GB781466A - Improvements in gaseous jet reaction nozzles - Google Patents

Improvements in gaseous jet reaction nozzles

Info

Publication number
GB781466A
GB781466A GB9325/54A GB932554A GB781466A GB 781466 A GB781466 A GB 781466A GB 9325/54 A GB9325/54 A GB 9325/54A GB 932554 A GB932554 A GB 932554A GB 781466 A GB781466 A GB 781466A
Authority
GB
United Kingdom
Prior art keywords
nozzles
supported
duct
diverging
thrust
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
GB9325/54A
Inventor
Charles Frederick Toms
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.)
HUNTING PERCIVAL AIRCRAFT Ltd
Original Assignee
HUNTING PERCIVAL 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 HUNTING PERCIVAL AIRCRAFT Ltd filed Critical HUNTING PERCIVAL AIRCRAFT Ltd
Priority to GB9325/54A priority Critical patent/GB781466A/en
Publication of GB781466A publication Critical patent/GB781466A/en
Expired legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet flaps

Abstract

781,466. Jet propulsion plant. HUNTING PERCIVAL AIRCRAFT, Ltd. June 27, 1955 [March 30, 1954], No. 9325/54. Class 110 (3). [Also in Group XXXIII] A gaseous jet reaction nozzle for the propulsion, lift, or control of aircraft comprises a smooth continuous duct 11, Fig. 1, having at one end a pair of diverging walls 12, 13 and a wedge-shaped diverting member 16 having its apex directed towards the duct, so as to divide the duct outlet into two diverging nozzles through which the flow is diverted, said member being arranged for movement towards and away from said walls to vary the relative sizes of the nozzles and hence the value and/or direction of the thrust. The member 16 is supported in Fig. 1 by two parallel links 22 fixed to shafts 23 supported by fixed structure 24. A lever 28 is secured to one shaft 23 as a control. In Fig. 4, there are two members 30, 31 adapted to divide the duct outlet into a central nozzle and two diverging side nozzles. The members are supported by parallel links 35, 36 on pivots 37, 38, and are shown in full lines in the position in which maximum thrust is developed, and are shown shaded and in chain lines in the position in which minimum thrust is developed.
GB9325/54A 1954-03-30 1954-03-30 Improvements in gaseous jet reaction nozzles Expired GB781466A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB9325/54A GB781466A (en) 1954-03-30 1954-03-30 Improvements in gaseous jet reaction nozzles

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB9325/54A GB781466A (en) 1954-03-30 1954-03-30 Improvements in gaseous jet reaction nozzles

Publications (1)

Publication Number Publication Date
GB781466A true GB781466A (en) 1957-08-21

Family

ID=9869781

Family Applications (1)

Application Number Title Priority Date Filing Date
GB9325/54A Expired GB781466A (en) 1954-03-30 1954-03-30 Improvements in gaseous jet reaction nozzles

Country Status (1)

Country Link
GB (1) GB781466A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2981061A (en) * 1959-07-03 1961-04-25 Robert W Lilligren Gyroscopic stabilizer for rocket
EP0126399A1 (en) * 1983-05-13 1984-11-28 Robertson GAL Gesellschaft für angewandte Lufttechnik mbH Fluid duct presenting a reduced construction
GB2282854A (en) * 1993-10-01 1995-04-19 Znamensky Vladimir P Method and nozzle for producing thrust
GB2292125A (en) * 1981-10-13 1996-02-14 Rolls Royce Thrust vectoring gas turbine engine nozzle
JP2007532826A (en) * 2004-04-13 2007-11-15 エアロジェット−ジェネラル・コーポレーション Thrust vector control system for plug-nozzle rocket engine

Cited By (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2981061A (en) * 1959-07-03 1961-04-25 Robert W Lilligren Gyroscopic stabilizer for rocket
GB2292125A (en) * 1981-10-13 1996-02-14 Rolls Royce Thrust vectoring gas turbine engine nozzle
US5499765A (en) * 1981-10-13 1996-03-19 Rolls-Royce Limited Nozzle capable of varying the direction of discharge of fluid therefrom
GB2292125B (en) * 1981-10-13 1996-07-10 Rolls Royce Nozzle capable of varying the direction of discharge of fluid therefrom
EP0126399A1 (en) * 1983-05-13 1984-11-28 Robertson GAL Gesellschaft für angewandte Lufttechnik mbH Fluid duct presenting a reduced construction
GB2282854A (en) * 1993-10-01 1995-04-19 Znamensky Vladimir P Method and nozzle for producing thrust
JP2007532826A (en) * 2004-04-13 2007-11-15 エアロジェット−ジェネラル・コーポレーション Thrust vector control system for plug-nozzle rocket engine

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