USD930549S1 - Aircraft winglet - Google Patents

Aircraft winglet Download PDF

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Publication number
USD930549S1
USD930549S1 US29/718,857 US201929718857F USD930549S US D930549 S1 USD930549 S1 US D930549S1 US 201929718857 F US201929718857 F US 201929718857F US D930549 S USD930549 S US D930549S
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US
United States
Prior art keywords
view
aircraft winglet
aircraft
winglet
perspective
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.)
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Application number
US29/718,857
Inventor
Pascal Bochud
David LeBlond
François Pepin
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.)
Bombardier Inc
Original Assignee
Bombardier Inc
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 Bombardier Inc filed Critical Bombardier Inc
Priority to US29/718,857 priority Critical patent/USD930549S1/en
Assigned to BOMBARDIER INC. reassignment BOMBARDIER INC. ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: BOCHUD, PASCAL, LEBLOND, DAVID, PEPIN, FRANCOIS
Priority to US29/803,359 priority patent/USD1013609S1/en
Application granted granted Critical
Publication of USD930549S1 publication Critical patent/USD930549S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Description

FIG. 1 is a perspective view of an aircraft illustrating an aircraft winglet according to a first embodiment of our new design in use;
FIG. 2 is a perspective view of the aircraft winglet according to the first embodiment;
FIG. 3 is a front view thereof;
FIG. 4 is a rear view thereof;
FIG. 5 is a top view thereof;
FIG. 6 is a bottom view thereof;
FIG. 7 is a right side view thereof;
FIG. 8 is a left side view thereof;
FIG. 9 is a perspective view of an aircraft illustrating an aircraft winglet according to a second embodiment of our new design in use;
FIG. 10 is a perspective view of the aircraft winglet according to the second embodiment;
FIG. 11 is a front view thereof;
FIG. 12 is a rear view thereof;
FIG. 13 is a top view thereof;
FIG. 14 is a bottom view thereof;
FIG. 15 is a right side view thereof;
FIG. 16 is a left side view thereof;
FIG. 17 is a perspective view of an aircraft illustrating an aircraft winglet according to a third embodiment of our new design in use;
FIG. 18 is a perspective view of the aircraft winglet according to the third embodiment;
FIG. 19 is a front view thereof;
FIG. 20 is a rear view thereof;
FIG. 21 is a top view thereof;
FIG. 22 is a bottom view thereof;
FIG. 23 is a right side view thereof; and,
FIG. 24 is a left side view thereof.
The broken lines illustrate environmental structure and form no part of the claimed design.

Claims (1)

    CLAIM
  1. We claim the ornamental design for an aircraft winglet, as shown and described.
US29/718,857 2019-12-30 2019-12-30 Aircraft winglet Active USD930549S1 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
US29/718,857 USD930549S1 (en) 2019-12-30 2019-12-30 Aircraft winglet
US29/803,359 USD1013609S1 (en) 2019-12-30 2021-08-12 Aircraft winglet

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US29/718,857 USD930549S1 (en) 2019-12-30 2019-12-30 Aircraft winglet

Related Child Applications (1)

Application Number Title Priority Date Filing Date
US29/803,359 Division USD1013609S1 (en) 2019-12-30 2021-08-12 Aircraft winglet

Publications (1)

Publication Number Publication Date
USD930549S1 true USD930549S1 (en) 2021-09-14

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ID=77636049

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US29/718,857 Active USD930549S1 (en) 2019-12-30 2019-12-30 Aircraft winglet
US29/803,359 Active USD1013609S1 (en) 2019-12-30 2021-08-12 Aircraft winglet

Family Applications After (1)

Application Number Title Priority Date Filing Date
US29/803,359 Active USD1013609S1 (en) 2019-12-30 2021-08-12 Aircraft winglet

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US (2) USD930549S1 (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD978057S1 (en) * 2020-12-23 2023-02-14 Bombardier Inc. Aircraft winglet
USD1013609S1 (en) * 2019-12-30 2024-02-06 Bombardier Inc. Aircraft winglet

