GB1024894A - Improvements in aircraft jet-propulsion power-plants - Google Patents

Improvements in aircraft jet-propulsion power-plants

Info

Publication number
GB1024894A
GB1024894A GB19545/63A GB1954563A GB1024894A GB 1024894 A GB1024894 A GB 1024894A GB 19545/63 A GB19545/63 A GB 19545/63A GB 1954563 A GB1954563 A GB 1954563A GB 1024894 A GB1024894 A GB 1024894A
Authority
GB
United Kingdom
Prior art keywords
turbo
fan
aircraft
fan unit
central
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
GB19545/63A
Inventor
John Wotton
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.)
Vickers Armstrongs Aircraft Ltd
Original Assignee
Vickers Armstrongs Aircraft 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 Vickers Armstrongs Aircraft Ltd filed Critical Vickers Armstrongs Aircraft Ltd
Priority to GB19545/63A priority Critical patent/GB1024894A/en
Priority to DE19641431145 priority patent/DE1431145A1/en
Priority to NL6405438A priority patent/NL6405438A/xx
Publication of GB1024894A publication Critical patent/GB1024894A/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
    • B64D29/00—Power-plant nacelles, fairings, or cowlings
    • B64D29/04—Power-plant nacelles, fairings, or cowlings associated with fuselages
    • 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

Landscapes

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

Abstract

1,024,894. Aircraft power plant. VICKERSARMSTBONG (AIRCRAFT) Ltd. May 7, 1964 [May 16, 1963], No. 19545/63. Heading B7G. An aircraft jet-propulsion engine installation comprises a central engine 12 (Fig. 2, not shown), buried in the tail end of the fuselage and two outboard engines 13, 14 respectively mounted in nacelles or pods attached to the opposite sides of the fuselage 10 laterally of said central engine, each of said engines being a by-pass gas turbine unit having at its after end a supplementary turbo fan unit 127, 137, 147 respectively and an annular cowl 125, 135, 145 surrounding the respective turbo-fan unit and arranged to receive boundary layer air from surfaces lying ahead thereof, the rotor of each turbo-fan unit being furnished with fan-blades which extend into, and or rotating, sweep the interior of its respective cowl to ingest said boundary layer air therein. The fairing for the central turbo-fan 127 may have an additional air entry duct and the outboard engines may have thrust reversing units 134, 144. The jet nozzles 123, 133, 143 may have elliptical profiles and transverse extensible rods, whereby the profiles may be altered in shape. Reference has been directed by the Comptroller to Specification 974,384.
GB19545/63A 1963-05-16 1963-05-16 Improvements in aircraft jet-propulsion power-plants Expired GB1024894A (en)

Priority Applications (3)

Application Number Priority Date Filing Date Title
GB19545/63A GB1024894A (en) 1963-05-16 1963-05-16 Improvements in aircraft jet-propulsion power-plants
DE19641431145 DE1431145A1 (en) 1963-05-16 1964-05-12 Jet engine for aircraft
NL6405438A NL6405438A (en) 1963-05-16 1964-05-15

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19545/63A GB1024894A (en) 1963-05-16 1963-05-16 Improvements in aircraft jet-propulsion power-plants

Publications (1)

Publication Number Publication Date
GB1024894A true GB1024894A (en) 1966-04-06

Family

ID=10131179

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19545/63A Expired GB1024894A (en) 1963-05-16 1963-05-16 Improvements in aircraft jet-propulsion power-plants

Country Status (3)

Country Link
DE (1) DE1431145A1 (en)
GB (1) GB1024894A (en)
NL (1) NL6405438A (en)

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR3012417A1 (en) * 2013-10-31 2015-05-01 Snecma TURBOREACTOR NACELLE
EP2597037A3 (en) * 2011-11-24 2015-11-25 Rolls-Royce plc An Aircraft
US9266617B2 (en) 2011-10-24 2016-02-23 Rolls-Royce Plc Propulsive system
EP3048042A1 (en) * 2015-01-23 2016-07-27 General Electric Company Gas-electric propulsion system for an aircraft
US9764848B1 (en) 2016-03-07 2017-09-19 General Electric Company Propulsion system for an aircraft
WO2018057230A1 (en) * 2016-09-21 2018-03-29 General Electric Company Aircraft having an aft engine
WO2018057242A1 (en) * 2016-09-26 2018-03-29 General Electric Company Aircraft having an aft engine
WO2019243119A1 (en) * 2018-06-21 2019-12-26 Safran Rear propulsion system for an aircraft
US10762726B2 (en) 2017-06-13 2020-09-01 General Electric Company Hybrid-electric propulsion system for an aircraft
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9266617B2 (en) 2011-10-24 2016-02-23 Rolls-Royce Plc Propulsive system
EP2597037A3 (en) * 2011-11-24 2015-11-25 Rolls-Royce plc An Aircraft
FR3012417A1 (en) * 2013-10-31 2015-05-01 Snecma TURBOREACTOR NACELLE
US11673678B2 (en) 2015-01-23 2023-06-13 General Electric Company Gas-electric propulsion system for an aircraft
US10000293B2 (en) 2015-01-23 2018-06-19 General Electric Company Gas-electric propulsion system for an aircraft
EP3048042A1 (en) * 2015-01-23 2016-07-27 General Electric Company Gas-electric propulsion system for an aircraft
US10414508B2 (en) 2015-01-23 2019-09-17 General Electric Company Gas-electric propulsion system for an aircraft
US11312502B2 (en) 2015-01-23 2022-04-26 General Electric Company Gas-electric propulsion system for an aircraft
US9764848B1 (en) 2016-03-07 2017-09-19 General Electric Company Propulsion system for an aircraft
WO2018057230A1 (en) * 2016-09-21 2018-03-29 General Electric Company Aircraft having an aft engine
US11299283B2 (en) 2016-09-21 2022-04-12 General Electric Company Aircraft having an aft engine
US10370110B2 (en) 2016-09-21 2019-08-06 General Electric Company Aircraft having an aft engine
EP3984879A1 (en) * 2016-09-21 2022-04-20 General Electric Company Aircraft having an aft engine
US10364021B2 (en) 2016-09-26 2019-07-30 General Electric Company Aircraft having an aft engine and stabilizer root fillet
WO2018057242A1 (en) * 2016-09-26 2018-03-29 General Electric Company Aircraft having an aft engine
US10762726B2 (en) 2017-06-13 2020-09-01 General Electric Company Hybrid-electric propulsion system for an aircraft
WO2019243119A1 (en) * 2018-06-21 2019-12-26 Safran Rear propulsion system for an aircraft
US11097849B2 (en) 2018-09-10 2021-08-24 General Electric Company Aircraft having an aft engine

Also Published As

Publication number Publication date
NL6405438A (en) 1964-11-17
DE1431145A1 (en) 1968-11-28

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