GB580053A - Improvements in apparatus for increasing the magnus effect - Google Patents

Improvements in apparatus for increasing the magnus effect

Info

Publication number
GB580053A
GB580053A GB526344A GB526344A GB580053A GB 580053 A GB580053 A GB 580053A GB 526344 A GB526344 A GB 526344A GB 526344 A GB526344 A GB 526344A GB 580053 A GB580053 A GB 580053A
Authority
GB
United Kingdom
Prior art keywords
cylinder
discharged
interior
arms
rotor
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
GB526344A
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 GB526344A priority Critical patent/GB580053A/en
Publication of GB580053A publication Critical patent/GB580053A/en
Expired legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F03—MACHINES OR ENGINES FOR LIQUIDS; WIND, SPRING, OR WEIGHT MOTORS; PRODUCING MECHANICAL POWER OR A REACTIVE PROPULSIVE THRUST, NOT OTHERWISE PROVIDED FOR
    • F03D—WIND MOTORS
    • F03D3/00—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor 
    • F03D3/005—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  the axis being vertical
    • F03D3/007—Wind motors with rotation axis substantially perpendicular to the air flow entering the rotor  the axis being vertical using the Magnus effect
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/08—Influencing air flow over aircraft surfaces, not otherwise provided for using Magnus effect
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
    • Y02E10/00—Energy generation through renewable energy sources
    • Y02E10/70—Wind energy
    • Y02E10/74—Wind turbines with rotation axis perpendicular to the wind direction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Life Sciences & Earth Sciences (AREA)
  • Sustainable Development (AREA)
  • Sustainable Energy (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)

Abstract

580,053. Propelling ships and aircraft. MASSEY, H. P. March 21, 1944, No. 5263. [Classes 4 and 114] In order to increase the magnus lifting or propulsive effect of a rotating member, fluid is circulated through the interior of the member and discharged from openings in the periphery thereof. As applied to an aeroplane, Fig. 1, a hollow cylinder 12 is mounted at the leading edge of the wing 10, and air is supplied to the interior of the cylinder by a fan, or by the propeller of the aircraft, and discharged through radial or inclined slots 25 in the cylinder wall. The cylinder may be mounted near the mid section of the wing instead of at the leading edge, and may be of uniform diameter throughout its length or flared towards its outer end. As shown in Fig. 6, the invention may be utilised to augment the lift of helicopter rotor arms, a fan 70 supplying air to the rotor head from whence it passes to the interior of the arms and is discharged through slots 62 in the peripheral surface thereof. The rotor arms are rotated about their longitudinal axes by means of gear wheels 64 which mesh with gear teeth 66 on the rotor head. The air may be circulated through the rotor arms by means of fans at the outer ends thereof. When applied to the propulsion of ships the rotating member is mounted with its axis vertical.
GB526344A 1944-03-21 1944-03-21 Improvements in apparatus for increasing the magnus effect Expired GB580053A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB526344A GB580053A (en) 1944-03-21 1944-03-21 Improvements in apparatus for increasing the magnus effect

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB526344A GB580053A (en) 1944-03-21 1944-03-21 Improvements in apparatus for increasing the magnus effect

Publications (1)

Publication Number Publication Date
GB580053A true GB580053A (en) 1946-08-26

Family

ID=9792797

Family Applications (1)

Application Number Title Priority Date Filing Date
GB526344A Expired GB580053A (en) 1944-03-21 1944-03-21 Improvements in apparatus for increasing the magnus effect

Country Status (1)

Country Link
GB (1) GB580053A (en)

