USD777014S1 - Integrated stiffener - Google Patents

Integrated stiffener Download PDF

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Publication number
USD777014S1
USD777014S1 US29/499,210 US201429499210F USD777014S US D777014 S1 USD777014 S1 US D777014S1 US 201429499210 F US201429499210 F US 201429499210F US D777014 S USD777014 S US D777014S
Authority
US
United States
Prior art keywords
integrated stiffener
stiffener
integrated
view
elevational view
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.)
Active
Application number
US29/499,210
Inventor
Michael Joseph Wolfer
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.)
Servi-Sure LLC
Original Assignee
Servi-Sure LLC
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 Servi-Sure LLC filed Critical Servi-Sure LLC
Priority to US29/499,210 priority Critical patent/USD777014S1/en
Assigned to Servi-Sure, LLC reassignment Servi-Sure, LLC ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: WOLFER, MICHAEL JOSEPH
Priority to JPD2015-2729F priority patent/JP1548482S/ja
Application granted granted Critical
Publication of USD777014S1 publication Critical patent/USD777014S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

FIG. 1 is a front perspective view of the integrated stiffener of the present design;
FIG. 2 is a front elevational view thereof, the rear elevational view being a mirror image thereof;
FIG. 3 is a right side elevational view thereof, the left side elevational view being a mirror image thereof;
FIG. 4 is a top plan view thereof; and,
FIG. 5 is a bottom plan view thereof.
Broken lines are used to illustrate features of the integrated stiffener which form no part of the claimed design.

Claims (1)

    CLAIM
  1. The ornamental design for an integrated stiffener, as shown and described.
US29/499,210 2014-08-12 2014-08-12 Integrated stiffener Active USD777014S1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US29/499,210 USD777014S1 (en) 2014-08-12 2014-08-12 Integrated stiffener
JPD2015-2729F JP1548482S (en) 2014-08-12 2015-02-12

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/499,210 USD777014S1 (en) 2014-08-12 2014-08-12 Integrated stiffener

Publications (1)

Publication Number Publication Date
USD777014S1 true USD777014S1 (en) 2017-01-24

Family

ID=55761968

Family Applications (1)

Application Number Title Priority Date Filing Date
US29/499,210 Active USD777014S1 (en) 2014-08-12 2014-08-12 Integrated stiffener

Country Status (2)

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US (1) USD777014S1 (en)
JP (1) JP1548482S (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD1002338S1 (en) * 2021-12-09 2023-10-24 Ameristar Perimeter Security Usa Inc. Fencing bracket

Citations (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3118545A (en) * 1962-12-17 1964-01-21 Ernest B Rosner Anodizing rack structure
US3290238A (en) * 1962-03-16 1966-12-06 Reynolds Metals Co Anodizing rack construction
US3366567A (en) * 1965-06-28 1968-01-30 Harry D. Elbaum Electroplating rack
US4828202A (en) * 1979-09-27 1989-05-09 The Boeing Company Method and apparatus for wideband vibration damping of reinforced skin structures
US6170157B1 (en) * 1996-03-22 2001-01-09 The Boeing Company Determinant spar assembly
US6371821B1 (en) * 1996-01-11 2002-04-16 Nature's Wing Fin Designs, Llc High efficiency hydrofoil and swim fin designs
US6508909B1 (en) * 2000-03-07 2003-01-21 Construcciones Aeronauticas S.A. Process for manufacturing pre-cured parts of composite material with green-applied stiffeners
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US20080142461A1 (en) * 2006-12-15 2008-06-19 Shenzhen Futaihong Precision Industry Co.,Ltd. Rack apparatus with retaining member for use in anodizing
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US8353479B2 (en) * 2007-11-13 2013-01-15 Airbus Operations Gmbh Arrangement of two fuselage sections of an aircraft and a connecting structure for connecting fuselage skins
US8480030B2 (en) * 2007-09-18 2013-07-09 Airbus Operations Gmbh Structural component and method for stiffening an external skin
US8899522B2 (en) * 2011-03-30 2014-12-02 Airbus Operations, S.L. Aircraft fuselage with high strength frames
US20150034763A1 (en) * 2013-08-01 2015-02-05 Airbus Operations (S.A.S.) Aircraft fuselage frame element integrating tabs for the fastening of stiffeners
US20150321742A1 (en) * 2012-12-21 2015-11-12 Airbus Operations (Sas) Stiffener for an aircraft fuselage, method for manufacturing same, and aircraft fuselage equipped with such a stiffener
US9199417B1 (en) * 2013-01-02 2015-12-01 The Boeing Company Systems and methods for assembling stiffened composite structures
USD752944S1 (en) * 2014-08-12 2016-04-05 Servi-Sure, LLC Aerospace handle with wing stiffener
US20160244185A1 (en) * 2015-02-23 2016-08-25 The Boeing Company Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners

