The present invention relates generally to manufacturing processes, and, more specifically, to shot peening of workpieces.
Metal components or parts are typically manufactured in multiple steps to achieve the final size, configuration, and surface finish thereof. Metal components may be cast in complex three dimensional (3D) configurations, with and without subsequent precision machining of various surfaces thereof.
A gas turbine engine includes many complex 3D parts cast and machined for use in various components thereof. Turbine rotor blades include an airfoil extending outwardly from a supporting platform and dovetail. The dovetail is configured with axial lobes or tangs for mounting each blade in corresponding dovetail slots in the perimeter of a supporting rotor disk.
During operation, energy is extracted from hot combustion gases that flow past the turbine rotor blades which in turn rotate the supporting rotor disk for powering a compressor in a typical configuration. The blades are subject to centrifugal loads during operation, which loads are carried radially inwardly through the supporting dovetails into the perimeter of the rotor disk.
The turbine blades are typically formed of high strength superalloy material having enhanced strength at the elevated temperatures typically found in the turbine. To further enhance the strength of the turbine rotor blades the various surfaces of the dovetails may be shot peened in one of the last manufacturing steps producing the blades.
Shot peening is a mature process in which metal shot is discharged in stream of pressurized air over the surface of a metal workpiece to plastically deform the surface layer thereof and introduce residual compressive stress therein. The residual compressive stress reduces the stresses experienced in the component during operation, such as in the rotating environment of the gas turbine engine.
Since the shot peening process is effected at the end of the manufacturing cycle for the typical component, corresponding care must be used in the process to avoid damaging the component or incompletely shot peening the intended surface thereof. Uniform shot peening of the entire turbine blade dovetail, for example, will ensure maximum strength of the blade during operation and a correspondingly long service life.
However, shot peening adds to the time and cost of manufacture of components, such as the turbine blades, and in the typical gas turbine engine a multitude of turbine blades are found and must be suitably manufactured at competitive cost.
In one conventional shot peening apparatus enjoying many years of successful commercial service in the United States, individual turbine blades are mounted upside down in corresponding supporting cans which expose upwardly the corresponding dovetail while protecting the turbine airfoil inside the can.
Eight blades in corresponding cans may be mounted to the perimeter of a supporting turntable inside a fully enclosed cabinet for performing shot peening of the blade dovetails. Each can is indexed into position next to a gang or set of shot peening nozzles mounted from a common support rod. The individual nozzles in the set are manually aligned with a single dovetail for aiming the shot stream at a common target point thereon.
During operation, the cabinet is closed, and the support rod for the nozzles oscillates vertically for discharging the shot stream simultaneously from the set of nozzles over the surface area of the blade dovetail as it rotates with the can on the common turntable.
In less than a minute per blade, the entire dovetail may be suitably shot peened over its full exposed surface notwithstanding the serpentine configuration of the serrations or dovetail lobes thereon. The use of accurately aligned multiple shotpeen nozzles ensures accurate shot peening of the dovetail as it rotates during the process while the nozzles oscillate vertically.
However, each of the multiple nozzles requires corresponding initial alignment relative to the corresponding blade workpiece supported in the can, which alignment is typically done manually by an operator and therefore extends the setup time of the process.
Furthermore, two sets of shotpeen nozzles may be mounted inside the cabinet from corresponding supporting rods for permitting the simultaneous shot peening of two blade dovetails in their corresponding supporting cans.
Each of these multiple shotpeen nozzles must be independently aligned with the corresponding workpiece. And, each of the nozzles in each set must also be aligned relative to each other for ensuring the coincidence of the separate shot streams therefrom at a common target point on the workpiece.
The blade workpieces are typically shot peened in large batches following the initial alignment of the nozzles in the cabinet. The blades are simply inserted into the corresponding supporting cans for shot peening thereof and replaced by subsequent turbine blades until the full batch of blades has been shot peened. Prior to the next batch of blades requiring shot peening, the alignment of the shotpeen nozzles is measured in a conventional manner using Almen strips, with the multiple nozzles being realigned if required.
Accordingly, it is desired to provide an improved shotpeen nozzle in a multi-nozzle apparatus for shot peening workpieces with improved alignment of the nozzles.
A shotpeen nozzle includes a tubular core mounted in a casing. The casing has an inlet for receiving shot in a stream of pressurized air, and the core includes an outlet for discharging the stream. A laser is mounted to the casing for projecting a laser beam in parallel with the core at its outlet in the direction of discharge of the stream therefrom.
