USD723447S1 - Fuselage - Google Patents

Fuselage Download PDF

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Publication number
USD723447S1
USD723447S1 US29/387,647 US201129387647F USD723447S US D723447 S1 USD723447 S1 US D723447S1 US 201129387647 F US201129387647 F US 201129387647F US D723447 S USD723447 S US D723447S
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US
United States
Prior art keywords
fuselage
view
design
elevation view
radii
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
US29/387,647
Inventor
Jan Lesemann
Michael Meyer
Bernd Trahmer
Ralph Sturm
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.)
Airbus Operations GmbH
Original Assignee
Airbus Operations GmbH
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 Airbus Operations GmbH filed Critical Airbus Operations GmbH
Assigned to AIRBUS OPERATIONS GMBH reassignment AIRBUS OPERATIONS GMBH ASSIGNMENT OF ASSIGNORS INTEREST (SEE DOCUMENT FOR DETAILS). Assignors: LESEMANN, JAN, MEYER, MICHAEL, TRAHMER, BERND, STURM, RALPH
Application granted granted Critical
Publication of USD723447S1 publication Critical patent/USD723447S1/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

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Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/06—Frames; Stringers; Longerons ; Fuselage sections
    • B64C1/068—Fuselage sections
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Body Structure For Vehicles (AREA)
  • Moulding By Coating Moulds (AREA)

Description

FIG. 1 is a perspective view of the fuselage, in accordance with the present invention;
FIG. 2 is a top plan view of the fuselage shown in FIG. 1;
FIG. 3 is a bottom plan view of the fuselage shown in FIG. 1;
FIG. 4 is a right side elevation view of the fuselage shown in FIG. 1, the left side being a mirror image thereof;
FIG. 5 is a front elevation view of the fuselage shown in FIG. 1; and,
FIG. 6 is a representational elevation view of FIG. 5, shown solely for the purpose of illustrating that the fuselage is composed of four degrees of radii in six segments. The angled partial broken lines indicate the point at which one radius meets another radius. These broken lines form no part of the claimed design. The broken line circle shown intersecting the fuselage is shown solely to emphasize the six radii segments, and forms no part of the claimed design.
The jagged circumferential lines wrapping around the middle portion of the fuselage in FIGS. 1-4 indicate that the appearance of any portion of the article between the break lines forms no part of the claimed design. The windows and floor of this embodiment are shown in broken line and as such form no part of the claimed invention.

Claims (1)

    CLAIM
  1. The ornamental design for a fuselage, as shown and described.
US29/387,647 2010-09-16 2011-03-16 Fuselage Active USD723447S1 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102010045588 2010-09-16
DE102010045588.1A DE102010045588B4 (en) 2010-09-16 2010-09-16 Fuselage segment for an aircraft

Publications (1)

Publication Number Publication Date
USD723447S1 true USD723447S1 (en) 2015-03-03

Family

ID=45768851

Family Applications (2)

Application Number Title Priority Date Filing Date
US29/387,647 Active USD723447S1 (en) 2010-09-16 2011-03-16 Fuselage
US13/233,336 Active 2032-05-10 US8757545B2 (en) 2010-09-16 2011-09-15 Segment of a fuselage of an aircraft

Family Applications After (1)

Application Number Title Priority Date Filing Date
US13/233,336 Active 2032-05-10 US8757545B2 (en) 2010-09-16 2011-09-15 Segment of a fuselage of an aircraft

Country Status (2)

Country Link
US (2) USD723447S1 (en)
DE (1) DE102010045588B4 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2983826B1 (en) * 2011-12-12 2013-12-20 Airbus Operations Sas FRONT STRUCTURE IMPROVED WITH COMPARTMENT FOR LANDING TRAIN.
CN213008694U (en) * 2019-08-01 2021-04-20 尼克研究与工程有限公司 Light conveyor body
US11453473B2 (en) 2019-08-09 2022-09-27 Luc VAN BAVEL Aircraft fuselage
DE102019132823A1 (en) * 2019-11-28 2021-06-02 Telair International Gmbh Airplane for freight and passenger transport, freight container and method for loading an airplane

