ES2144416T3 - Dispositivo de aleron con rotor y metodo correspondiente. - Google Patents

Dispositivo de aleron con rotor y metodo correspondiente.

Info

Publication number
ES2144416T3
ES2144416T3 ES92912183T ES92912183T ES2144416T3 ES 2144416 T3 ES2144416 T3 ES 2144416T3 ES 92912183 T ES92912183 T ES 92912183T ES 92912183 T ES92912183 T ES 92912183T ES 2144416 T3 ES2144416 T3 ES 2144416T3
Authority
ES
Spain
Prior art keywords
rotor
wing
flap apparatus
craft
landing
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 - Lifetime
Application number
ES92912183T
Other languages
English (en)
Inventor
Frank S Malvestuto Jr
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
Application granted granted Critical
Publication of ES2144416T3 publication Critical patent/ES2144416T3/es
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C3/00—Wings
    • B64C3/10—Shape of wings
    • B64C3/14—Aerofoil profile
    • B64C3/141—Circulation Control Airfoils
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
    • B63B—SHIPS OR OTHER WATERBORNE VESSELS; EQUIPMENT FOR SHIPPING 
    • B63B1/00—Hydrodynamic or hydrostatic features of hulls or of hydrofoils
    • B63B1/16—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces
    • B63B1/24—Hydrodynamic or hydrostatic features of hulls or of hydrofoils deriving additional lift from hydrodynamic forces of hydrofoil type
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C19/00—Aircraft control not otherwise provided for
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C23/00—Influencing air flow over aircraft surfaces, not otherwise provided for
    • B64C23/02—Influencing air flow over aircraft surfaces, not otherwise provided for by means of rotating members of cylindrical or similar form
    • 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
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Combustion & Propulsion (AREA)
  • Chemical & Material Sciences (AREA)
  • Ocean & Marine Engineering (AREA)
  • Other Liquid Machine Or Engine Such As Wave Power Use (AREA)
  • Auxiliary Devices For And Details Of Packaging Control (AREA)
  • Toys (AREA)
  • Hydraulic Turbines (AREA)
  • Cereal-Derived Products (AREA)
  • Manufacturing And Processing Devices For Dough (AREA)
  • Supplying Of Containers To The Packaging Station (AREA)

Abstract

Ala (14) de un vehículo del tipo que se desplaza por un uido determinado, poseyendo el ala (14) un borde delantero dispuesto en la parte delantera y un borde posterior (22) dispuesto en la parte posterior, de manera que una parte del borde posterior (22) está recortada formando un rebaje y en el que un dispositivo (10) de alerón con rotor, que comprende un rotor motorizado (18) rotativo alrededor de un eje de rotación (32) a efectos de generar una fuerza de empuje (34), queda montado en el rebaje, caracterizándose porque: el rotor (18) está montado mediante dispositivos de acoplamiento (20, 28) que permiten que el eje de rotación (32) del rotor (18) pueda pivotar alrededor de un eje longitudinal (26) que se extiende a lo largo de las alas (14), de manera tal que por la rotación del rotor (18) y en todas las orientaciones de pivotamiento del eje de rotación (32) entre 0º y 180º con exclusión relativa a un plano cordal (36) del ala (14), las puntas (37) del rotor (18) cuando se encuentran ensu posición más adelantada pasan a través del volumen espacial definido como volumen que idealmente estaría ocupado por la parte correspondiente al borde posterior del ala (14) que ha sido recortado para conseguir el rebaje.
ES92912183T 1991-04-09 1992-04-09 Dispositivo de aleron con rotor y metodo correspondiente. Expired - Lifetime ES2144416T3 (es)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US07/683,596 US5195702A (en) 1991-04-09 1991-04-09 Rotor flap apparatus and method

Publications (1)

Publication Number Publication Date
ES2144416T3 true ES2144416T3 (es) 2000-06-16

Family

ID=24744710

Family Applications (1)

Application Number Title Priority Date Filing Date
ES92912183T Expired - Lifetime ES2144416T3 (es) 1991-04-09 1992-04-09 Dispositivo de aleron con rotor y metodo correspondiente.

Country Status (8)

Country Link
US (1) US5195702A (es)
EP (1) EP0533915B1 (es)
AT (1) ATE186031T1 (es)
AU (1) AU656205B2 (es)
DE (1) DE69230207T2 (es)
DK (1) DK0533915T3 (es)
ES (1) ES2144416T3 (es)
WO (1) WO1992018383A1 (es)

