Nacelle deflection measurement assembly
A deflection measurement assembly according to an example of the present disclosure includes, among other things, a nacelle arranged about an axis to define a flow path, a cable assembly arranged at least partially about the axis, and a transducer coupled to the cable assembly.
1. A propulsion system, comprising:
a gas turbine engine defining an engine axis, the engine including a turbine section configured to drive a fan section;
a nacelle assembly including a fan nacelle and a core cowling arranged about the engine axis to define a bypass flow path, and the core cowling defining a core flow path, the fan nacelle including a stationary first nacelle section and a second nacelle section, the second nacelle section axially moveable along the engine axis in a direction away from the first nacelle section such that the second nacelle section defines a radial opening to the bypass flow path; and
a deflection measurement assembly, comprising:
a cable assembly coupled to the nacelle assembly, wherein the cable assembly includes at least one cable disposed at least partially about a perimeter of the second nacelle section; and
a transducer coupled to the cable assembly, the transducer configured to be actuated in response to a change in a cross-sectional area of at least one of the bypass flow path and the core flow path.
2. The propulsion system as recited in claim 1 , wherein the transducer is a linear variable differential transducer.
3. The propulsion system as recited in claim 1 , wherein the cable assembly is arranged at least partially about the engine axis.
4. The propulsion system as recited in claim 1 , comprising a controller coupled to the transducer, the controller operable to determine a deflection of the nacelle assembly based upon the change in the cross-section area.
5. The propulsion system as recited in claim 1 , wherein the fan nacelle is fixedly attached to a pylon, the transducer is coupled to a first end of the at least one cable, and a second end of the at least one cable is coupled to the pylon.
6. The propulsion system as recited in claim 2 , comprising:
a controller coupled to the transducer, the controller operable to determine a deflection of the nacelle assembly based upon the change in the cross-section area.
7. A method of measuring deflection of a nacelle assembly, comprising:
providing a nacelle defining a flow path that extends along an engine axis, the nacelle including a stationary first nacelle section and a second nacelle section, the second nacelle section axially moveable along the axis in a direction away from the first nacelle section such that the second nacelle section a radial opening to the flow path;
positioning a cable assembly about the engine axis, the cable assembly moveable relative to the axis in response to a change in a cross-sectional area of the flow path, wherein the cable assembly includes at least one cable disposed at least partially about a perimeter of the second nacelle section; and
actuating a transducer is response to movement of the cable assembly.
8. The method as recited in claim 7 , wherein the transducer is coupled to a first end of the at least one cable.
9. The method as recited in claim 7 , comprising determining a deflection of the nacelle at a location adjacent to the cable assembly based upon the step of actuating the transducer.
10. The method as recited in claim 9 , wherein the step of determining the deflection of the nacelle includes comparing the change in the cross-section area to a predetermined quantity.
11. The propulsion system as recited in claim 6 , wherein the fan nacelle is fixedly attached to a pylon, the transducer is coupled to a first end of the at least one cable, and a second end of the at least one cable is coupled to the pylon.