Flow ingestion discourager with ridged pattern for a turbomachine shroud

Delvaux , et al. Dec

Patent Grant D871468

U.S. patent number D871,468 [Application Number D/598,691] was granted by the patent office on 2019-12-31 for flow ingestion discourager with ridged pattern for a turbomachine shroud. This patent grant is currently assigned to General Electric Company. The grantee listed for this patent is General Electric Company. Invention is credited to John McConnell Delvaux, Matthew Troy Hafner, Glenn Curtis Taxacher.


United States Patent D871,468
Delvaux ,   et al. December 31, 2019

Flow ingestion discourager with ridged pattern for a turbomachine shroud

Claims

CLAIM The ornamental design for a flow ingestion discourager with ridged pattern for a turbomachine shroud, as shown and described.
Inventors: Delvaux; John McConnell (Fountain Inn, SC), Hafner; Matthew Troy (Honea Path, SC), Taxacher; Glenn Curtis (Simpsonville, SC)
Applicant:
Name City State Country Type

General Electric Company

Schenectady

NY

US
Assignee: General Electric Company (Schenectady, NY)
Appl. No.: D/598,691
Filed: March 28, 2017

Current U.S. Class: D15/138
Current International Class: 1509
Field of Search: ;D15/7,122,123,126,138,139,199

References Cited [Referenced By]

U.S. Patent Documents
2812159 November 1957 Krebs
5618161 April 1997 Papageorgiou
5632598 May 1997 Maier
D586831 February 2009 Khanin
D611510 March 2010 Khanin
2002/0164247 November 2002 Nadeau
2007/0231131 October 2007 Aynes
2008/0072572 March 2008 Beutin
2008/0298970 December 2008 Ferber
2012/0121437 May 2012 Borufka
2012/0141253 June 2012 Weidmann
2012/0230818 September 2012 Shepherd
2013/0183135 July 2013 Fishler
2013/0243600 September 2013 Noble
2015/0017013 January 2015 Tozzi
2016/0024939 January 2016 Nilsson
2016/0025108 January 2016 Englebert
2016/0221881 August 2016 Delvaux
2016/0245103 August 2016 Gimat
2016/0273373 September 2016 Filipenco
2018/0371922 December 2018 Sitkiewicz
Primary Examiner: Palasik; Patricia A
Attorney, Agent or Firm: Wilson; Charlotte C. Pemrick; James W.

Description



FIG. 1 is a top and perspective view of a design for a flow ingestion discourager with a ridged pattern for a turbomachine shroud.

FIG. 2 is a top view of the design for the flow ingestion discourager with a ridged pattern of FIG. 1 for a turbomachine shroud.

FIG. 3 is a side, elevational view of the design for the flow ingestion discourager of FIG. 1 for a turbomachine shroud, illustrating the ridged pattern being located towards the forward end of the shroud. The forward end is the left side of the shroud in FIG. 3.

FIG. 4 is a side, elevational view of the design for the flow ingestion discourager of FIG. 1 for a turbomachine shroud, illustrating the ridged pattern being located towards the forward end of the shroud. The forward end is the right side of the shroud in FIG. 4.

FIG. 5 is a front view of the design for the flow ingestion discourager with ridged pattern of FIG. 1 for a turbomachine shroud, illustrating a front edge of the ridged pattern on the shroud.

FIG. 6 is a rear view of the design for the flow ingestion discourager with ridged pattern of FIG. 1 for a turbomachine shroud, illustrating a rear or aft edge of the ridged pattern on the shroud.

FIG. 7 is a top and perspective view of the design for the flow ingestion discourager with a ridged pattern of FIG. 1 for a turbomachine shroud, showing the position of the flow ingestion discourager relative to an inspection hole located in the forward end of the shroud.

FIG. 8 is a top view of the design for the flow ingestion discourager with a ridged pattern of FIG. 1 for a turbomachine shroud, showing the position of the flow ingestion discourager relative to an inspection hole located in the forward end of the shroud; and,

FIG. 9 is a front view of the design for a flow ingestion discourager with a ridged pattern of FIG. 1 for a turbomachine shroud, showing the position of the flow ingestion discourager relative to an inspection hole located in the forward end of the shroud.

The broken lines in the drawings represent portions of the flow ingestion discourager with ridged pattern for a turbomachine shroud which form no part of the claimed design.

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Patent Diagrams and Documents

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