ATE529332T1 - Flügel-rumpf-verkleidung für ein flugzeug - Google Patents

Flügel-rumpf-verkleidung für ein flugzeug

Info

Publication number
ATE529332T1
ATE529332T1 AT07380076T AT07380076T ATE529332T1 AT E529332 T1 ATE529332 T1 AT E529332T1 AT 07380076 T AT07380076 T AT 07380076T AT 07380076 T AT07380076 T AT 07380076T AT E529332 T1 ATE529332 T1 AT E529332T1
Authority
AT
Austria
Prior art keywords
wing
section
fairing
separate
aircraft
Prior art date
Application number
AT07380076T
Other languages
English (en)
Inventor
Del Lago Mario Jimenez
Serrano Julian Perez
Original Assignee
Airbus Operations Sl
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 Sl filed Critical Airbus Operations Sl
Application granted granted Critical
Publication of ATE529332T1 publication Critical patent/ATE529332T1/de

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • 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
    • B64C1/26—Attaching the wing or tail units or stabilising surfaces
    • 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
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Laminated Bodies (AREA)
  • Tires In General (AREA)
  • Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
  • Toys (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
AT07380076T 2006-10-31 2007-03-20 Flügel-rumpf-verkleidung für ein flugzeug ATE529332T1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES200602769A ES2317762B1 (es) 2006-10-31 2006-10-31 Carena ventral para un avion.

Publications (1)

Publication Number Publication Date
ATE529332T1 true ATE529332T1 (de) 2011-11-15

Family

ID=38969345

Family Applications (1)

Application Number Title Priority Date Filing Date
AT07380076T ATE529332T1 (de) 2006-10-31 2007-03-20 Flügel-rumpf-verkleidung für ein flugzeug

Country Status (5)

Country Link
US (1) US8128029B2 (de)
EP (1) EP1918194B1 (de)
AT (1) ATE529332T1 (de)
EA (1) EA011937B1 (de)
ES (1) ES2317762B1 (de)

Families Citing this family (20)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102008016104A1 (de) * 2008-03-28 2009-10-08 Airbus Deutschland Gmbh Durchbrandsicherer Flugzeugrumpf
FR2936489B1 (fr) * 2008-09-30 2012-07-20 Airbus France Troncon central d'aeronef avec carenage ventral travaillant
FR2995589B1 (fr) * 2012-09-19 2015-07-31 Liebherr Aerospace Toulouse Sas Panneau de carrosserie pour vehicule de transport comprenant un dispositif d'echange thermique et vehicule de transport comprenant un tel panneau de carrosserie
FR2999149B1 (fr) * 2012-12-10 2015-01-16 Airbus Operations Sas Fuselage pour aeronef comportant un dispositif de liaison configure pour etre relie a un caisson de voilure de l'aeronef et pour transmettre a ce caisson des efforts subis par le fuselage
FR3000020B1 (fr) * 2012-12-26 2015-01-30 Airbus Operations Sas Avion a fuselage pourvu d'excroissances laterales delimitant des espaces de stockage
ES2578427T3 (es) 2012-12-27 2016-07-26 Airbus Operations S.L. Una carena ventral de una aeronave con una capacidad de almacenamiento mejorada
CN103612746B (zh) * 2013-10-24 2016-09-21 中国商用飞机有限责任公司 翼吊布局飞机中吊挂的整流罩结构
US10486796B2 (en) * 2016-09-26 2019-11-26 General Electric Company Aircraft having an AFT engine and stabilizer with a varying line of maximum thickness
US10364021B2 (en) * 2016-09-26 2019-07-30 General Electric Company Aircraft having an aft engine and stabilizer root fillet
EP3619109B1 (de) * 2017-05-01 2022-01-05 Bombardier Inc. Flugzeugflügeleinheit mit durch oberflügelhaut definiertem druckboden
US10773787B2 (en) 2017-06-14 2020-09-15 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US10766598B2 (en) * 2017-06-14 2020-09-08 The Boeing Company Wing-to-fuselage joints and aircraft including the same
US20190185134A1 (en) * 2017-12-19 2019-06-20 Thomas Hsueh Adjustable Fuselage Location Joint Method
FR3077801B1 (fr) * 2018-02-14 2022-04-22 Dassault Aviat Portion d'aeronef a trainee d'onde reduite
WO2019178064A1 (en) * 2018-03-12 2019-09-19 Aero Design Labs, Inc. Wing-to-body trailing edge fairing and method of fabricating same
RU2701899C1 (ru) * 2018-11-29 2019-10-02 Федеральное государственное унитарное предприятие "Центральный аэрогидродинамический институт имени профессора Н.Е. Жуковского" (ФГУП "ЦАГИ") Фюзеляж летательного аппарата
CA3084642A1 (en) * 2019-06-24 2020-12-24 Bombardier Inc. Wing to fuse junction shaping, and associated systems and methods
US20220410246A1 (en) * 2021-06-25 2022-12-29 Ultracell Llc Fuselage heat exchanger for cooling power source for unmanned aerial vehicles (uavs)
CN114620200B (zh) * 2022-03-25 2023-10-24 中国舰船研究设计中心 一种基于catia的水面船舶型线精光顺方法
FR3140347A1 (fr) * 2022-09-29 2024-04-05 Dassault Aviation Portion d'aéronef à trainée réduite