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* Cited by examiner, † Cited by third party
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US4674709A (en) 1983-06-20 1987-06-23 Welles Stanley W Airframe design
US4722499A (en) * 1982-11-18 1988-02-02 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Auxiliary wing tips for an aircraft
US5275358A (en) * 1991-08-02 1994-01-04 The Boeing Company Wing/winglet configurations and methods for aircraft
US20090039204A1 (en) * 2007-08-09 2009-02-12 The Boeing Company Wingtip Feathers, Including Forward Swept Feathers, and Associated Aircraft Systems and Methods
US20090084904A1 (en) 2007-10-02 2009-04-02 The Boeing Company Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods
US20110024573A1 (en) * 2009-05-06 2011-02-03 Quiet Wing Technologies, Inc. Extended winglet with load balancing characteristics
US7988099B2 (en) * 2001-06-21 2011-08-02 Airbus Operations Limited Winglet
WO2012007358A1 (en) 2010-07-14 2012-01-19 Airbus Operations Limited Wing tip device
US20120312928A1 (en) * 2011-06-09 2012-12-13 Gratzer Louis B Split Blended Winglet
US8366056B2 (en) * 2007-06-21 2013-02-05 Airbus Operations Limited Winglet
US20130139421A1 (en) * 2011-12-05 2013-06-06 Airbus Operations Limited Wingtip fin of an aircraft
US20130256460A1 (en) * 2012-03-30 2013-10-03 The Boeing Company Performance-enhancing winglet system and method
US20150041597A1 (en) * 2011-07-14 2015-02-12 Airbus Operations Gmbh Wingtip device of a wing, and also a wing with such a wingtip device
US20150203190A1 (en) * 2013-04-19 2015-07-23 The Boeing Company Winglet attach fitting and method for attaching a split winglet to a wing
US20160009379A1 (en) * 2013-12-05 2016-01-14 The Boeing Company One-Piece Composite Bifurcated Winglet
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
US9908612B2 (en) * 2011-10-01 2018-03-06 The Boeing Company Fold wing tip having stub spar
US9988142B2 (en) 2014-09-16 2018-06-05 Airbus Operations Gmbh Wing for an aircraft, and an aircraft comprising such a wing
US10287002B2 (en) * 2013-12-05 2019-05-14 Tamarack Aerospace Group, Inc. Wingtip device
US10336440B2 (en) * 2014-01-20 2019-07-02 Airbus Operations Limited Curved winglet
US10501170B2 (en) * 2014-04-04 2019-12-10 Airbus Operations Limited Aircraft wing with a wing tip device and a strut
US10538307B2 (en) * 2011-10-01 2020-01-21 The Boeing Company Hinged raked wing tip
US10625847B2 (en) * 2017-04-21 2020-04-21 Textron Innovations Inc. Split winglet
WO2020146399A1 (en) 2019-01-07 2020-07-16 Aviation Partners, Inc. High-performance winglet

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5348253A (en) * 1993-02-01 1994-09-20 Gratzer Louis B Blended winglet
GB0420601D0 (en) * 2004-09-16 2004-10-20 Qinetiq Ltd Wing tip devices
DE102006055090A1 (en) * 2006-11-21 2008-05-29 Airbus Deutschland Gmbh Wing i.e. airfoil wing, end form for wing of commercial aircraft, has transition area arranged between wing and winglet, where local V-form changes continuously from wing to winglet in transition area
FR2948628B1 (en) * 2009-08-03 2012-02-03 Airbus Operations Sas AIRPLANE WITH LACET CONTROL BY DIFFERENTIAL TRAINING
CN102762453B (en) * 2009-12-10 2015-03-25 约翰内斯堡威特沃特斯兰德大学 Method for reducing in flight wake vortices and aircraft wingtip arrangement
GB201018185D0 (en) * 2010-10-28 2010-12-08 Airbus Operations Ltd Wing tip device attachment apparatus and method
EP2855275B1 (en) * 2012-05-31 2020-07-29 Bombardier Inc. Lighting array for an aircraft
USD732657S1 (en) * 2014-02-27 2015-06-23 Delta T Corporation Winglet
US9637225B1 (en) * 2015-11-16 2017-05-02 Textron Innovations Inc. Aircraft winglet
USD930549S1 (en) * 2019-12-30 2021-09-14 Bombardier Inc. Aircraft winglet
US20210197961A1 (en) * 2019-12-30 2021-07-01 Bombardier Inc. Winglet systems for aircraft
USD978057S1 (en) * 2020-12-23 2023-02-14 Bombardier Inc. Aircraft winglet

