter body including a probe aperture and a slot. The probe adapter further includes a driver slidably mounted within the slot and slidable between a first position and a second position. The driver includes a first end and a second end opposite the first end. The first end includes a ramped recess extending in a direction from the first end toward the second end. The probe adapter further includes a threaded fastener configured to contact the second end of the driver so as to retain the driver in the first position.

A system for imaging a component defining a negative space is provided comprising a component imaging assembly, a bolus insert, and an imaging device. The bolus insert is positionable in the component's negative space when the component is positioned within an imaging device imaging field to produce a component image. A method is provided comprising positioning a bolus insert within a component's negative space and scanning the component having the bolus insert to create an image of the component. A component imaging assembly is provided comprising a component including a first portion having a first thickness that is greater than a second thickness of a second portion; and a bolus insert positioned adjacent the second portion that has a bolus thickness substantially similar to a difference between the first and second thicknesses. The bolus insert has a bolus material density within fifteen percent (15%) of a component material density.

A system for imaging a component defining a negative space is provided comprising a component imaging assembly, a bolus insert, and an imaging device. The bolus insert is positionable in the component's negative space when the component is positioned within an imaging device imaging field to produce a component image. A method is provided comprising positioning a bolus insert within a component's negative space and scanning the component having the bolus insert to create an image of the component. A component imaging assembly is provided comprising a component including a first portion having a first thickness that is greater than a second thickness of a second portion; and a bolus insert positioned adjacent the second portion that has a bolus thickness substantially similar to a difference between the first and second thicknesses. The bolus insert has a bolus material density within fifteen percent (15%) of a component material density.

An acquisition unit is configured to acquire measurement values of a target device. The measurement values that are acquired include at least a temperature and a flow rate of an input fluid to be input to the target device, and a temperature and a flow rate of an output fluid to be output from the target device. A correction unit is configured to obtain a correction measurement value by which the measurement values are corrected through thermal equilibrium calculations based on the measurement values. A distance calculation unit is configured to calculate a Mahalanobis distance with a factor of the correction measurement value.

An acquisition unit is configured to acquire measurement values of a target device. The measurement values that are acquired include at least a temperature and a flow rate of an input fluid to be input to the target device, and a temperature and a flow rate of an output fluid to be output from the target device. A correction unit is configured to obtain a correction measurement value by which the measurement values are corrected through thermal equilibrium calculations based on the measurement values. A distance calculation unit is configured to calculate a Mahalanobis distance with a factor of the correction measurement value.

A method for gathering flight load data for a gas turbine engine includes providing a plurality of blocker doors rotatably mounted to a translating sleeve and a plurality of blocker door islands, each blocker door island disposed between circumferentially adjacent blocker doors of the plurality of blocker doors and mounted to at least one mounting point of the translating sleeve, wherein a blocker door island of the plurality of blocker door islands is a data acquisition unit; and connecting the data acquisition unit to at least one sensor in communication with the translating sleeve.

A method for gathering flight load data for a gas turbine engine includes providing a plurality of blocker doors rotatably mounted to a translating sleeve and a plurality of blocker door islands, each blocker door island disposed between circumferentially adjacent blocker doors of the plurality of blocker doors and mounted to at least one mounting point of the translating sleeve, wherein a blocker door island of the plurality of blocker door islands is a data acquisition unit; and connecting the data acquisition unit to at least one sensor in communication with the translating sleeve.