JPS6226200A - 飛行機の変形された胴尾部 - Google Patents

飛行機の変形された胴尾部

Info

Publication number
JPS6226200A
JPS6226200A JP61172924A JP17292486A JPS6226200A JP S6226200 A JPS6226200 A JP S6226200A JP 61172924 A JP61172924 A JP 61172924A JP 17292486 A JP17292486 A JP 17292486A JP S6226200 A JPS6226200 A JP S6226200A
Authority
JP
Japan
Prior art keywords
tail
section
fuselage
cross
airplane
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.)
Pending
Application number
JP61172924A
Other languages
English (en)
Japanese (ja)
Inventor
エルンスト・ハインリツヒ・ヒルシエル
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 JPS6226200A publication Critical patent/JPS6226200A/ja
Pending 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)
JP61172924A 1985-07-24 1986-07-24 飛行機の変形された胴尾部 Pending JPS6226200A (ja)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE19853526472 DE3526472A1 (de) 1985-07-24 1985-07-24 Rumpfheckmodifikation von flugzeugen
DE3526472.1 1985-07-24

Publications (1)

Publication Number Publication Date
JPS6226200A true JPS6226200A (ja) 1987-02-04

Family

ID=6276637

Family Applications (1)

Application Number Title Priority Date Filing Date
JP61172924A Pending JPS6226200A (ja) 1985-07-24 1986-07-24 飛行機の変形された胴尾部

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
FR2585326A1 (fr) 1987-01-30
DE3526472C2 (enExample) 1987-05-07
FR2585326B3 (fr) 1987-10-16
GB8618031D0 (en) 1986-08-28
GB2177989A (en) 1987-02-04

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