Patent Citations (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4722499A (en) * 1982-11-18 1988-02-02 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Auxiliary wing tips for an aircraft
US4674709A (en) 1983-06-20 1987-06-23 Welles Stanley W Airframe design
US5275358A (en) * 1991-08-02 1994-01-04 The Boeing Company Wing/winglet configurations and methods for aircraft
US7988099B2 (en) * 2001-06-21 2011-08-02 Airbus Operations Limited Winglet
US8366056B2 (en) * 2007-06-21 2013-02-05 Airbus Operations Limited Winglet
US20090039204A1 (en) * 2007-08-09 2009-02-12 The Boeing Company Wingtip Feathers, Including Forward Swept Feathers, and Associated Aircraft Systems and Methods
US7900876B2 (en) 2007-08-09 2011-03-08 The Boeing Company Wingtip feathers, including forward swept feathers, and associated aircraft systems and methods
US20090084904A1 (en) 2007-10-02 2009-04-02 The Boeing Company Wingtip Feathers, Including Paired, Fixed Feathers, and Associated Systems and Methods
US9302766B2 (en) * 2008-06-20 2016-04-05 Aviation Partners, Inc. Split blended winglet
US20110024573A1 (en) * 2009-05-06 2011-02-03 Quiet Wing Technologies, Inc. Extended winglet with load balancing characteristics
WO2012007358A1 (en) 2010-07-14 2012-01-19 Airbus Operations Limited Wing tip device
US20130092797A1 (en) * 2010-07-14 2013-04-18 Airbus Operations Gmbh Wing tip device
US20120312928A1 (en) * 2011-06-09 2012-12-13 Gratzer Louis B Split Blended Winglet
US8944386B2 (en) 2011-06-09 2015-02-03 Aviation Partners, Inc. Split blended winglet
US20150041597A1 (en) * 2011-07-14 2015-02-12 Airbus Operations Gmbh Wingtip device of a wing, and also a wing with such a wingtip device
US10538307B2 (en) * 2011-10-01 2020-01-21 The Boeing Company Hinged raked wing tip
US9908612B2 (en) * 2011-10-01 2018-03-06 The Boeing Company Fold wing tip having stub spar
US20130139421A1 (en) * 2011-12-05 2013-06-06 Airbus Operations Limited Wingtip fin of an aircraft
US8936219B2 (en) 2012-03-30 2015-01-20 The Boeing Company Performance-enhancing winglet system and method
US20130256460A1 (en) * 2012-03-30 2013-10-03 The Boeing Company Performance-enhancing winglet system and method
US20150203190A1 (en) * 2013-04-19 2015-07-23 The Boeing Company Winglet attach fitting and method for attaching a split winglet to a wing
US20160009379A1 (en) * 2013-12-05 2016-01-14 The Boeing Company One-Piece Composite Bifurcated Winglet
US10287002B2 (en) * 2013-12-05 2019-05-14 Tamarack Aerospace Group, Inc. Wingtip device
US10336440B2 (en) * 2014-01-20 2019-07-02 Airbus Operations Limited Curved winglet
US10501170B2 (en) * 2014-04-04 2019-12-10 Airbus Operations Limited Aircraft wing with a wing tip device and a strut
US9988142B2 (en) 2014-09-16 2018-06-05 Airbus Operations Gmbh Wing for an aircraft, and an aircraft comprising such a wing
US10625847B2 (en) * 2017-04-21 2020-04-21 Textron Innovations Inc. Split winglet
WO2020146399A1 (en) 2019-01-07 2020-07-16 Aviation Partners, Inc. High-performance winglet

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD1013609S1 (en) * 2019-12-30 2024-02-06 Bombardier Inc. Aircraft winglet
USD978057S1 (en) * 2020-12-23 2023-02-14 Bombardier Inc. Aircraft winglet

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