BACKGROUND
The present invention relates generally to turbomachines and, more specifically, to the drilling of holes in a turbomachine casing section without having to remove and relocate the casing section to a work area.
There are occasions when it is necessary to install ancillary components, for example, engine health sensor packages or other instrumentation, on a turbine and/or compressor casing. Typically, multiple holes are drilled into the casing in order to mount the various components and/or sensors. Because of the potential and even likely damage to rotating rotor components caused by loose drill chips or shavings, the casing section (generally the upper casing section) is removed completely from the lower casing section and placed on the ground or other supporting structure, away from the lower casing section. While this approach eliminates the concern for loose drill chips or shavings during subsequent turbine operation, it requires additional heavy-duty equipment and costly extended engine downtime.
It would therefore be desirable to provide a methodology and related apparatus by which casing drilling could be carried out while the upper casing remains substantially in situ, but while also eliminating the potential for loose drill chips or shavings from dropping down into the lower casing section which supports the rotatable blade and/or bucket wheels of the turbine engine or compressor rotor.

BRIEF SUMMARY OF THE INVENTION
Accordingly, in one exemplary but nonlimiting embodiment, there is provided a method of drilling one or more holes, substantially in situ, in a turbomachine casing, comprising: locating piping including at least one vacuum head within the turbomachine casing in proximity to a hole to be drilled; drilling at least one hole in the turbomachine casing such that drill chips or shavings caused by the drilling are collected in the vacuum head; and applying a vacuum through the piping to the at least one vacuum head to thereby remove the drill chips or shavings collected in the vacuum head to a location outside the turbomachine casing.
In another exemplary but nonlimiting embodiment, the invention provides a method of drilling a plurality of holes, substantially in situ, in a turbomachine casing having separable upper and lower casing sections comprising: raising the upper casing section a predetermined distance above the lower casing section; for each of said pluarality of holes, installing piping including a vacuum head into the upper casing section, locating the vacuum head in proximity to the respective hole to be drilled, and so that the piping extends from each vacuum head to a location outside the upper casing section; drilling the plurality of holes in the upper casing section such that drill chips or shavings caused by the drilling are collected in the vacuum head associated with each respective hole; and applying a vacuum through the piping to each vacuum head to thereby remove the drill chips or shavings collected in each vacuum head to a location outside the upper casing section.
. 3

In still another exemplary but nonlimiting embodiment, the invention provides an apparatus for removing drilling chips or shavings from inside a turbomachine casing comprising: piping adapted for insertion into the turbomachine casing, the piping having a vacuxom head at one end and a connector adapted for connection to a vacuum source at an opposite end; and support hardware including a clamp for attaching the piping to the turbomachine casing such that the vacuum head is located below a hole to be drilled.
The invention will now be described in detail in connection with the drawings identified below,
BRIEF DESCRIPTION OF THE DRAWINGS
Fig. 1 is a simplified perspective view of upper and lower turbine casing sections, where the upper casing section is raised above the lower casing section for implementing a drilling process in accordance with an exemplary but nonlimiting embodiment described herein;
Fig. 2 is a partial section view of the upper casing section showing a plurality of holes drilled in the upper casing section for receiving a corresponding number of sensor elements;
Fig. 3 is a partial perspective view of the upper casing section, showing vacuum piping installed within the upper casing section;
Fig. 4 is another perspective view showing the vacuum piping from a different angle; and
4