The invention, in accordance with preferred and exemplary embodiments, together with further objects and advantages thereof, is more particularly described in the following detailed description taken in conjunction with the accompanying drawings in which:
Illustrated schematically in
The dovetail 18 is conventional and is configured as an axial-entry dovetail with a plurality of serrations or dovetail lobes configured for mounting the blade to the perimeter of a supporting rotor disk (not shown) having corresponding axial dovetail slots extending through the perimeter thereof.
The shot peening apparatus 10 includes a suitable housing or cabinet 20 in which is mounted a rotary turntable 22. Mounted around the circumference of the turntable are a plurality of rotary cans 24, such as eight, in which corresponding ones of the workpiece blades 12 are suitably mounted upside down to expose the corresponding dovetails 18 while hiding and protecting the airfoils 14 therein. Each can includes a suitable rubber boot specifically configured for mounting the 3D airfoil and protecting it from abrasion during the shot peening operation.
The turntable 22 is mounted in the cabinet for rotation about its centerline axis for indexing corresponding ones of the cans 24 and the blades 12 supported therein in turn for undergoing shot peening. The individual cans 24 are suitably mounted on the turntable for powered rotation about their centerline axes during the shot peening process.
A plurality of shotpeen nozzles 26 are mounted by corresponding adjustable brackets 28 to a common support rod 30 inside the cabinet 20. The support rod 30 is in turn suspended from a suitable carriage 32 configured for oscillating the rod and nozzles attached thereto in vertical translation inside the cabinet during operation.
But for the nozzles 26, the shotpeen apparatus illustrated in
This apparatus includes high strength, rubber supply hoses 34 joined to respective ones of the improved nozzles 26, instead of conventional nozzles originally provided with the machine, for delivering a stream 36 of small metal shot 38 in pressurized air 40 for shot peening of the blade dovetails 18. The shot 38 is initially contained in a suitable hopper 42 and is delivered by gravity into the pressurized airstream commonly provided by shop air contained in a storage tank or accumulator.
The exemplary nozzle 26 illustrated in
The casing 46 has an inlet 48 at a proximal end thereof for receiving or mounting the supply hose 34 in flow communication with the corresponding end of the core 44. The casing inlet 48 is in the form of a counterbore or socket in which the distal end of the hose 34 may be inserted and fixedly joined thereto using suitable set screws for example.
The core 44 has an outlet 50 at an opposite distal end of the casing for discharging the shot stream 36 received from the hose 34 during shotpeen operation.
Each shotpeen nozzle 26 further includes a suitable laser 52 mounted to the casing 46 for projecting a visible laser beam 54 in parallel with the core 44 at the outlet 50 thereof in the same direction of discharge of the stream 36 from the outlet 50. The laser may have any conventional configuration such as a small battery operated red laser, with a simple push button on-off switch.
As further described hereinbelow, the laser 52 significantly improves the accuracy and speed of initial alignment of the individual nozzles 26 inside the cabinet illustrated in
The metal casing 46 illustrated in
In the preferred embodiment illustrated in
This preferred alignment of the laser 52 may be effected by providing a bowed core 44 that includes a shallow bow or bend 60 disposed at an intermediate longitudinal position between the inlet 48 and outlet 50. A small access hole 62 extends through the bend of the core and is coaxially aligned with the center bore 58 thereof.
The laser 52 is mounted in the casing 46 behind the bend 60 and is coaxially aligned with the access hole 62 and bore 58 for projecting the laser beam 54 coaxially therethrough and out the center of the core outlet 50 during the alignment process. In this configuration, the laser 52 is hidden inside the casing pocket 56 behind the discharge end of the nozzle which further protects the laser from ricochet damage from the shot during the peening operation.
Since the shot being carried through the supply hose 44 is abrasive, the carbide core 44 is preferably straight on opposite ends or sides of the middle bend 60 therein, with a large obtuse bend angle A between the two straight ends of the core and casing. The bend angle A may be about 150 degrees for example and should be as large as practical for introducing a shallow bend in the nozzle sufficient for mounting the laser to project the laser beam coaxially through the discharge end of the core.
The bend 60 between the two straight ends of the carbide core 44 has a smooth internal surface which promotes the smooth turning of the shot stream between the inlet and outlet ends of the core during shot peening operation.