Patent Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3290238A (en) * 1962-03-16 1966-12-06 Reynolds Metals Co Anodizing rack construction
US3118545A (en) * 1962-12-17 1964-01-21 Ernest B Rosner Anodizing rack structure
US3366567A (en) * 1965-06-28 1968-01-30 Harry D. Elbaum Electroplating rack
US4828202A (en) * 1979-09-27 1989-05-09 The Boeing Company Method and apparatus for wideband vibration damping of reinforced skin structures
US6371821B1 (en) * 1996-01-11 2002-04-16 Nature's Wing Fin Designs, Llc High efficiency hydrofoil and swim fin designs
US6170157B1 (en) * 1996-03-22 2001-01-09 The Boeing Company Determinant spar assembly
US6766984B1 (en) * 1998-07-16 2004-07-27 Icom Engineering Corporation Stiffeners for aircraft structural panels
US6508909B1 (en) * 2000-03-07 2003-01-21 Construcciones Aeronauticas S.A. Process for manufacturing pre-cured parts of composite material with green-applied stiffeners
US7527222B2 (en) * 2004-04-06 2009-05-05 The Boeing Company Composite barrel sections for aircraft fuselages and other structures, and methods and systems for manufacturing such barrel sections
US7134629B2 (en) * 2004-04-06 2006-11-14 The Boeing Company Structural panels for use in aircraft fuselages and other structures
US7325771B2 (en) * 2004-09-23 2008-02-05 The Boeing Company Splice joints for composite aircraft fuselages and other structures
US20080142461A1 (en) * 2006-12-15 2008-06-19 Shenzhen Futaihong Precision Industry Co.,Ltd. Rack apparatus with retaining member for use in anodizing
US7798340B2 (en) * 2006-12-15 2010-09-21 Shenzhen Futaihong Precision Industry Co., Ltd. Rack apparatus with retaining member for use in anodizing
US8480030B2 (en) * 2007-09-18 2013-07-09 Airbus Operations Gmbh Structural component and method for stiffening an external skin
US8353479B2 (en) * 2007-11-13 2013-01-15 Airbus Operations Gmbh Arrangement of two fuselage sections of an aircraft and a connecting structure for connecting fuselage skins
US8899522B2 (en) * 2011-03-30 2014-12-02 Airbus Operations, S.L. Aircraft fuselage with high strength frames
US20150321742A1 (en) * 2012-12-21 2015-11-12 Airbus Operations (Sas) Stiffener for an aircraft fuselage, method for manufacturing same, and aircraft fuselage equipped with such a stiffener
US9199417B1 (en) * 2013-01-02 2015-12-01 The Boeing Company Systems and methods for assembling stiffened composite structures
US20150034763A1 (en) * 2013-08-01 2015-02-05 Airbus Operations (S.A.S.) Aircraft fuselage frame element integrating tabs for the fastening of stiffeners
USD752944S1 (en) * 2014-08-12 2016-04-05 Servi-Sure, LLC Aerospace handle with wing stiffener
US20160244185A1 (en) * 2015-02-23 2016-08-25 The Boeing Company Method, System and Apparatus for Assembling a Composite Wing Skin with Stiffeners

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD1002338S1 (en) * 2021-12-09 2023-10-24 Ameristar Perimeter Security Usa Inc. Fencing bracket

Also Published As

Publication number Publication date
JP1548482S (en) 2016-04-25

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