Device for cleaning a turbomachine module

Patent metadata

Field	Value
Publication number	US-10344617-B2
Application number	US-201415104120-A
Country	US
Kind code	B2
Filing date	Dec 5, 2014
Priority date	Dec 16, 2013
Publication date	Jul 9, 2019
Grant date	Jul 9, 2019

Abstract

A device for cleaning, for example degritting or desanding, a turbomachine module comprising: (i) structure for isolating bearings of the module, by containment in a closed enclosure; (ii) structure for overpressurizing said enclosure; (iii) means for stripping material deposited in the walls of annular recesses of the module; and (iv) structure for sucking up the material thus stripped.

First claim

The invention claimed is:

1. Device for cleaning a turbine engine module, said module comprising rotor discs defining between them at least one annular cavity to be cleaned, these discs extending around at least one bearing, the device comprising:
means for isolating said at least one bearing which is, at least in part, to be surrounded by said at least one annular cavity to be cleaned,
means for establishing an excess pressure in said means for isolating,
means for removing material deposited on at least one wall of said at least one cavity in the module, and
means for suctioning removed material.

2. Device according to claim 1 , wherein the means for isolating comprise two annular members configured so as to be mounted coaxially in front of and behind the module, respectively.

3. Device according to claim 2 , wherein each of the members comprises annular sealing means configured so as to cooperate with an annular element of the module.

4. Device according to claim 2 , wherein a first of the members comprises an annular skirt which is made of a resilient material and is elastically deformable between a first position in which it is substantially cylindrical and a second position in which it is substantially frustoconical and is capable of cooperating, by its external periphery, with a first annular element of the module, such as the internal periphery of a rotor disc.

5. Device according to claim 4 , wherein the first member comprises an air chamber that is inflatable and radially expandable, and is surrounded by the annular skirt so that the inflation and radial expansion of the air chamber causes deformation of the skirt from its first to its second position.

6. Device according to claim 5 , wherein the air chamber is equipped with a valve that is connected to one end of a hose, the opposite end of which is located substantially at one end of the first member.

7. Device according to claim 2 , wherein a second of the members comprises a cylindrical sleeve configured to receive a shaft of the module, this sleeve comprising a first closed end and a second end comprising means for fixing on a second annular element of the module, such as a cylindrical wall of the module.

8. Device according to claim 7 , wherein the second end of the sleeve is connected to the internal periphery of an annular membrane, the external periphery of which comprises said means for fixing to the second element of the module, said membrane preferably being made of a resilient material.

9. Device according to claim 7 , wherein the sleeve comprises a pressure relief valve.

10. Device according to claim 1 , wherein the suctioning means comprise a bell housing configured so as to be mounted coaxially with the module and comprising means for connecting to a suction unit.

11. Device according to claim 10 , wherein the bell housing comprises, at its top, an opening for the sleeve to pass through.

12. Device according to claim 10 , wherein the suctioning means further comprise an annular plate that is coaxial with the bell housing, this plate being configured so as to be applied to the module and comprising means for rotationally guiding the bell housing about its axis.

13. Device according to claim 10 , wherein the bell housing comprises a window for access to said at least one annular cavity in the module and for manipulation of said removing means.

14. Device according to claim 1 , wherein it comprises a carriage comprising means for supporting and rotationally guiding the module about its longitudinal axis, which is oriented substantially vertically.

15. Method for cleaning a turbine engine module, said module comprising rotor discs defining between them at least one annular cavity to be cleaned, these discs extending around at least one bearing, the method comprising:
providing a device for cleaning comprising:
means for isolating said at least one bearing which is, at least in part, to be surrounded by said at least one annular cavity to be cleaned,
means for establishing an excess pressure in said means for isolating,
means for removing material deposited on at least one wall of said at least one cavity in the module, and
means for suctioning removed material,

isolating said at least one bearing by confining it in said means for isolating,
establishing an excess pressure in said means for isolating, and
removing the material deposited on at least one wall of said at least one cavity in the module, and simultaneously suctioning the material thus removed.

16. Device according to claim 7 , wherein the sleeve comprises means for connection to said means for establishing excess pressure.

Assignees

• Snecma
• Safran Aircraft Engines

Inventors

• Domalain Vincent
• Gourlet Frédéric
• Vareecke Sylvain

Classifications

• F05D2220/323

  for aircraft propulsion, e.g. jet engines · CPC title

• B08B17/04

  by using removable coverings · CPC title

• F01D25/002 Primary

  Cleaning of turbomachines · CPC title

• F01D5/06

  Rotors for more than one axial stage, e.g. of drum or multiple disc type; Details thereof, e.g. shafts, shaft connections {(F01D5/022, F01D5/023 take precedence)} · CPC title

• F01D25/16

  Arrangement of bearings; Supporting or mounting bearings in casings (bearings per se F16C) · CPC title