GB1397068A - Aircraft - Google Patents

Aircraft

Info

Publication number
GB1397068A
GB1397068A GB2968971A GB2968971A GB1397068A GB 1397068 A GB1397068 A GB 1397068A GB 2968971 A GB2968971 A GB 2968971A GB 2968971 A GB2968971 A GB 2968971A GB 1397068 A GB1397068 A GB 1397068A
Authority
GB
United Kingdom
Prior art keywords
wing
engine
aircraft
jet
deflectors
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
GB2968971A
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.)
Hawker Siddeley Aviation Ltd
Original Assignee
Hawker Siddeley Aviation Ltd
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 Hawker Siddeley Aviation Ltd filed Critical Hawker Siddeley Aviation Ltd
Priority to GB2968971A priority Critical patent/GB1397068A/en
Publication of GB1397068A publication Critical patent/GB1397068A/en
Expired legal-status Critical Current

Links

Classifications

    • 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
    • B64D27/20—Aircraft characterised by the type or position of power plants of jet type within, or attached to, fuselages
    • 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
    • Y02T50/40—Weight reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

1397068 Jet propulsion engines on aircraft HAWKER SIDDELEY AVIATION Ltd 26 June 1972 29689/71 Heading B7G An aircraft has jet propulsion engines 17 mounted so that their air intakes 20 are over the trailing edge of wing 10 and their efflux passes over tailplane 15. The wing is of low aspect ratio or delta shape and is preferably a double delta, the leading edge having an inboard part 11 strongly swept back and an outboard part less strongly swept back. The bypass air from each engine is split and delivered rearwardly from ducts 18 on either side of main jet 19, so that the total jet efflux is flattened. The engine may also have a forward extension (24), Fig. 5 (not shown), leading to a flattened air intake (25). Lift fans 21 may be mounted in the wing, and lift may be augmented by cascade deflectors 22 on the tail plane 15 or by deflectors (23), Fig. 4 (not shown), integral with the engine pod.
GB2968971A 1971-06-24 1971-06-24 Aircraft Expired GB1397068A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2968971A GB1397068A (en) 1971-06-24 1971-06-24 Aircraft

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2968971A GB1397068A (en) 1971-06-24 1971-06-24 Aircraft

Publications (1)

Publication Number Publication Date
GB1397068A true GB1397068A (en) 1975-06-11

Family

ID=10295537

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2968971A Expired GB1397068A (en) 1971-06-24 1971-06-24 Aircraft

Country Status (1)

Country Link
GB (1) GB1397068A (en)

Cited By (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2873096A1 (en) * 2004-07-15 2006-01-20 Airbus France Sas MULTI-ENGINE
FR2892705A1 (en) * 2005-11-03 2007-05-04 Airbus France Sas Aircraft with reduced environmental impact has one or more rear-mounted turboprop engines between vertical fins or horizontal planes of tail assembly
FR2899200A1 (en) 2006-03-28 2007-10-05 Airbus France Sas Commercial aircraft, has fairing articulated with respect to propeller drive such that air stream blown by counter-rotative propellers is oriented with respect to axis of drive for controlling direction and depth of aircraft
FR2900906A1 (en) * 2006-05-09 2007-11-16 Airbus France Sas Engine e.g. turbo shaft engine, fixation system for aircraft, has holding fastening device with skid and cradles integrated with masts and fan casing, respectively, where cradles have articulation axes traversing, with clearances, orifices
FR2905356A1 (en) 2006-09-05 2008-03-07 Airbus France Sas Aircraft e.g. commercial aircraft, fabricating method, involves arranging turbo-propeller between wings and horizontal tail, such that lower part of one lobe partially meets wings and lower part of another lobe partially meets tail
FR2919268A1 (en) * 2007-07-26 2009-01-30 Airbus France Sa SHIPPING PLANE
FR2919267A1 (en) * 2007-07-26 2009-01-30 Airbus France Sa Aircraft e.g. silence aircraft, has high-bypass-ratio fan engines placed side-by-side in propulsion system such that outlets of nozzles are located between vertical fins of vertical tail, above fuselage in front of rear end of fuselage
WO2010103252A1 (en) * 2009-03-12 2010-09-16 Airbus Operations (S.A.S.) Airplane with a tailcoat tail assembly and rear engine
JP2012106726A (en) * 2010-11-15 2012-06-07 Boeing Co:The Method and apparatus for reducing aircraft noise
US8608109B2 (en) 2011-11-10 2013-12-17 The Boeing Company Payload use of wing to body volume in an elliptical fuselage
ES2435805A1 (en) * 2012-06-22 2013-12-23 Fº JAVIER PORRAS VILA Anti-fall system of an aircraft, with rear spoiler for nozzle (Machine-translation by Google Translate, not legally binding)
CN109911194A (en) * 2018-11-22 2019-06-21 周雯韵 A kind of short distance or vertically taking off and landing flyer using distributed power system
CN112498679A (en) * 2020-12-14 2021-03-16 江西洪都航空工业股份有限公司 Tilting composite power aircraft
CN112678206A (en) * 2020-12-29 2021-04-20 中国航天空气动力技术研究院 Pneumatic layout structure and design method of reusable carrier
US20210339844A1 (en) * 2020-04-29 2021-11-04 Airbus Operations S.L. Rear end section for an aircraft

