FR2585326B3 - Configuration d'arriere de fuselage d'avion - Google Patents

Configuration d'arriere de fuselage d'avion

Info

Publication number
FR2585326B3
FR2585326B3 FR8610711A FR8610711A FR2585326B3 FR 2585326 B3 FR2585326 B3 FR 2585326B3 FR 8610711 A FR8610711 A FR 8610711A FR 8610711 A FR8610711 A FR 8610711A FR 2585326 B3 FR2585326 B3 FR 2585326B3
Authority
FR
France
Prior art keywords
aircraft fuselage
rear configuration
fuselage rear
configuration
aircraft
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
Application number
FR8610711A
Other languages
English (en)
French (fr)
Other versions
FR2585326A1 (fr
Inventor
Ernst Heinrich Hirschel
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 Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Messerschmitt Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2585326A1 publication Critical patent/FR2585326A1/fr
Application granted granted Critical
Publication of FR2585326B3 publication Critical patent/FR2585326B3/fr
Expired legal-status Critical Current

Links

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
    • 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)
  • Mechanical Engineering (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Toys (AREA)
  • Main Body Construction Of Washing Machines And Laundry Dryers (AREA)
  • Lining And Supports For Tunnels (AREA)
  • Underground Or Underwater Handling Of Building Materials (AREA)
FR8610711A 1985-07-24 1986-07-23 Configuration d'arriere de fuselage d'avion Expired FR2585326B3 (fr)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19853526472 DE3526472A1 (de) 1985-07-24 1985-07-24 Rumpfheckmodifikation von flugzeugen

Publications (2)

Publication Number Publication Date
FR2585326A1 FR2585326A1 (fr) 1987-01-30
FR2585326B3 true FR2585326B3 (fr) 1987-10-16

Family

ID=6276637

Family Applications (1)

Application Number Title Priority Date Filing Date
FR8610711A Expired FR2585326B3 (fr) 1985-07-24 1986-07-23 Configuration d'arriere de fuselage d'avion

Country Status (5)

Country Link
US (1) US4712751A (enExample)
JP (1) JPS6226200A (enExample)
DE (1) DE3526472A1 (enExample)
FR (1) FR2585326B3 (enExample)
GB (1) GB2177989A (enExample)

Families Citing this family (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
USD308663S (en) 1987-05-06 1990-06-19 The Boeing Company Airplane
US4976396A (en) * 1987-11-13 1990-12-11 The Boeing Company Aircraft configuration with aft mounted engines
US4953812A (en) * 1987-11-13 1990-09-04 The Boeing Company Aircraft configuration with aft mounted engines and method
DE4404810C2 (de) * 1994-02-16 1999-12-09 Daimler Chrysler Aerospace Rumpfheck für ein Verkehrsflugzeug
US5692704A (en) * 1995-06-07 1997-12-02 Buttgereit; Volker Body tail unit for a commercial aircraft
US5677508A (en) * 1995-08-15 1997-10-14 Hughes Missile Systems Company Missile having non-cylindrical propulsion section
US5908175A (en) * 1997-11-19 1999-06-01 Magnes; Gene One-piece airplane tail-cone with inspection door(s)
DE102010045588B4 (de) * 2010-09-16 2017-04-06 Airbus Operations Gmbh Rumpfsegment für ein Luftfahrzeug
ES2709346T3 (es) 2015-03-06 2019-04-16 Airbus Operations Gmbh Mamparo de presión trasero extendido
EP4304929A4 (en) * 2021-03-10 2025-03-05 ZSM Holdings LLC AIRCRAFT FUSELAGE CONFIGURATIONS FOR UPWARD BEND OF A REAR FUSELAGE

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE674433C (de) * 1937-05-08 1939-04-14 Messerschmitt Boelkow Blohm An Luftfahrzeugen angeordnete, aus Wellblech bestehende Aussenbeplankung
FR1114301A (fr) * 1954-04-05 1956-04-11 Procédé économique de construction cellulaire
US3023860A (en) * 1957-03-18 1962-03-06 Floyd P Ellzey Body construction
US3955781A (en) * 1974-03-10 1976-05-11 Andrei Nikolaevich Tupolev Supersonic aircraft with the engines disposed under the delta wing middle portion

Also Published As

Publication number Publication date
US4712751A (en) 1987-12-15
DE3526472A1 (de) 1987-02-05
JPS6226200A (ja) 1987-02-04
FR2585326A1 (fr) 1987-01-30
DE3526472C2 (enExample) 1987-05-07
GB8618031D0 (en) 1986-08-28
GB2177989A (en) 1987-02-04

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