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB366345A (en) * 1930-04-07 1932-02-04 Johann Anton Sanders Improvements in and connected with aeroplanes
US3942746A (en) * 1971-12-27 1976-03-09 General Dynamics Corporation Aircraft having improved performance with beaver-tail afterbody configuration
DE4313592C2 (de) * 1993-04-26 2000-02-17 Daimler Chrysler Aerospace Großraumflugzeug
US5803405A (en) * 1995-06-07 1998-09-08 Northrop Grumman Corporation Expandable aircraft section
US6068215A (en) * 1995-12-21 2000-05-30 Mcdonnall Douglas Expandable aircraft cargo bay and method
US5779189A (en) * 1996-03-19 1998-07-14 Lockheed Martin Corporation System and method for diverting boundary layer air
US6176196B1 (en) * 1996-10-03 2001-01-23 Harold P. Halter Boat bottom hull design
FR2827028B1 (fr) * 2001-07-06 2003-09-26 Airbus France Aeronef a carenage ventral et joint pour un tel aeronef
EP1300335B1 (de) * 2001-10-05 2005-03-02 Airbus France Flugzeug mit Flügel-Rumpf-Verkleidungsdichtung
FR2836963A1 (fr) * 2002-03-08 2003-09-12 Airbus France Dispositif de fixation d'un element sur une structure d'aeronef
CN100488839C (zh) * 2003-05-05 2009-05-20 敏捷思有限责任公司 具有产生升力的机身的飞行器
US7093798B2 (en) * 2004-01-30 2006-08-22 The Boeing Company Transformable airplane
US7097136B2 (en) * 2004-04-13 2006-08-29 Lockheed Martin Corporation Immersible unmanned air vehicle and system for launch, recovery, and re-launch at sea
FR2869872B1 (fr) * 2004-05-04 2007-07-20 Airbus France Sas Cale de transition entre un moyen de fixation d'une aile sur un fuselage d'un aeronef et ladite aile, et aeronef comportant une telle cale.
FR2871436B1 (fr) * 2004-06-11 2007-09-07 Airbus France Sas Aeronef muni d'un carenage ventral, et carenage ventral.

Also Published As

Publication number Publication date
EA011937B1 (ru) 2009-06-30
ES2317762B1 (es) 2010-02-10
EP1918194A3 (de) 2010-07-07
EA200700565A1 (ru) 2008-06-30
US20080099610A1 (en) 2008-05-01
ES2317762A1 (es) 2009-04-16
EP1918194A2 (de) 2008-05-07
EP1918194B1 (de) 2011-10-19
US8128029B2 (en) 2012-03-06

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