GB952107A - A deflector assembly for controlling and deflecting the exhaust gases from a jet engine - Google Patents

A deflector assembly for controlling and deflecting the exhaust gases from a jet engine

Info

Publication number
GB952107A
GB952107A GB1843661A GB1843661A GB952107A GB 952107 A GB952107 A GB 952107A GB 1843661 A GB1843661 A GB 1843661A GB 1843661 A GB1843661 A GB 1843661A GB 952107 A GB952107 A GB 952107A
Authority
GB
United Kingdom
Prior art keywords
vane
vanes
range
deflecting
members
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
GB1843661A
Inventor
Michael Heinze Rueediger E Don
Frederick Bayley Sarsar
Yet Lin Yee
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.)
Northrop Grumman Corp
Original Assignee
Northrop Grumman Corp
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 Northrop Grumman Corp filed Critical Northrop Grumman Corp
Priority to GB1843661A priority Critical patent/GB952107A/en
Publication of GB952107A publication Critical patent/GB952107A/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/15—Control or regulation
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0066—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors with horizontal jet and jet deflector

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Supercharger (AREA)

Abstract

952,107. Deflecting jet streams on aircraft. NORTHROP CORPORATION. May 19, 1961, No. 18436/61. Headings B7G and B7W. [Also in Division G3] An aircraft jet propulsion engine thrust deflector has vanes 23-26 pivotally mounted in members 27, Fig. 6, and rotated by screw-jacks 28, control cables 32 and electrical apparatus (see Division G3). During the initial range of the rotation from a forward thrust position, Fig. 3, to a vertical thrust position, Fig. 2, via a S.T.O.L. position. Fig. 4, not shown, the vane 23 rotates through a greater angle than vane 24, vane 24 through a greater angle than vane 25 &c. and vice versa during the remaining range. The vanes co-operate to define convergentdivergent nozzles, Fig. 3, in the first range and convergent nozzles in the remaining range. Each vane is streamlined with maximum thickness located forward of the mid-section. This differential rotation of the vanes and the angle that members 27 make with the longitudinal axis of the engine, maintain a constant throat area l for each nozzle. The vanes may be moved to a reverse thrust position, Fig. 5, not shown.
GB1843661A 1961-05-19 1961-05-19 A deflector assembly for controlling and deflecting the exhaust gases from a jet engine Expired GB952107A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB1843661A GB952107A (en) 1961-05-19 1961-05-19 A deflector assembly for controlling and deflecting the exhaust gases from a jet engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1843661A GB952107A (en) 1961-05-19 1961-05-19 A deflector assembly for controlling and deflecting the exhaust gases from a jet engine

Publications (1)

Publication Number Publication Date
GB952107A true GB952107A (en) 1964-03-11

Family

ID=10112415

Family Applications (1)

Application Number Title Priority Date Filing Date
GB1843661A Expired GB952107A (en) 1961-05-19 1961-05-19 A deflector assembly for controlling and deflecting the exhaust gases from a jet engine

Country Status (1)

Country Link
GB (1) GB952107A (en)

Similar Documents

Publication Publication Date Title
GB937829A (en) Deflector assembly defining convergent nozzles
GB1040510A (en) Improvements in jet propulsion engines having thrust deflectors
US3032977A (en) Correlated bypass inlet and outlet control for a supersonic reaction powerplant
GB1179788A (en) Variable Area Exhaust Deflection System for a Gas Turbine Engine
GB1012780A (en) Improvements in dirigible thrust mechanism for jet propulsion engine
GB976449A (en) Improvements in thrust vectoring and modulating device
GB1019303A (en) Improvements in nozzle systems of jet propulsion engines
GB1161949A (en) Improvements in Aircraft Gas Generator Exhaust Nozzle Structures
GB1166396A (en) Improvements in Power Plant with Thrust Reverser.
GB1204268A (en) An exhaust arrangement for a jet engine
GB1262414A (en) Aircraft jet engine with vectoring nozzle for control purposes
GB1101663A (en) Variable area nozzles for jet propulsion engines
GB1114478A (en) Jet propulsion nozzle having a central bulbous body
GB952107A (en) A deflector assembly for controlling and deflecting the exhaust gases from a jet engine
GB1142660A (en) Improvements in combination jet exhaust nozzle and thrust reverser
GB908479A (en) Improvements in reingestion control means
GB1088153A (en) Improvements in thrust deflecting mechanism
GB1473543A (en) Gas turbine powerplants
GB1026590A (en) Aircraft having jet propulsion engines with thrust vectoring and modulating arrangements
GB1066268A (en) Jet propulsion power plant
GB1071075A (en) Improvements in aircraft
GB1132157A (en) Improvements in movable nozzles for directing the thrust of jet-propelled aircraft
GB1211492A (en) Improvements in or relating to apparatus for deflecting gas turbine engine exhaust gases
GB1061397A (en) Improvements in or relating to aircraft
GB979022A (en) Jet-controlled winged aircraft