Families Citing this family (22)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5803409A (en) * 1996-06-06 1998-09-08 Nielsen Engineering & Research, Inc. Method and apparatus for reducing the drag of flows over surfaces
AU753702B2 (en) 1999-11-08 2002-10-24 Automotive Safety Engineering Pty Ltd Safety bollard
US6732972B2 (en) * 2002-09-13 2004-05-11 Frank S. Malvestuto, Jr. High-lift, low-drag, stall-resistant airfoil
AU2003303967A1 (en) * 2003-12-29 2005-08-03 Frank S. Malvestuto Jr. High-lift, low-drag, stall-resistant airfoil
US7643865B2 (en) * 2004-06-30 2010-01-05 Given Imaging Ltd. Autonomous in-vivo device
KR101308348B1 (ko) * 2009-07-03 2013-09-17 자와하랄 네루 센터 포 어드밴스드 사이언티픽 리서치 날개-장착된 견인 프로펠러들/로터들에 의해 구동되는 비행체의 날개의 유도 또는 전체 항력을 감소시키는 최적의 날개 평면도들
GB2540169B (en) * 2015-07-08 2018-08-08 Ge Aviation Systems Llc Aircraft wing shaped to counter aerodynamic effects of propeller wake
WO2018066043A1 (ja) * 2016-10-03 2018-04-12 株式会社Ａｅｒｏｎｅｘｔ 配達用回転翼機
US10144503B1 (en) * 2018-02-22 2018-12-04 Kitty Hawk Corporation Fixed wing aircraft with trailing rotors
US11014652B1 (en) * 2018-05-03 2021-05-25 Ardura, Inc. Active lift control device and method
GB2581498B (en) * 2019-02-19 2021-03-17 Needwood Engineering Consulting Ltd Aircraft
US12570397B2 (en) * 2019-07-26 2026-03-10 Ubifly Technologies Private Limited Lift enhancement assembly of an aerial vehicle with fixed wings
US10981648B2 (en) 2019-08-02 2021-04-20 Kitty Hawk Corporation Fixed wing aircraft with trailing rotors and T-tail
JP7342250B2 (ja) * 2019-10-09 2023-09-11 キティー・ホーク・コーポレーション 異なる飛行モードのためのハイブリット電力システム
US12043419B2 (en) 2020-02-27 2024-07-23 Liviu Giurca Aircraft with vertical take-off and landing—VTOL
US12227290B2 (en) 2020-10-27 2025-02-18 Wisk Aero Llc Power distribution circuits for electrically powered aircraft
US12444938B2 (en) 2020-10-27 2025-10-14 Wisk Aero Llc Power distribution circuits for electrically powered aircraft
ES1269111Y (es) * 2021-04-18 2021-09-17 Alexandre Emilio Martin Dispositivo aeronautico de propulsion en flap con motor de helice
EP4310003A3 (en) * 2022-03-28 2024-03-13 Lilium eAircraft GmbH Propulsion assembly of an aerial vehicle, method of controlling an orientation and/or position of a propulsion unit of an aerial vehicle, and aerial vehicle
WO2023215632A1 (en) * 2022-05-06 2023-11-09 Rensselaer Polytechnic Institute Aircraft lift enhancement system
US11655024B1 (en) 2022-05-25 2023-05-23 Kitty Hawk Corporation Battery systems with power optimized energy source and energy storage optimized source
ES1302354Y (es) 2023-01-03 2023-10-19 Jin Pengliang Dispositivo de ayuda al despegue y/o aterrizaje de aeronaves

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2873710A (en) * 1956-03-06 1959-02-17 Stanley L Morel Submarine attitude control system
US2976077A (en) * 1957-01-17 1961-03-21 Jr John Mosley Totton Vehicle stabilizing means
US3179352A (en) * 1959-09-21 1965-04-20 Hiller Aircraft Company Inc Tilt wing aircraft
US3117746A (en) * 1961-03-06 1964-01-14 Products Design Inc Lift-propulsion device for aircraft
US3115317A (en) * 1961-03-09 1963-12-24 Hawker Siddeley Aviation Ltd Aircraft wing and tiltable ducted fan
US3179354A (en) * 1962-04-24 1965-04-20 Alvarez-Calderon Alberto Convertiplane and apparatus thereof
US3203649A (en) * 1963-12-23 1965-08-31 Ryan Aeronautical Co Rotor flap high lift system
US3273827A (en) * 1964-04-27 1966-09-20 Ryan Aeronautical Co Propeller-rotor high lift system for aircraft
USRE29023E (en) * 1965-10-22 1976-11-02 Means and method of rotor augmented lift for airplanes
US3512825A (en) * 1968-06-11 1970-05-19 Robert D Green Aerodynamic wing for racing cars
US3521589A (en) * 1969-02-19 1970-07-21 Frederick O Kemp Underwater vessel
US3856238A (en) * 1972-04-14 1974-12-24 F Malvestuto Aircraft transporter
US3965836A (en) * 1972-04-14 1976-06-29 Malvestuto Jr Frank S High speed water vessel

Also Published As

Publication number Publication date
DE69230207T2 (de) 2000-05-31
EP0533915A4 (en) 1993-08-04
DK0533915T3 (da) 2000-04-25
AU656205B2 (en) 1995-01-27
WO1992018383A1 (en) 1992-10-29
US5195702A (en) 1993-03-23
AU2014692A (en) 1992-11-17
ATE186031T1 (de) 1999-11-15
EP0533915B1 (en) 1999-10-27
DE69230207D1 (de) 1999-12-02
EP0533915A1 (en) 1993-03-31

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