The diameter of the access hole 62 may be as small as practical and corresponds generally with the diameter of the laser beam 54 itself, which in turn is a very small minor portion of the diameter of the center bore 58 of the core through which the shot stream is discharged during peening operation. Since the access hole 62 is disposed on the upstream side of the bend 60 and faces downstream in alignment with the discharge end of the core, the shot being carried by the core during operation travels away from the access hole 62 to prevent obstruction or clogging thereof during operation.
A method of using the shotpeen nozzle 26 illustrated in
The brackets 28 are adjustable with articulated joints and fasteners or screws as desired and are manually adjustable by the operator for aligning each nozzle 26 to aim the laser beam 54 at a suitable target 64 on the workpiece supported in the can 24. In this way, each nozzle may be suitably aligned using the laser beam 54 as the guide to determine the impact point of the shot which is subsequently discharged through the nozzles toward the workpiece.
The laser is then turned off upon completion of the alignment process. Shot peening operation may then be commenced by discharging the stream 36 of shot 38 in the pressurized air 40 through the corresponding hoses 34 and nozzles 26 for shot peening the specific workpiece 12 within the aim of one or more of the nozzles.
As indicated above, a plurality of the nozzles 26, such as the three illustrated in
All three lasers 52 are then turned on during the alignment process to project corresponding laser beams 54 from the corresponding outlets of the three nozzles toward the common workpiece 12.
Since the dovetail 18 undergoing the shot peening process has serpentine lobes or serrations which vary in facing direction, the three nozzles 26 are spaced apart vertically from each other and in different planes and angular orientations as desired to reach the workpiece from different angles of attack. The three laser beams 54 projecting out from each of the three nozzles readily permits the individual alignment of each nozzle 26 as required so that the three beams are aligned to the common target 64 on the workpiece 12 from the different attack angles of the three nozzles.
Once the three nozzles are accurately aligned to the common target 64, and the corresponding brackets 28 locked in position on the common support rod 30, all three lasers 52 of the three nozzles may then be turned off. The shot peening process may then commence by discharging respective streams 36 of the shot 38 in the pressurized air 40 from each of the nozzles simultaneously toward the target on the workpiece for shot peening thereof.
The cans 24 and workpieces 12 supported therein are rotated during the shot peening process, while the support rod 30 oscillates vertically to shot peen the entire external surface of the blade dovetail 18 in the same manner provided in the conventional apparatus disclosed above.
However, the improved laser-guided shotpeen nozzles 26 substantially decrease the initial alignment time for the three nozzles. And, following shot peening of a batch of the workpieces, the conventional Almen strips may be used to check alignment of the three nozzles, or the shot peening apparatus may be temporarily shut off to examine alignment of the nozzles by turning on the lasers for checking in-situ alignment with the workpiece.
Notwithstanding the hostile environment inside the shot peening cabinet illustrated in
While there have been described herein what are considered to be preferred and exemplary embodiments of the present invention, other modifications of the invention shall be apparent to those skilled in the art from the teachings herein, and it is, therefore, desired to be secured in the appended claims all such modifications as fall within the true spirit and scope of the invention.
Number | Name | Date | Kind |
---|---|---|---|
3937055 | Caruso et al. | Feb 1976 | A |
4152754 | DeFilippis et al. | May 1979 | A |
4401477 | Clauer et al. | Aug 1983 | A |
4420957 | Weber | Dec 1983 | A |
4432220 | Loersch et al. | Feb 1984 | A |
D282771 | Garrison | Feb 1986 | S |
4604881 | Lienert | Aug 1986 | A |
4724299 | Hammeke | Feb 1988 | A |
4937421 | Ortiz et al. | Jun 1990 | A |
5212976 | Company | May 1993 | A |
5306360 | Bharti et al. | Apr 1994 | A |
5671628 | Halila et al. | Sep 1997 | A |
5948293 | Somers et al. | Sep 1999 | A |
5993681 | Glogovsky | Nov 1999 | A |
6075593 | Trantow et al. | Jun 2000 | A |
6374158 | Fusaro | Apr 2002 | B1 |
6483076 | O'Loughlin et al. | Nov 2002 | B1 |
6490899 | Berthelet et al. | Dec 2002 | B1 |
6715701 | Julien | Apr 2004 | B1 |
6759626 | Clauer et al. | Jul 2004 | B1 |
Number | Date | Country | |
---|---|---|---|
20060101883 A1 | May 2006 | US |