Cited By (28)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2873096A1 (en) * 2004-07-15 2006-01-20 Airbus France Sas MULTI-ENGINE
WO2006016031A1 (en) * 2004-07-15 2006-02-16 Airbus France Multi-engine aircraft
US7905449B2 (en) 2004-07-15 2011-03-15 Airbus France Multi-engine aircraft
CN101300171B (en) * 2005-11-03 2012-07-04 空中客车运营简化股份公司 Aircraft having a reduced environmental impact
US8313055B2 (en) 2005-11-03 2012-11-20 Airbus Operations Sas Aircraft having a reduced environmental impact
WO2007051914A1 (en) * 2005-11-03 2007-05-10 Airbus France Aircraft having a reduced environmental impact
FR2892705A1 (en) * 2005-11-03 2007-05-04 Airbus France Sas Aircraft with reduced environmental impact has one or more rear-mounted turboprop engines between vertical fins or horizontal planes of tail assembly
FR2899200A1 (en) 2006-03-28 2007-10-05 Airbus France Sas Commercial aircraft, has fairing articulated with respect to propeller drive such that air stream blown by counter-rotative propellers is oriented with respect to axis of drive for controlling direction and depth of aircraft
US7819358B2 (en) 2006-03-28 2010-10-26 Airbus France Aircraft with reduced environmental impact
FR2900906A1 (en) * 2006-05-09 2007-11-16 Airbus France Sas Engine e.g. turbo shaft engine, fixation system for aircraft, has holding fastening device with skid and cradles integrated with masts and fan casing, respectively, where cradles have articulation axes traversing, with clearances, orifices
US8328132B2 (en) 2006-05-09 2012-12-11 Airbus Operations Sas Damage-tolerant attachment system for an aircraft engine
FR2905356A1 (en) 2006-09-05 2008-03-07 Airbus France Sas Aircraft e.g. commercial aircraft, fabricating method, involves arranging turbo-propeller between wings and horizontal tail, such that lower part of one lobe partially meets wings and lower part of another lobe partially meets tail
US7926760B2 (en) 2006-09-05 2011-04-19 Airbus France Method for producing an aircraft with reduced environmental impact and the aircraft thus obtained
US8152095B2 (en) 2007-07-26 2012-04-10 Airbus France Aircraft having a reduced acoustic signature
FR2919267A1 (en) * 2007-07-26 2009-01-30 Airbus France Sa Aircraft e.g. silence aircraft, has high-bypass-ratio fan engines placed side-by-side in propulsion system such that outlets of nozzles are located between vertical fins of vertical tail, above fuselage in front of rear end of fuselage
FR2919268A1 (en) * 2007-07-26 2009-01-30 Airbus France Sa SHIPPING PLANE
US8523101B2 (en) 2007-07-26 2013-09-03 Airbus Operations Sas Short take-off aircraft
US8651414B2 (en) 2009-03-12 2014-02-18 Airbus Operations S.A.S. Airplane with a tailcoat tail assembly and rear engine
FR2943039A1 (en) * 2009-03-12 2010-09-17 Airbus France PLANE TANK-TAIL AND REVERSE ENGINE.
WO2010103252A1 (en) * 2009-03-12 2010-09-16 Airbus Operations (S.A.S.) Airplane with a tailcoat tail assembly and rear engine
EP2452877A3 (en) * 2010-11-15 2014-10-08 The Boeing Company Method and apparatus for reducing aircraft noise
JP2012106726A (en) * 2010-11-15 2012-06-07 Boeing Co:The Method and apparatus for reducing aircraft noise
US8608109B2 (en) 2011-11-10 2013-12-17 The Boeing Company Payload use of wing to body volume in an elliptical fuselage
ES2435805A1 (en) * 2012-06-22 2013-12-23 Fº JAVIER PORRAS VILA Anti-fall system of an aircraft, with rear spoiler for nozzle (Machine-translation by Google Translate, not legally binding)
CN109911194A (en) * 2018-11-22 2019-06-21 周雯韵 A kind of short distance or vertically taking off and landing flyer using distributed power system
US20210339844A1 (en) * 2020-04-29 2021-11-04 Airbus Operations S.L. Rear end section for an aircraft
CN112498679A (en) * 2020-12-14 2021-03-16 江西洪都航空工业股份有限公司 Tilting composite power aircraft
CN112678206A (en) * 2020-12-29 2021-04-20 中国航天空气动力技术研究院 Pneumatic layout structure and design method of reusable carrier

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Legal Events

Date Code Title Description
PS Patent sealed
732 Registration of transactions, instruments or events in the register (sect. 32/1977)
PCNP Patent ceased through non-payment of renewal fee
732 Registration of transactions, instruments or events in the register (sect. 32/1977)