Figs. 5 is still another partial perspective view showing the vacuijm piping installed within the upper casing section.
DETAILED DESCRIPTION OF THE INVENTION
With reference initially to Fig. 1, a compressor case 10 is shown to include an upper casing half section (or, simply, "upper casing section") 12 and a lower casing half section (or, simply, "lower casing section") 14. In the upper casing section 12, a row of stator blades 16 is visible, it being understood that several rows of stator blades, as well as the remaining blades of the rows of stator blades, are assembled within the upper casing section and that the rotor and its associated rows of blades are assembled within the lower casing section.
In the example embodiment, and with reference to Fig. 2, it may be required to drill plural holes 18 into the upper casing section 12 for installation of various ancillary components/features such as, for example, engine health monitoring sensors 20 or other instrumentation on a temporary or permanent basis. Fig. 2 shows one possible drilling pattern where holes 18 are to be drilled at three different axial locations, with, for example, two holes (only one shown) spaced circumferentially at each of the three axial locations. The holes 18 may vary in diameter from, for example, about ^ inch to an inch or more, depending on the components or sensors to be installed. In addition, the holes normally will be at least partially threaded as shown in Fig. 2.
In order to drill the holes 18 in the upper casing section 12 in accordance with the exemplary but nonlimiting embodiment, the upper casing section 12 is raised initially from the lower

casing section 14 by about 20-30 inches, e.g., 24 inches, as shown in Fig. 1, and supported in the raised position by jacks or other supports 22. This permits sufficient access to the interior of the upper casing section to allow the temporary installation of vacuum apparatus for removing chips/shavings generated during drilling.
Figs. 3-5 show in greater detail how piping may be inserted temporarily into the upper casing section 12 to facilitate removal of any drill chips/shavings from each hole location. Specifically, for each hole 18 to be drilled, a piping elbow or vacuum head 24 is fixed to an axially-extending vacuum tube 26 that terminates at a vacuum supply fitting or connector 28 where the vacuum is applied (either directly or via additional piping). Tubes 26 may vary in length to accommodate the different axial locations of the holes 18. The elbow or vacuum head 24 and tubes 2 6 may be of any suitable material such as metal, PVC or the like, and tubes 2 6 may have a diameter of, for example, 1 to 3 inches, but all dimensions are subject to change depending on specific applications.
The vacuum head 24 is located directly under and/or engaged with the sensor installation hole location on the casing section. At the opposite end of the piping where a vacuum supply fitting 28 is located, the piping is fixed to a respective support bar 30 that, in turn, is fixed to the upper casing end face 32 or a temporarily-installed attachment plate 34 that is in turn mounted on the casing end face 32. A flexible friction sleeve 36 fitted about the supply pipe 24 and pulls the piping tightly against conventional friction lock device 38 via handle 40.
6

In the event one of the holes 18 to be drilled lies adjacent a flanged edge or other obstruction in the casing such that it is not possible to have the vacuum head engaged with the casing section interior wall at the hole location, it is within the scope of the invention to utilize a funnel-shaped vacuum head as shown at 42 in Figs. 3-5 that may be spaced below the casing wall but is nevertheless effective to catch all metal chips and/or shavings created by the drilling process. The diameter of the funnel-shaped head 42 may vary as needed, and, preferably, the funnel-shaped head is aligned substantially with a center line of the hole to be drilled. It is, of course, contemplated that the funnel-shaped head 42 engage the casing surface where practical.
It will be appreciated that the piping hardware is not limited to the specific arrangement described above. For example, tubes 2 6 may be connected to one or more vacuum sources separately, or all of the tubes 2 6 may be joined to a single manifold (not shown) that is, in turn, connected to a single vacuum source. The number and location of the holes to be drilled will dictate the location and support points for the piping hardware. It will also be appreciated that the vacuum pressure applied may also vary as required to provide effective chip/shaving removal.
Upon completion of the drilling operation and removal of the sensor package components, the vacuum tubes/heads 26, 24 and any associated mounting hardware (e.g., support rods 30, plate 34) are removed, and the upper casing 12 lowered onto the lower casing 14 and re-secured in the usual manner. Whether the sensor package or other component is installed before or after the re-assembly of the upper and lower casing sections depends on specific applications.
7

While the invention has been described in connection with what is presently considered to be the most practical and preferred embodiment, it is to be understood that the invention is not to be limited to the disclosed embodiment, but on the contrary, is intended to cover various modifications and equivalent arrangements included within the spirit and scope of the appended claims.
9

We Claim:
1. A method of drilling one or more holes, substantially in situ, in a turbomachine casing 10, comprising:
(a) locating piping 26 including at least one vacuum head 24 within the turbomachine casing in proximity to a hole 18 to be drilled;
(b) drilling at least one hole 18 in the casing 10 such that drill chips or shavings caused by the drilling are collected in the vacuum head 24; and
(c) applying a vacuum through said piping 26 to said at least one vacuum head 24 to thereby remove the drill chips or shavings collected in said vacuum head 24 to a location outside the turbomachine casing.