Cited By (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3473504A (en) * 1968-01-26 1969-10-21 Us Navy Water turbine drive for spinning flap control (or flettner rotor control)
WO1984003125A1 (en) * 1983-02-05 1984-08-16 Walter Tepe Method and device for utilizing wind energy
GB2213440A (en) * 1987-08-08 1989-08-16 Anthony Ngornadi Adimora Force generating apparatus
GB2266498A (en) * 1992-04-30 1993-11-03 Graeme Keith Walden Magnus effect lifter unit.
GB2316374A (en) * 1996-08-20 1998-02-25 Patrick Peebles Fluid dynamic lift generation
CN101672245B (en) * 2009-10-14 2012-07-04 上海大学 Horizontal-shaft wind turbine with rotating cylinder at front edge of paddle
CN103016260A (en) * 2012-11-26 2013-04-03 西安理工大学 Front edge wing and cylindrical wing combined wind turbine blade
EP2468628A3 (en) * 2010-12-22 2015-06-03 Airbus Defence and Space GmbH Hybrid rotor
WO2019106532A1 (en) * 2017-11-29 2019-06-06 Adriaan Francois Roberts Rotary machine
CN110242488A (en) * 2019-06-25 2019-09-17 哈尔滨工程大学 One kind being based on Magnus leading edge cylinder blade tide energy water conservancy generator
CN114030644A (en) * 2021-07-19 2022-02-11 中南大学 Novel fixed wing aircraft lift-increasing device suitable for Mars atmosphere and aircraft

Cited By (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3473504A (en) * 1968-01-26 1969-10-21 Us Navy Water turbine drive for spinning flap control (or flettner rotor control)
WO1984003125A1 (en) * 1983-02-05 1984-08-16 Walter Tepe Method and device for utilizing wind energy
GB2213440A (en) * 1987-08-08 1989-08-16 Anthony Ngornadi Adimora Force generating apparatus
GB2266498A (en) * 1992-04-30 1993-11-03 Graeme Keith Walden Magnus effect lifter unit.
GB2316374A (en) * 1996-08-20 1998-02-25 Patrick Peebles Fluid dynamic lift generation
CN101672245B (en) * 2009-10-14 2012-07-04 上海大学 Horizontal-shaft wind turbine with rotating cylinder at front edge of paddle
EP2468628A3 (en) * 2010-12-22 2015-06-03 Airbus Defence and Space GmbH Hybrid rotor
CN103016260A (en) * 2012-11-26 2013-04-03 西安理工大学 Front edge wing and cylindrical wing combined wind turbine blade
CN103016260B (en) * 2012-11-26 2014-10-01 西安理工大学 Front edge wing and cylindrical wing combined wind turbine blade
WO2019106532A1 (en) * 2017-11-29 2019-06-06 Adriaan Francois Roberts Rotary machine
CN110242488A (en) * 2019-06-25 2019-09-17 哈尔滨工程大学 One kind being based on Magnus leading edge cylinder blade tide energy water conservancy generator
CN114030644A (en) * 2021-07-19 2022-02-11 中南大学 Novel fixed wing aircraft lift-increasing device suitable for Mars atmosphere and aircraft
CN114030644B (en) * 2021-07-19 2024-02-09 中南大学 Fixed wing aircraft lift-increasing device suitable for Mars atmosphere and aircraft

Similar Documents

Publication Publication Date Title
US3814351A (en) Coaxial rotor yaw control
GB580053A (en) Improvements in apparatus for increasing the magnus effect
US1714917A (en) Propeller for aeroplanes
WO2020245379A8 (en) Aircraft with ducted propeller
US2609053A (en) Shrouded tail rotor
US2281203A (en) Driving mechanism for air rotors, especially aircraft sustaining rotors
GB1491253A (en) Variable length rotor or propeller blade
GB666491A (en) Improvements in or relating to aircraft
US3050007A (en) Propeller apparatus
GB1386335A (en) Rotary fluid moving propellor
US1971734A (en) Aircraft sustained by a lifting screw
US2544420A (en) Combustion chamber in rotating annular casing
US2612955A (en) Air screw, including a resonant pulse jet system
US3343768A (en) Aircraft
GB1003940A (en) Propellers, and convertiplanes equipped therewith
US2313934A (en) Tractor plane
GB383408A (en) Improvements in flying machines
US2449531A (en) Impeller
US2172932A (en) Variable pitch propeller
GB568548A (en) Improvements in aircraft
US2183555A (en) Aircraft
US1271896A (en) Aircraft.
GB666744A (en) Improvements in or relating to rotary wing sustained aircraft
US2453514A (en) Flying fuselage
JP1716076S (en) aircraft