Patent
   D871468
Priority
Mar 28 2017
Filed
Mar 28 2017
Issued
Dec 31 2019
Expiry
Dec 31 2034
Assg.orig
Entity
unknown
3
21
n/a
The ornamental design for a flow ingestion discourager with ridged pattern for a turbomachine shroud, as shown and described.

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.

Delvaux, John McConnell, Taxacher, Glenn Curtis, Hafner, Matthew Troy

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Executed onAssignorAssigneeConveyanceFrameReelDoc
Mar 28 2017General Electric Company(assignment on the face of the patent)
Mar 28 2017DELVAUX, JOHN MCCONNELLGeneral Electric CompanyASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0417650329 pdf
Mar 28 2017HAFNER, MATTHEW TROYGeneral Electric CompanyASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0417650329 pdf
Mar 28 2017TAXACHER, GLENN CURTISGeneral Electric CompanyASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0417650329 pdf
Nov 10 2023General Electric CompanyGE INFRASTRUCTURE TECHNOLOGY LLCASSIGNMENT OF ASSIGNORS INTEREST SEE DOCUMENT FOR DETAILS 0657270001 pdf
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