Manifold for washing gas turbine aircraft engines

Description

FIG. 1 is a rear and side perspective view of a manifold for washing gas turbine aircraft engines, showing my new design;

FIG. 2 is a front elevational view thereof;

FIG. 3 is a side elevational view thereof from the left of FIG. 2;

FIG. 4 is a side elevational view thereof from the right of FIG. 2;

FIG. 5 is a rear elevational view thereof;

FIG. 6 is a top plan view thereof; and,

FIG. 7 is a bottom plan view thereof.

Claims

CLAIM The ornamental design for a manifold for washing gas turbine aircraft engines, as shown.

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Inventors:	Asplund; Peter (Hasselby, SE)
Assignee:	Gas Turbine Efficiency AB (Jarfalla, SE)
Appl. No.:	D/232,193
Filed:	June 16, 2005

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Foreign Application Priority Data

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Jan 26, 2005 [EM]			000286729-0001

Current U.S. Class:	D32/4
Current International Class:	1505
Field of Search:	;D32/1,15,25,35 ;239/550,565,566,722,754

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References Cited [Referenced By]

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U.S. Patent Documents

D243610	March 1977	Craig
D244532	May 1977	Poston
D321574	November 1991	Shevers et al.
5289642	March 1994	Sloan
D394921	June 1998	Cherinchak
6079640	June 2000	Merritts
2006/0243828	November 2006	Angelone

Primary Examiner: Zarfas; Louis S.
Assistant Examiner: Sims; Kathleen M.
Attorney, Agent or Firm: Young & Thompson