Granted Patent B2

US 12,522,377 · App. 18/978,930 · Granted Jan 13, 2026

Inventors: Satya Mohan Vamsi Andalam (Bangalore, IN); Vivek Janu (Bangalore, IN); Vamshi Krishna Reddy Kommareddy (Hyderabad, IN); Sandeep Kumar (Bangalore, IN); Andrew Crispin Graham (Badminton, GB)

Assignee: General Electric Company

B64F5/60F01D21/003G01N21/9515B64F5/40F05D2260/83

Abstract

Claims (21)

1 . An apparatus for servicing internal components of a turbine engine, the apparatus comprising:

a flexible hollow tube having a length wherein the flexible hollow tube comprises a plurality of openings disposed along the length of the flexible hollow tube;

a latching mechanism connected to or incorporated with the flexible hollow tube;

a servicing device to be inserted through the flexible hollow tube, the servicing device being freely moveable through the flexible hollow tube and decoupled from the latching mechanism;

wherein the flexible hollow tube is shaped and configured so as to enable proximate positioning of the flexible hollow tube with respect to a rotatable component of a turbine engine allowing attachment of the flexible hollow tube to the rotatable component via the latching mechanism after the flexible hollow tube is inserted through an entry port of the turbine engine;

wherein the latching mechanism is configured to be attached to the rotatable component when the rotatable component is rotated; and

wherein after positioning, the servicing apparatus is to operate through different ones of the plurality of openings at different times.

2 . The apparatus of claim 1 , wherein the plurality of openings are disposed on different sides of the flexible hollow tube.

3 . The apparatus of claim 2 , wherein the plurality of openings are arranged so that the servicing device exits the flexible hollow tube in different directions.

4 . The apparatus of claim 1 , wherein the latching mechanism comprises a hook.

5 . The apparatus of claim 4 , wherein the hook is integrally formed with the flexible hollow tube.

6 . The apparatus of claim 1 , wherein the latching mechanism comprises a wedge mechanism.

7 . The apparatus of claim 1 , further comprising an adapter, the adapter to be positioned at least partially within the turbine engine and being configured to provide a guide path for the flexible hollow tube after being inserted at the entry port.

8 . The apparatus of claim 1 , wherein the servicing device is a first servicing device, the apparatus further comprising a second servicing device configured to be inserted into the flexible hollow tube after the first servicing device has been removed from the flexible hollow tube and while the flexible hollow tube remains in the turbine.

9 . The apparatus of claim 1 , wherein the flexible hollow tube is constructed of Silicone rubber or Thermoplastic elastomers (TPEs).

10 . The apparatus of claim 1 , wherein the servicing device is a borescope.

11 . The apparatus of claim 10 , wherein the borescope includes a camera.

12 . The apparatus of claim 1 , wherein the apparatus is used to perform an inspection operation.

13 . The apparatus of claim 12 , wherein the inspection operation involves an inspection of a shroud in an aircraft engine.

14 . The apparatus of claim 1 , wherein the flexible hollow tube is circular in the cross section.

15 . The apparatus of claim 1 , wherein the servicing device includes one or more of a drill, sealant dispenser, or laser energy device.

Assignments (2)

Continuity (2)

References Cited (120)