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Joseph Leonard Moroso

from Greenville, SC
Age ~58
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Also known as:
Joseph L Moroso, Joe L Moroso, Leonard J Moroso, Joseph L Moroson, Joseph O
Phone and address:
4 Thistle Ln, Greenville, SC 29615
(864) 284-0282
Related to:
John D Hawkins, 71Karen Stevens, 78John Wiley, 55
Connected to:
Douglas J Morosoff, 64Mark W Moross, 59Sandra Morote, 62Lauren P Morotti, 36Helene P Morotto, 71Michael M Moroukian, 72Manuel J Moroun, 97Margaret J Moroun, 71Christina E Morovics, 44Donald L Morovits, 89

Joseph Moroso Phones & Addresses

  • 4 Thistle Ln, Greenville, SC 29615 (864) 284-0282
  • Hobe Sound, FL
  • Milton, FL
  • Longwood, FL
  • 4 W Thistle Ln, Greenville, SC 29615 (864) 809-0908

Work

Position: Production Occupations

Education

Degree: High school graduate or higher

Publications

Us Patents

Repaired Turbine Nozzle

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US Patent:
7484928, Feb 3, 2009
Filed:
Mar 21, 2007
Appl. No.:
11/723739
Inventors:
Brian Peter Arness - Simpsonville SC, US
Graham David Sherlock - Greenville SC, US
Joseph Leonard Moroso - Greenville SC, US
Stewart William Beitz - Greenville SC, US
Graydon Wayne Peters - Humble TX, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 9/02
US Classification:
415115
Abstract:
A trailing edge coupon for the trailing edge of a airfoil of a turbine nozzle segment is welded to an airfoil section of the nozzle segment having a damaged trailing edge portion removed. The coupon includes film cooling holes spaced one from the other along a pressure side wall portion of the coupon and a plurality of radially spaced openings along the trailing edge. By welding the pressure and suction side edges of the coupon to the pressure and side edges of the remaining portion of the airfoil, the operating life of the nozzle is extended.

System For Regulating A Cooling Fluid Within A Turbomachine

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US Patent:
7914253, Mar 29, 2011
Filed:
May 1, 2007
Appl. No.:
11/799162
Inventors:
Sivaraman Vedhagiri - Greer SC, US
Ravi Meenaksh - Greenville SC, US
Jesse Trout - Simpsonville SC, US
William Parker - Simpsonville SC, US
Eric Scicchitano - Montreal, CA
Joseph Moroso - Greenville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D 25/12
F01D 11/02
US Classification:
415115, 415230
Abstract:
A system for regulating a cooling fluid within a turbomachine. The system may include a plurality of bypass chambers, wherein each of the plurality of bypass chambers allows for the cooling fluid to pass from the compressor section to the at least one wheelspace area. The system may also include a plurality of bypass plugs, wherein each of the plurality of bypass plugs is insertable into a bypass chamber opening on each of the plurality of bypass chambers.

Method Of Replacing A Composite Airfoil

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US Patent:
8146250, Apr 3, 2012
Filed:
May 30, 2008
Appl. No.:
12/129930
Inventors:
Joseph L. Moroso - Greenville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
B23P 6/00
B29C 73/00
B29C 45/14
US Classification:
298891, 2988971, 2940201, 2940218, 264 361, 264139, 264279
Abstract:
A method of replacing a portion of a composite airfoil in a turbine. The method comprises the steps of providing a turbine with a plurality of composite airfoils mounted on a wheel. At least one of the composite airfoils has a core made of a non-plastic material and a plastic airfoil portion to envelope at least a portion of the core. A composite airfoil having an airfoil portion in need of replacement is accessed. The plastic airfoil portion is removed to expose the core while the core is mounted on the wheel. A plastic airfoil portion is molded to envelope the core while the core is mounted on the wheel.

