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GB8321281D0 - Underwing engine installation - Google Patents

Underwing engine installation

Info

Publication number
GB8321281D0
GB8321281D0 GB838321281A GB8321281A GB8321281D0 GB 8321281 D0 GB8321281 D0 GB 8321281D0 GB 838321281 A GB838321281 A GB 838321281A GB 8321281 A GB8321281 A GB 8321281A GB 8321281 D0 GB8321281 D0 GB 8321281D0
Authority
GB
United Kingdom
Prior art keywords
engine installation
underwing
underwing engine
installation
engine
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
GB838321281A
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.)
BAE Systems PLC
Original Assignee
British Aerospace PLC
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 British Aerospace PLC filed Critical British Aerospace PLC
Priority to GB838321281A priority Critical patent/GB8321281D0/en
Publication of GB8321281D0 publication Critical patent/GB8321281D0/en
Priority to GB08419904A priority patent/GB2144688B/en
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C7/00—Structures or fairings not otherwise provided for
    • B64C7/02—Nacelles
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/10—Influencing air flow over aircraft surfaces by affecting boundary layer flow using other surface properties, e.g. roughness
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/06—Influencing air flow over aircraft surfaces, not otherwise provided for by generating vortices
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D27/00—Arrangement or mounting of power plants in aircraft; Aircraft characterised by the type or position of power plants
    • B64D27/02—Aircraft characterised by the type or position of power plants
    • B64D27/16—Aircraft characterised by the type or position of power plants of jet type
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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)
  • Structures Of Non-Positive Displacement Pumps (AREA)
GB838321281A 1983-08-06 1983-08-06 Underwing engine installation Pending GB8321281D0 (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB838321281A GB8321281D0 (en) 1983-08-06 1983-08-06 Underwing engine installation
GB08419904A GB2144688B (en) 1983-08-06 1984-08-03 Underwing engine installation for aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB838321281A GB8321281D0 (en) 1983-08-06 1983-08-06 Underwing engine installation

Publications (1)

Publication Number Publication Date
GB8321281D0 true GB8321281D0 (en) 1983-09-28

Family

ID=10546964

Family Applications (2)

Application Number Title Priority Date Filing Date
GB838321281A Pending GB8321281D0 (en) 1983-08-06 1983-08-06 Underwing engine installation
GB08419904A Expired GB2144688B (en) 1983-08-06 1984-08-03 Underwing engine installation for aircraft

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB08419904A Expired GB2144688B (en) 1983-08-06 1984-08-03 Underwing engine installation for aircraft

Country Status (1)

Country Link
GB (2) GB8321281D0 (en)

Families Citing this family (29)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2555960B1 (en) * 1983-12-06 1986-09-19 Aerospatiale BOOM AIRCRAFT WING PROVIDED WITH A HYPERSUSTENTATOR SYSTEM AND AN ENGINE SUSPENSION MAT, AS WELL AS AN ENGINE SUSPENSION MAT FOR SUCH A WING
US5443230A (en) * 1993-12-21 1995-08-22 United Technologies Corporation Aircraft wing/nacelle combination
WO1998017529A1 (en) 1996-10-22 1998-04-30 The Boeing Company Airplane with unswept slotted cruise wing airfoil
DE19910551C2 (en) * 1999-03-10 2001-04-05 Eads Airbus Gmbh Aircraft wing with at least one short-coupled engine
US7059563B2 (en) 2003-06-03 2006-06-13 The Boeing Company Systems, apparatuses, and methods for moving aircraft control surfaces
US7243881B2 (en) 2003-06-03 2007-07-17 The Boeing Company Multi-function trailing edge devices and associated methods
US6964397B2 (en) 2003-07-18 2005-11-15 The Boeing Company Nacelle chine installation for drag reduction
US6799739B1 (en) 2003-11-24 2004-10-05 The Boeing Company Aircraft control surface drive system and associated methods
US7424350B2 (en) 2004-02-02 2008-09-09 The Boeing Company Vehicle control systems and corresponding sizing methods
US7270305B2 (en) 2004-06-15 2007-09-18 The Boeing Company Aircraft leading edge apparatuses and corresponding methods
US6978971B1 (en) 2004-06-15 2005-12-27 The Boeing Company Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7494094B2 (en) 2004-09-08 2009-02-24 The Boeing Company Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) 2004-09-30 2007-09-04 The Boeing Company Leading edge flap apparatuses and associated methods
US7322547B2 (en) 2005-01-31 2008-01-29 The Boeing Company Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) 2005-02-04 2008-03-04 The Boeing Company Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) 2005-04-27 2007-12-18 The Boeing Company Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7300021B2 (en) 2005-05-20 2007-11-27 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7721999B2 (en) 2005-05-20 2010-05-25 The Boeing Company Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) 2005-06-21 2008-05-06 The Boeing Company Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) 2005-08-10 2009-03-10 The Boeing Company Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) 2005-09-07 2009-11-03 The Boeing Company Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
US7708231B2 (en) 2005-11-21 2010-05-04 The Boeing Company Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7475854B2 (en) 2005-11-21 2009-01-13 The Boeing Company Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
FR2899201B1 (en) * 2006-03-31 2009-02-13 Airbus France Sas AIRCRAFT WING ARRANGEMENT COMPRISING A MOTOR ATTACHING MATTING DEFINING IN ZONE BEFORE A SIDE CHANNEL OF AIR FLOW
US7578484B2 (en) 2006-06-14 2009-08-25 The Boeing Company Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US7954769B2 (en) 2007-12-10 2011-06-07 The Boeing Company Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) 2007-12-11 2010-08-03 The Boeing Company Trailing edge device catchers and associated systems and methods
US8382045B2 (en) 2009-07-21 2013-02-26 The Boeing Company Shape-changing control surface
FR2954270B1 (en) * 2009-12-18 2012-06-01 Airbus Operations Sas AIR FENDER WITH MOBILE ATTACK INCOPORING A JUNCTION COMPONENT WITH THE ENGINE MAT

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB1118340A (en) * 1966-12-30 1968-07-03 Rolls Royce Mounting means for an aircraft engine
US4314681A (en) * 1979-08-31 1982-02-09 General Electric Company Drag-reducing component
EP0120009B1 (en) * 1982-09-30 1988-11-30 The Boeing Company Shock inducing pod for causing flow separation

Also Published As

Publication number Publication date
GB2144688A (en) 1985-03-13
GB8419904D0 (en) 1984-09-05
GB2144688B (en) 1986-09-17

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