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GB629143A - Improvements in or relating to aircraft power unit installations - Google Patents

Improvements in or relating to aircraft power unit installations

Info

Publication number
GB629143A
GB629143A GB19233/47A GB1923347A GB629143A GB 629143 A GB629143 A GB 629143A GB 19233/47 A GB19233/47 A GB 19233/47A GB 1923347 A GB1923347 A GB 1923347A GB 629143 A GB629143 A GB 629143A
Authority
GB
United Kingdom
Prior art keywords
units
turbine
unit
aircraft
group
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
GB19233/47A
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.)
Individual
Original Assignee
Individual
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 Individual filed Critical Individual
Priority to GB19233/47A priority Critical patent/GB629143A/en
Publication of GB629143A publication Critical patent/GB629143A/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
    • B64D27/18—Aircraft characterised by the type or position of power plants of jet type within, or attached to, wings
    • 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
    • B64D27/10—Aircraft characterised by the type or position of power plants of gas-turbine type 
    • B64D27/12—Aircraft characterised by the type or position of power plants of gas-turbine type  within, or attached to, wings
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
    • F02C6/02—Plural gas-turbine plants having a common power output

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)

Abstract

629,143. Aircraft power plant. WHITTLE, F. July 18, 1947, No. 19233. [Class 4] [Also in Group XXVI] An aircraft power plant installation comprises two or more gas turbine units grouped in echelon formation relatively to the longitudinal axis of the machine and so arranged that the frontal aspect or outline of each unit (except the leading unit) is partly obscured by that of the unit ahead of it, in order that the aggregate effective frontal area of the group is less than the sum of the frontal areas of the several units. Figs. 1 and 2 show a group of two gas turbines 1, 1 arranged in a nacelle 2, the outboard unit being arranged with its compressor casing adjacent the jet tube of the inboard unit. As shown, the turbine-compressor axes of the two units are inclined to the fore- and-aft axis of the aircraft and the rear ends of the jet tubes are parallel thereto, but the axes of both units may be parallel to the aircraft axis. Fig. 5 shows a group of three turbines with their turbine-compressor axes parallel to the aircraft axis, but with the jet tubes of the inboard and outboard units diverging fanwise. The exhaust ducts of some or all of the units may converge into a common duct. In the further embodiment according to Fig. 7 the exhaust ducts 1 of two turbines 2 converge to an annular duct 3 housing a turbine 5 driving a pusher propeller 10, or a ducted fan, the turbine exhaust being discharged through two lateral ducts 7 disposed one on either side of the propeller or fan.
GB19233/47A 1947-07-18 1947-07-18 Improvements in or relating to aircraft power unit installations Expired GB629143A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB19233/47A GB629143A (en) 1947-07-18 1947-07-18 Improvements in or relating to aircraft power unit installations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB19233/47A GB629143A (en) 1947-07-18 1947-07-18 Improvements in or relating to aircraft power unit installations

Publications (1)

Publication Number Publication Date
GB629143A true GB629143A (en) 1949-09-13

Family

ID=10125921

Family Applications (1)

Application Number Title Priority Date Filing Date
GB19233/47A Expired GB629143A (en) 1947-07-18 1947-07-18 Improvements in or relating to aircraft power unit installations

Country Status (1)

Country Link
GB (1) GB629143A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3036285A (en) * 1957-11-29 1962-05-22 Bryant Electric Co Wiring device
FR3043648A1 (en) * 2015-11-13 2017-05-19 Snecma PROPELLANT VOILURE OF AN AIRCRAFT
US10421553B2 (en) * 2015-01-20 2019-09-24 United Technologies Corporation Pusher fan engine with in wing configuration
US11286885B2 (en) * 2013-08-15 2022-03-29 Raytheon Technologies Corporation External core gas turbine engine assembly

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3036285A (en) * 1957-11-29 1962-05-22 Bryant Electric Co Wiring device
US11286885B2 (en) * 2013-08-15 2022-03-29 Raytheon Technologies Corporation External core gas turbine engine assembly
US10421553B2 (en) * 2015-01-20 2019-09-24 United Technologies Corporation Pusher fan engine with in wing configuration
FR3043648A1 (en) * 2015-11-13 2017-05-19 Snecma PROPELLANT VOILURE OF AN AIRCRAFT
US10450079B2 (en) 2015-11-13 2019-10-22 Safran Aircraft Engines Propulsive wing of an aircraft

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