Radial Retainer For Single Lobe Turbine Blade Attachment And Method For Radially Retaining A Turbine Blade In A Turbine Blade Slot

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US Patent:
20040067137, Apr 8, 2004
Filed:
Oct 2, 2002
Appl. No.:
10/065316
Inventors:
Joseph Moroso - Greenville SC, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
F01D005/32
US Classification:
416/221000
Abstract:
The invention provides for a simple and inexpensive fabrication to provide radial position retention to minimize the problems associated with single lobe attachment radial slop.

Turbine Airfoil Trailing Edge Repair And Methods Therefor

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US Patent:
20050235492, Oct 27, 2005
Filed:
Apr 22, 2004
Appl. No.:
10/829281
Inventors:
Brian Arness - Simpsonville SC, US
Graham Sherlock - Greenville SC, US
Joseph Moroso - Greenville SC, US
Stewart Beitz - Greenville SC, US
Graydon Peters - Humble TX, US
International Classification:
B63H001/16
F03B003/12
US Classification:
029889100, 029402080
Abstract:
A trailing edge coupon for the trailing edge of a airfoil of a turbine nozzle segment is welded to an airfoil section of the nozzle segment having a damaged trailing edge portion removed. The coupon includes film cooling holes spaced one from the other along a pressure side wall portion of the coupon and a plurality of radially spaced openings along the trailing edge. By welding the pressure and suction side edges of the coupon to the pressure and side edges of the remaining portion of the airfoil, the operating life of the nozzle is extended.

Tip Shroud Attachment For Stator Vane

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US Patent:
20070122274, May 31, 2007
Filed:
Nov 29, 2005
Appl. No.:
11/288400
Inventors:
C. Moorman - Simpsonville SC, US
Joseph Moroso - Greenville SC, US
William Miller - Simpsonville SC, US
Jennifer Michenfelder - Fountain Inn SC, US
Assignee:
General Electric Company - Schnectady NY
International Classification:
F04D 29/54
US Classification:
415209300
Abstract:
A stator vane segment and tip shroud segment assembly comprising: a plurality of vanes, each having an airfoil portion and a radially inner tip, each tip formed with at least one radially inwardly projecting tenon; and a tip shroud segment extending over the radially inner tips of the vanes, the tip shroud segment formed with a plurality of holes, each hole fitted with a bushing that receives a respective one of the tenons.

Method Of Repairing The Turbine Airfoil Nozzle Segment

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US Patent:
20070184182, Aug 9, 2007
Filed:
Mar 21, 2007
Appl. No.:
11/723742
Inventors:
Brian Arness - Simpsonville SC, US
Graham Sherlock - Greenville SC, US
Joseph Moroso - Greenville SC, US
Stewart Beitz - Greenville SC, US
Graydon Peters - Humble TX, US
Assignee:
General Electric Company - Schenectady NY
International Classification:
B05D 3/00
US Classification:
427140000
Abstract:
A trailing edge coupon for the trailing edge of a airfoil of a turbine nozzle segment is welded to an airfoil section of the nozzle segment having a damaged trailing edge portion removed. The coupon includes film cooling holes spaced one from the other along a pressure side wall portion of the coupon and a plurality of radially spaced openings along the trailing edge. By welding the pressure and suction side edges of the coupon to the pressure and side edges of the remaining portion of the airfoil, the operating life of the nozzle is extended.

Method For Making A Composite Airfoil

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US Patent:
20090077802, Mar 26, 2009
Filed:
Sep 20, 2007
Appl. No.:
11/858333
Inventors:
Joseph L. Moroso - Greenville SC, US
Thomas R. Tipton - Greer SC, US
International Classification:
B21D 53/78
B21K 3/04
US Classification:
2988971, 2642711, 264313
Abstract:
A method of manufacturing a composite airfoil includes the step of providing a core made of a metal or ceramic material. A plastic airfoil portion is molded to envelope at least a portion of the core.
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Joseph Leonard Moroso from Greenville, SC, age ~58 Get Report