GB545587A - Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions - Google Patents

Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions

Info

Publication number
GB545587A
GB545587A GB149741A GB149741A GB545587A GB 545587 A GB545587 A GB 545587A GB 149741 A GB149741 A GB 149741A GB 149741 A GB149741 A GB 149741A GB 545587 A GB545587 A GB 545587A
Authority
GB
United Kingdom
Prior art keywords
vanes
shaft
blades
guide pin
camber
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
GB149741A
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.)
JAMES RUSSELL KENNEDY
Original Assignee
JAMES RUSSELL KENNEDY
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 JAMES RUSSELL KENNEDY filed Critical JAMES RUSSELL KENNEDY
Priority to GB149741A priority Critical patent/GB545587A/en
Publication of GB545587A publication Critical patent/GB545587A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B63SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63HMARINE PROPULSION OR STEERING
    • B63H5/00Arrangements on vessels of propulsion elements directly acting on water
    • B63H5/07Arrangements on vessels of propulsion elements directly acting on water of propellers
    • B63H5/14Arrangements on vessels of propulsion elements directly acting on water of propellers characterised by being mounted in non-rotating ducts or rings, e.g. adjustable for steering purpose
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C11/00Propellers, e.g. of ducted type; Features common to propellers and rotors for rotorcraft
    • B64C11/001Shrouded propellers

Abstract

545,587. Screw propellers, fans and the like. ADAMTCHIK, M. T., and KENNEDY, J. R. Feb. 4, 1941, No. 1497. [Class 114] [Also in Group XXVI] For directing the flow of fluid on to the propelling or impelling blades of a marine or air craft, pump, fan or turbine, a number of flexible vanes, which are variable both in pitch and in camber, is pivotally mounted on axes that are stationary relative to the propelling or impelling blades, enabling the vanes to be set either at a positive or negative angle to the general direction of flow of the fluid. In the construction shown in Fig. 1, in which the vanes 9 are supported between a boss I and an outer casing 3 so as to be applied as a self-contained unit to the aircraft or engine frame in advance of the propeller hub 24 and blades 4, each vane.is carried by a sleeve 8 rotatable upon a shaft 7 extending between the boss 1 and casing 3, and.is also connected to a second shaft 12 from which extends a guide pin 17, while a sleeve 18 surrounding the shaft is provided with a guide pin 19 at its inner end. The guide pins 17, 19 and a third guide pin 16 attached by a lever 14, Fig. 4, to the shaft 8 engage slots 20, 21, 22 in a sliding control plate 23, Fig. 3, the inclination of the slots being so arranged that, as the plate 23 is displaced in either direction from its mid position, the vanes 9 are swung to a positive or negative angle and at the same time are flexed to a curved form as shown in the extreme positions in Fig. 5. Preferably, the number of vanes 9 differs from the number of propeller blades 4, while the sliding plates 23 controlling the vanes are simultaneously operated. In a modification, Fig. 8,. in which the vanes 29 are associated with the blades 42 of an impeller fan or pump, and are secured to shafts 28, simultaneous adjustment of the vanes is effected by means of a rotatable ring 41 connected to levers 35 which are engaged by pins 33 depending from ball joints 32 disposed at the inner ends of the shaft 31 that determine the pitch and camber of the vanes 29.
GB149741A 1941-02-04 1941-02-04 Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions Expired GB545587A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB149741A GB545587A (en) 1941-02-04 1941-02-04 Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB149741A GB545587A (en) 1941-02-04 1941-02-04 Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions

Publications (1)

Publication Number Publication Date
GB545587A true GB545587A (en) 1942-06-03

Family

ID=9723015

Family Applications (1)

Application Number Title Priority Date Filing Date
GB149741A Expired GB545587A (en) 1941-02-04 1941-02-04 Improvements in and relating to apparatus applicable to screw propellors for obtaining maximum efficiency under all conditions

Country Status (1)

Country Link
GB (1) GB545587A (en)

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3397836A (en) * 1967-01-03 1968-08-20 Gen Motors Corp Flexible vane and variable vane cascades
US4075500A (en) * 1975-08-13 1978-02-21 Grumman Aerospace Corporation Variable stator, diffuser augmented wind turbine electrical generation system
GB2149022A (en) * 1983-10-27 1985-06-05 Rolls Royce Warpable guide vanes for turbomachines
WO2005014980A1 (en) * 2003-08-12 2005-02-17 Honeywell International Inc. Variable nozzle device made from sheet metal
WO2005064151A1 (en) * 2003-12-31 2005-07-14 Envision Corporation Wind powered turbine engine
US7726935B2 (en) 2004-05-19 2010-06-01 Envision Corporation Wind turbine rotor projection
US7726933B2 (en) 2003-12-31 2010-06-01 Envision Corporation Wind powered turbine engine—horizontal rotor configuration
EP3093235A1 (en) * 2015-05-13 2016-11-16 Rolls-Royce plc Aircraft
CN110242578A (en) * 2019-07-17 2019-09-17 安德里茨(中国)有限公司 Axial flow pump blade inner angle adjustment device and axial-flow pump

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3397836A (en) * 1967-01-03 1968-08-20 Gen Motors Corp Flexible vane and variable vane cascades
US4075500A (en) * 1975-08-13 1978-02-21 Grumman Aerospace Corporation Variable stator, diffuser augmented wind turbine electrical generation system
GB2149022A (en) * 1983-10-27 1985-06-05 Rolls Royce Warpable guide vanes for turbomachines
WO2005014980A1 (en) * 2003-08-12 2005-02-17 Honeywell International Inc. Variable nozzle device made from sheet metal
CN100419221C (en) * 2003-08-12 2008-09-17 霍尼韦尔国际公司 Variable nozzle device made from sheet metal
US7845899B2 (en) 2003-12-31 2010-12-07 Envision Corporation Fluid powered turbine engine
WO2005064151A1 (en) * 2003-12-31 2005-07-14 Envision Corporation Wind powered turbine engine
US7726933B2 (en) 2003-12-31 2010-06-01 Envision Corporation Wind powered turbine engine—horizontal rotor configuration
US7726935B2 (en) 2004-05-19 2010-06-01 Envision Corporation Wind turbine rotor projection
EP3093235A1 (en) * 2015-05-13 2016-11-16 Rolls-Royce plc Aircraft
US10358229B2 (en) 2015-05-13 2019-07-23 Rolls-Royce Plc Aircraft
CN110242578A (en) * 2019-07-17 2019-09-17 安德里茨(中国)有限公司 Axial flow pump blade inner angle adjustment device and axial-flow pump
CN110242578B (en) * 2019-07-17 2024-04-09 安德里茨(中国)有限公司 Axial flow pump blade angle adjusting device and axial flow pump

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