Citations (21)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB560580A (en) 1942-11-13 1944-04-11 Laurence Rachard Morphew Improvements in or relating to the construction of streamlined panel structures
US3955781A (en) 1974-03-10 1976-05-11 Andrei Nikolaevich Tupolev Supersonic aircraft with the engines disposed under the delta wing middle portion
US4712751A (en) 1985-07-24 1987-12-15 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Tail end structure for an aircraft fuselage
US5806797A (en) * 1992-10-13 1998-09-15 The Boeing Company Airplane fuselage
US20040031881A1 (en) 2000-10-13 2004-02-19 Jamgarov Stephan Grigoryevich Aircraft provided with carrying fuselage
US6834833B2 (en) 2001-10-02 2004-12-28 The Boeing Company Twin aisle small airplane
WO2007120201A1 (en) 2005-11-15 2007-10-25 The Boeing Company Weight optimized pressurizable aircraft fuselage structures having near elliptical cross sections
US20080093503A1 (en) 2004-11-15 2008-04-24 Bruno Cacciaguerra Structural frame for an aircraft fuselage
GB2443542A (en) 2006-11-02 2008-05-07 Boeing Co Fuselage structure
US7410352B2 (en) * 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation
US20080209712A1 (en) * 2006-08-04 2008-09-04 Bruno Bisiach Device and method for working work pieces, such as aircraft's fuselage parts
US20090152399A1 (en) * 2006-05-31 2009-06-18 Airbus Deutschland Gmbh Line system arrangement in an aircraft or spacecraft having a fuselage
US20100084510A1 (en) * 2006-09-29 2010-04-08 Airbus Aircraft comprising a fuselage with a floor extending in the longitudinal plane of the fuselage
US7721992B2 (en) * 2007-03-07 2010-05-25 The Boeing Company Aircraft floor to fuselage attachment
US7787979B2 (en) * 2007-03-14 2010-08-31 The Boeing Company Splicing fuselage sections without shims
US7861970B2 (en) * 2006-11-02 2011-01-04 The Boeing Company Fuselage structure including an integrated fuselage stanchion
US20110001006A1 (en) * 2009-07-02 2011-01-06 Airbus Operations Process for making an aircraft having a floor
US7896291B2 (en) * 2006-04-10 2011-03-01 Airbus Deutschland Gmbh Aircraft door with oversizing
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
US8146860B2 (en) * 2006-04-10 2012-04-03 Airbus Operations Gmbh Aircraft fuselage with circular-arc-shaped exterior contour
US8215582B2 (en) * 2006-03-29 2012-07-10 Airbus Operations Limited Aircraft fuselage interior

Patent Citations (24)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB560580A (en) 1942-11-13 1944-04-11 Laurence Rachard Morphew Improvements in or relating to the construction of streamlined panel structures
US3955781A (en) 1974-03-10 1976-05-11 Andrei Nikolaevich Tupolev Supersonic aircraft with the engines disposed under the delta wing middle portion
US4712751A (en) 1985-07-24 1987-12-15 Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung Tail end structure for an aircraft fuselage
US5806797A (en) * 1992-10-13 1998-09-15 The Boeing Company Airplane fuselage
US20040031881A1 (en) 2000-10-13 2004-02-19 Jamgarov Stephan Grigoryevich Aircraft provided with carrying fuselage
US6834833B2 (en) 2001-10-02 2004-12-28 The Boeing Company Twin aisle small airplane
US7874516B2 (en) 2004-11-15 2011-01-25 Airbus France Structural frame for an aircraft fuselage
US20080093503A1 (en) 2004-11-15 2008-04-24 Bruno Cacciaguerra Structural frame for an aircraft fuselage
US7410352B2 (en) * 2005-04-13 2008-08-12 The Boeing Company Multi-ring system for fuselage barrel formation
WO2007120201A1 (en) 2005-11-15 2007-10-25 The Boeing Company Weight optimized pressurizable aircraft fuselage structures having near elliptical cross sections
US8215582B2 (en) * 2006-03-29 2012-07-10 Airbus Operations Limited Aircraft fuselage interior
US8146860B2 (en) * 2006-04-10 2012-04-03 Airbus Operations Gmbh Aircraft fuselage with circular-arc-shaped exterior contour
US7896291B2 (en) * 2006-04-10 2011-03-01 Airbus Deutschland Gmbh Aircraft door with oversizing
US20090152399A1 (en) * 2006-05-31 2009-06-18 Airbus Deutschland Gmbh Line system arrangement in an aircraft or spacecraft having a fuselage
US20080209712A1 (en) * 2006-08-04 2008-09-04 Bruno Bisiach Device and method for working work pieces, such as aircraft's fuselage parts
US20100084510A1 (en) * 2006-09-29 2010-04-08 Airbus Aircraft comprising a fuselage with a floor extending in the longitudinal plane of the fuselage
US7735779B2 (en) * 2006-11-02 2010-06-15 The Boeing Company Optimized fuselage structure
US7861970B2 (en) * 2006-11-02 2011-01-04 The Boeing Company Fuselage structure including an integrated fuselage stanchion
US20080105785A1 (en) 2006-11-02 2008-05-08 Griess Kenneth H Optimized fuselage structure
GB2443542A (en) 2006-11-02 2008-05-07 Boeing Co Fuselage structure
US7721992B2 (en) * 2007-03-07 2010-05-25 The Boeing Company Aircraft floor to fuselage attachment
US7787979B2 (en) * 2007-03-14 2010-08-31 The Boeing Company Splicing fuselage sections without shims
US7967250B2 (en) * 2008-05-12 2011-06-28 EMBRAER—Empresa Brasileira de Aeronáutica Hybrid aircraft fuselage structural components and methods of making same
US20110001006A1 (en) * 2009-07-02 2011-01-06 Airbus Operations Process for making an aircraft having a floor

Non-Patent Citations (2)

* Cited by examiner, † Cited by third party
Title
Drawings from the notice of invention with cross-section depictions of the fuselages of Airbus 320, Boeing 737 and Boeing 767 airplanes, 1 page.
U.S. Appl. No. 13/233,336, filed Sep. 15, 2011.

Also Published As

Publication number Publication date
US20120068014A1 (en) 2012-03-22
DE102010045588B4 (en) 2017-04-06
US8757545B2 (en) 2014-06-24
DE102010045588A1 (en) 2012-03-22

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