GB1094913A - Improvements in or relating to turbojet engines for vertical take-off and landing aircraft - Google Patents

Improvements in or relating to turbojet engines for vertical take-off and landing aircraft

Info

Publication number
GB1094913A
GB1094913A GB1585265A GB1585265A GB1094913A GB 1094913 A GB1094913 A GB 1094913A GB 1585265 A GB1585265 A GB 1585265A GB 1585265 A GB1585265 A GB 1585265A GB 1094913 A GB1094913 A GB 1094913A
Authority
GB
United Kingdom
Prior art keywords
nozzles
engine
relating
vertical take
axis
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
GB1585265A
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.)
MAN Turbo GmbH
Original Assignee
MAN Turbo GmbH
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 MAN Turbo GmbH filed Critical MAN Turbo GmbH
Publication of GB1094913A publication Critical patent/GB1094913A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • F02K1/004—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector by using one or more swivable nozzles rotating about their own axis

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Transmission Devices (AREA)
  • Toys (AREA)

Abstract

1,094,913. Jet propelled aircraft. M.A.N. TURBO G.m.b.H. April 13, 1965 [April 16, 1964], No. 15852/65. Heading B7G. A by-pass gas turbine engine has two propelling nozzles 7 rotatable about a common transverse axis, each comprising an elbow bend and an arcuate portion downstream of the bend so that the thrust vectors pass forwardly of the said axis when the engine, disposed with its axis horizontal, is producing direct lift. The nozzles are rotated, either independently or together, by jacks acting on the peripheries of the rotatable nozzles at their mounting, or on a shaft 9 on which they are mounted. The nozzles may be mounted on the engine, or on a nacelle or fuselage containing the engine. The shaft 9 has guide vanes 15 fixed to it.
GB1585265A 1964-04-16 1965-04-13 Improvements in or relating to turbojet engines for vertical take-off and landing aircraft Expired GB1094913A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DEM60671A DE1219804B (en) 1964-04-16 1964-04-16 Turbine jet engine for aircraft taking off and landing vertically

Publications (1)

Publication Number Publication Date
GB1094913A true GB1094913A (en) 1967-12-13

Family

ID=7309903

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1585265A Expired GB1094913A (en) 1964-04-16 1965-04-13 Improvements in or relating to turbojet engines for vertical take-off and landing aircraft

Country Status (2)

Country Link
DE (1) DE1219804B (en)
GB (1) GB1094913A (en)

Also Published As

Publication number Publication date
DE1219804B (en) 1966-06-23

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