GB2177989A - Aircraft fuselage tails - Google Patents

Aircraft fuselage tails Download PDF

Info

Publication number
GB2177989A
GB2177989A GB08618031A GB8618031A GB2177989A GB 2177989 A GB2177989 A GB 2177989A GB 08618031 A GB08618031 A GB 08618031A GB 8618031 A GB8618031 A GB 8618031A GB 2177989 A GB2177989 A GB 2177989A
Authority
GB
United Kingdom
Prior art keywords
ofthe
cross
tail
aircrafttail
radius
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.)
Withdrawn
Application number
GB08618031A
Other languages
English (en)
Other versions
GB8618031D0 (en
Inventor
Prof Dr Ernst Heinric 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 GB8618031D0 publication Critical patent/GB8618031D0/en
Publication of GB2177989A publication Critical patent/GB2177989A/en
Withdrawn legal-status Critical Current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 And Supports For Tunnels (AREA)
  • Underground Or Underwater Handling Of Building Materials (AREA)
  • Main Body Construction Of Washing Machines And Laundry Dryers (AREA)
  • Toys (AREA)
  • Casting Or Compression Moulding Of Plastics Or The Like (AREA)
  • Lining Or Joining Of Plastics Or The Like (AREA)
GB08618031A 1985-07-24 1986-07-23 Aircraft fuselage tails Withdrawn GB2177989A (en)

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
GB8618031D0 GB8618031D0 (en) 1986-08-28
GB2177989A true GB2177989A (en) 1987-02-04

Family

ID=6276637

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08618031A Withdrawn GB2177989A (en) 1985-07-24 1986-07-23 Aircraft fuselage tails

Country Status (5)

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

Cited By (3)

* 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
US4953812A (en) * 1987-11-13 1990-09-04 The Boeing Company Aircraft configuration with aft mounted engines and method
US4976396A (en) * 1987-11-13 1990-12-11 The Boeing Company Aircraft configuration with aft mounted engines

Families Citing this family (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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
WO2022191838A1 (en) * 2021-03-10 2022-09-15 Zsm Holdings Llc Aircraft fuselage configurations for upward deflection of aft 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

Cited By (3)

* 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
US4953812A (en) * 1987-11-13 1990-09-04 The Boeing Company Aircraft configuration with aft mounted engines and method
US4976396A (en) * 1987-11-13 1990-12-11 The Boeing Company Aircraft configuration with aft mounted engines

Also Published As

Publication number Publication date
FR2585326A1 (fr) 1987-01-30
US4712751A (en) 1987-12-15
DE3526472C2 (https=) 1987-05-07
DE3526472A1 (de) 1987-02-05
GB8618031D0 (en) 1986-08-28
JPS6226200A (ja) 1987-02-04
FR2585326B3 (fr) 1987-10-16

Similar Documents

Publication Publication Date Title
GB2177989A (en) Aircraft fuselage tails
EP0525912B1 (en) Wing/winglet configurations and methods for aircraft
EP0122790B1 (en) Aircraft wing and winglet arrangement
US20050173592A1 (en) Lifting foil
GB2076109A (en) Improving aircraft stability
KR20140048256A (ko) 윙의 윙팁 장치 및 이러한 윙팁 장치를 갖는 윙
EP3366572A1 (en) Protective finish for wing tip devices
US20200407039A1 (en) Wing-to-body trailing edge fairing and method of fabricating same
EP3626609B1 (en) A wing tip device
Hefner et al. An overview of concepts for aircraft drag reductions
CN210681131U (zh) 一种机翼结构
WO1995017334A1 (en) Aircraft wing/nacelle combination
CN110386243B (zh) 一种高升阻比的低速无人机翼型
US11447239B2 (en) Aircraft wing and wing tip device
Smith Three-dimensional viscous and inviscid separation of a vortex sheet from a smooth non-slender body
US4377267A (en) Vortex tranquilizer
CN105000159A (zh) U型风帆结构
Lee Jr et al. Installation effects of long-duct pylon-mounted nacelles on a twin-jet transport model with swept supercritical wing
Liu et al. Flow patterns and aerodynamic characteristics of a wing-strake configuration
Maskew A quadrilateral vortex method applied to configurations with high circulation
GB2171361A (en) Separation plate for hydrofoil keel for sailing vessels
CN219018376U (zh) 一种线束分支防护护套
CN102167154A (zh) 飞机翼尖装置
Lawford Low-speed wind-tunnel tests on an unswept wing-fuselage model of aspect ratio 9.8, with tangential blowing over trailing-edge flaps and ailerons, including the effect of slipstream
CN102167153A (zh) 后缘对齐的飞机翼尖装置

Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)