2. The method of claim 1 wherein during step (a), said vacuum head 24 is engaged with an interior surface of said turbomachine casing 10 substantially directly under said at least one hole 18 to be drilled.
3. The method of claim 1 wherein during step (a), said vacuum head 24 is located below an interior surface of said turbomachine casing 10, in substantially direct alignment with a center line of said at least one hole 18 to be drilled.
4. The method of claim 3 wherein said vacuum head comprises a funnel-shaped component 42.
5. The method of claim 1 wherein said vacuum head 24 is connected to an axially-oriented section of said piping 26 that extends at least to an edge of said turbomachine casing, said
9

axially-oriented section supported at said edge of said turbomachine casing.
6. The method of claim 1 wherein said at least one hole 18 comprises multiple holes, and wherein said at least one vacuum head 24 comprises multiple vacuum heads located, respectively, in proximity to each of said multiple holes to be drilled.
7. The method of claim 6 wherein a vacuum is applied separately to each vacuum head 24,
8. A method of drilling a plurality of holes 18, substantially in situ, in a turbomachine casing 10 having separable upper and lower casing sections 12, 14 comprising:

(a) raising the upper casing section 12 a predetermined distance above the lower casing section 14;
(b) for each of said pluralityof holes 18, installing piping 26 including a vacuum head 24 into the upper casing section 12, locating the vacuum head 24 in proximity to the respective hole 18 to be drilled, and so that said piping extends from each said vacuum head to a location outside the upper casing section 12;
(c) drilling said plurality of holes 18 in the upper casing section 12 such that drill chips or shavings caused by the drilling are collected in the vacuum head 24 associated with each respective hole; and
(d) applying a vacuum through said piping 26 to each said vacuum head 24 to thereby remove the drill chips or shavings collected in each said vacuum head 24 to a location outside said upper casing section,
lo

9. The method of claim 8 wherein during step (b), each said
vacuum head 24 is engaged with an interior surface of said
upper casing section 12 substantially directly under a
respective one of said plurality of holes 18 to be drilled.
10. The method of claim 8 wherein during step (b), said vacuum head 24 is located below an interior surface of said upper casing section 12, in substantially direct alignment with a center line of said at least one hole to be drilled.
11. The method of claim 8 including securing said piping 26 to said upper casing section 12 to an edge 32 of said upper casing section 12 at a location remote from said vacuum head 24.
12. The method of claim 11 wherein securing said piping to said upper casing section 12 is achieved at least partially by using a sleeve clamp 36.
13. The method of claim 8 wherein, during step (a) the upper casing section 12 is raised between about 20-30 inches.
14. The method of claim 8 further comprising:

(e) removing the piping 26 and vacuum head 24 at each of said plurality of holes; and
(f) lowering the upper casing section 12 onto the lower casing section 14.
15. Apparatus for removing drilling chips or shavings from
inside a turbomachine casing 10 comprising:
piping 2 6 adapted for insertion into the turbomachine casing 10, the piping 2 6 having a vacuum head 24 at one end and a connector 28 adapted for connection to a vacuum source at an opposite end; and support hardware 30, 36 including a clamp 36
I!

for attaching the piping to the turbomachine casing such that the vaccuiti head is located below a hole to be drilled.
Dated this the 23rd Day of April, 2012 . H
MANISHA SINGH NAIR
Agent for the Applicant [IN/PA-740]
LEX ORBIS IP PRACTICE