Imaging systems and methods for data-driven apparatus inspection
Systems and methods for imaging are provided. For example, a system may include an imaging probe that comprises a housing, an imaging portion comprising a camera, and a processor. The housing may be mountable to an inspection window of an apparatus, providing a view into an interior portion of the apparatus with one or more rotatable components therein. The imaging portion may be (a) extendable out of the housing and into the interior portion of the apparatus such that the camera are positioned within the interior portion of the apparatus and (b) retractable into the housing such that the camera are not positioned within the interior portion of the apparatus. The processor may automatically extend and retract the imaging portion and capture a plurality of images of the one or more rotatable components when the imaging portion is extended.
1. An imaging system comprising:
an imaging probe, the imaging probe comprising:
a housing mountable to an inspection window of an apparatus, the inspection window providing a view into an interior portion of the apparatus with one or more components therein;
an imaging portion comprising a camera, wherein the imaging portion is (a) extendable at least partially out of the housing and into the interior portion of the apparatus to position the camera within the interior portion of the apparatus and (b) retractable from the interior portion of the apparatus to remove the camera from within the interior portion of the apparatus into the housing; and
a processor that automatically controls extension and retraction of the imaging portion and controls capturing a plurality of images of the one or more components using the imaging portion when the imaging portion is extended.
2. The system of claim 1 , wherein the processor controls automatic extension of the imaging portion during shutdown of the apparatus.
3. The system of claim 1 , wherein the one or more components comprise one or more rotatable components.
4. The system of claim 3 , wherein the processor controls automatically extending the imaging portion when the apparatus has been switched off and the one or more rotatable components have a rotational speed that is decreasing and is below a predetermined threshold rotational speed.
5. The system of claim 3 , wherein the processor controls automatically retracting the imaging portion after a predetermined amount of time has lapsed since the apparatus has been switched off.
6. The system of claim 1 , wherein the processor controls selectively extending and/or retracting the imaging portion based on user input.
7. The system of claim 1 , wherein the processor controls automatically transmitting the captured plurality of images to a probe monitoring device, the probe monitoring device comprising a monitoring device processor for (a) receiving the plurality of images from the imaging probe, (b) analyzing the plurality of images using a data model to identify damage to the one or more components, and (c) generating a report indicating a presence or absence of identified damage to the one or more components.
8. The system of claim 1 , wherein the imaging portion further comprises a light.
9. The system of claim 1 , wherein the apparatus is a gas turbine engine on an aircraft, wherein the one or more components comprise a plurality of turbine blades, and wherein the processor automatically extends the imaging portion when one or more of (a) the aircraft engine is at cut-off by a throttle of the aircraft and/or an engine cut off switch of the aircraft, (b) the plurality of turbine blades has a rotational speed that is decreasing and is below a predetermined threshold rotational speed, and (c) a weight-on-wheels switch of the aircraft is activated.
10. The system of claim 9 , wherein the processor controls automatically retracting the imaging portion if the imaging portion is extended and (a) after a predetermined amount of time has lapsed since the aircraft engine has been switched off or (b) when the throttle of the aircraft is at an idle position and an engine start switch of the aircraft is in an on position.
11. A method for imaging one or more components within an interior portion of an apparatus using an imaging probe mounted to an inspection window of the apparatus, the inspection window providing a view into the interior portion of the apparatus, the method comprising
automatically extending, at least partially, an imaging portion of the imaging probe out of a housing of the imaging probe and into the interior portion of the apparatus such that a camera of the imaging portion are positioned within the interior portion of the apparatus;
automatically capturing, by the camera of the imaging portion, a plurality of images of the one or more components when the imaging portion is extended; and
automatically retracting, at least partially, the imaging portion into the housing such that the camera are not positioned within the interior portion of the apparatus.
12. The method of claim 11 , wherein the imaging portion is automatically extended during shutdown of the apparatus.
13. The method of claim 11 , wherein the one or more components comprise one or more rotatable components.
14. The method of claim 13 , wherein the imaging portion is automatically extended when the apparatus has been switched off and the one or more rotatable components have a rotational speed that is decreasing and is below a predetermined threshold rotational speed.
15. The method of claim 13 , wherein the imaging portion is automatically retracted after a predetermined amount of time has lapsed since the apparatus has been switched off.
16. The method of claim 11 , further comprising selectively extending and retracting the imaging portion based on user input.
17. The method of claim 11 , further comprising:
analyzing the plurality of images using a data model to identify damage to the one or more components; and
generating a report indicating a presence or absence of identified damage to the one or more components.
18. The method of claim 11 , wherein the apparatus is a gas turbine engine on an aircraft;
wherein the one or more components comprise a plurality of turbine blades; and
wherein the imaging portion is automatically extended when one or more of (a) the aircraft engine is at cut-off by throttle of the aircraft and/or an engine cut off switch of the aircraft, (b) the plurality of turbine blades has a rotational speed that is decreasing and is below a predetermined threshold rotational speed, and (c) a weight-on-wheels switch of the aircraft is activated.
19. The method of claim 18 , wherein the imaging portion is automatically retracted if the imaging portion is extended and (a) after a predetermined amount of time has lapsed since the aircraft engine has been switched off or (b) when the throttle of the aircraft is at an idle position and an engine start switch of the aircraft is in an on position.
20. A computer program product comprising at least one non-transitory computer-readable storage medium having computer program code thereon that, in execution with at least one processor, is configured for:
automatically extending, at least partially, an imaging portion of an imaging probe out of a housing of the imaging probe and into an interior portion of an apparatus such that a camera of the imaging portion is positioned within the interior portion of the apparatus;
automatically capturing, by the camera of the imaging portion, a plurality of images of one or more components within the interior portion of the apparatus when the imaging portion is extended; and
automatically retracting, at least partially, the imaging portion into the housing such that the camera is not positioned within the interior portion of the apparatus.