USD371732S - Attachment tool for a system for repairing damaged gas turbine engine airfoils - Google Patents

Attachment tool for a system for repairing damaged gas turbine engine airfoils Download PDF

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Publication number
USD371732S
USD371732S US29/032,386 US3238694F USD371732S US D371732 S USD371732 S US D371732S US 3238694 F US3238694 F US 3238694F US D371732 S USD371732 S US D371732S
Authority
US
United States
Prior art keywords
gas turbine
turbine engine
attachment tool
repairing damaged
damaged gas
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
US29/032,386
Inventor
James L. Owens
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Raytheon Technologies Corp
Original Assignee
United Technologies Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by United Technologies Corp filed Critical United Technologies Corp
Priority to US29/032,386 priority Critical patent/USD371732S/en
Assigned to UNITED TECHNOLOGIES CORPORATION reassignment UNITED TECHNOLOGIES CORPORATION ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: OWENS, JAMES L.
Application granted granted Critical
Publication of USD371732S publication Critical patent/USD371732S/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

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Description

FIG. 1 is a front view of an attachment tool for a system for repairing damaged gas turbine engine airfoils showing my new design;
FIG. 2 is a left side view thereof;
FIG. 3 is a right side view thereof; and,
FIG. 4 is a top view thereof.
The broken line showing the abradable end piece is not part of the claimed design.

Claims (1)

  1. The ornamental design for an attachment tool for a system for repairing damaged gas turbine engine airfoils, as shown and described.
US29/032,386 1994-10-27 1994-10-27 Attachment tool for a system for repairing damaged gas turbine engine airfoils Expired - Lifetime USD371732S (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US29/032,386 USD371732S (en) 1994-10-27 1994-10-27 Attachment tool for a system for repairing damaged gas turbine engine airfoils

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/032,386 USD371732S (en) 1994-10-27 1994-10-27 Attachment tool for a system for repairing damaged gas turbine engine airfoils

Publications (1)

Publication Number Publication Date
USD371732S true USD371732S (en) 1996-07-16

Family

ID=71069269

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/032,386 Expired - Lifetime USD371732S (en) 1994-10-27 1994-10-27 Attachment tool for a system for repairing damaged gas turbine engine airfoils

Country Status (1)

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US (1) USD371732S (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120323254A1 (en) * 2011-06-20 2012-12-20 Medtronic, Inc. Medical assemblies and methods for implementation of multiple medical leads through a single entry

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
Ventrol™ Levin Tube gastric sump, National Catheter Corp. Catalog, no date available, p. 16.

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US20120323254A1 (en) * 2011-06-20 2012-12-20 Medtronic, Inc. Medical assemblies and methods for implementation of multiple medical leads through a single entry
US10758262B2 (en) * 2011-06-20 2020-09-01 Medtronic, Inc. Medical assemblies and methods for implantation of multiple medical leads through a single entry

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