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WO2000047470A3 - Systeme de transport aerien personnel sans ailes - Google Patents

Systeme de transport aerien personnel sans ailes Download PDF

Info

Publication number
WO2000047470A3
WO2000047470A3 PCT/US2000/002456 US0002456W WO0047470A3 WO 2000047470 A3 WO2000047470 A3 WO 2000047470A3 US 0002456 W US0002456 W US 0002456W WO 0047470 A3 WO0047470 A3 WO 0047470A3
Authority
WO
WIPO (PCT)
Prior art keywords
diameter
platform
inner platform
downward
wingless
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.)
Ceased
Application number
PCT/US2000/002456
Other languages
English (en)
Other versions
WO2000047470B1 (fr
WO2000047470A2 (fr
Inventor
Karl F Milde 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
Priority claimed from US09/352,522 external-priority patent/US6179247B1/en
Application filed by Individual filed Critical Individual
Priority to AU46398/00A priority Critical patent/AU4639800A/en
Publication of WO2000047470A2 publication Critical patent/WO2000047470A2/fr
Publication of WO2000047470A3 publication Critical patent/WO2000047470A3/fr
Publication of WO2000047470B1 publication Critical patent/WO2000047470B1/fr
Anticipated expiration legal-status Critical
Ceased legal-status Critical Current

Links

Classifications

    • 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
    • B64C29/0016—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 free or ducted propellers or by blowers
    • B64C29/0025—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 free or ducted propellers or by blowers the propellers being fixed relative to the fuselage
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Emergency Lowering Means (AREA)
  • Toys (AREA)

Abstract

L'invention concerne un système de transport aérien sans ailes comprenant deux parties principales. Premièrement, une plate-forme interne circulaire sensiblement horizontale dont l'extrémité externe a un premier diamètre (D1), laquelle comporte un siège accueillant au moins une personne et un carénage formant une surface supérieure lisse qui s'étend vers l'extérieur et vers le bas jusqu'à l'extrémité externe. Deuxièmement, une plate-forme externe annulaire sensiblement horizontale coaxiale par rapport à la plate-forme interne, laquelle a une ouverture centrale de second diamètre (D2) et un carénage formant une surface supérieure sensiblement lisse qui s'étend vers l'intérieur et vers le bas dans l'ouverture centrale. Le second diamètre (D2) est supérieur au premier diamètre (D1). De préférence, au moins cinq propulseurs sont disposés dans l'espace compris entre les plates-formes interne et externe pour fournir une poussée d'air vers le bas. De préférence également, une bulle hémisphérique en plastique transparent est placée sur le haut de la plate-forme interne pour protéger les passagers et assurer un écoulement fluide de l'air.
PCT/US2000/002456 1999-02-09 2000-02-01 Systeme de transport aerien personnel sans ailes Ceased WO2000047470A2 (fr)

Priority Applications (1)

Application Number Priority Date Filing Date Title
AU46398/00A AU4639800A (en) 1999-02-09 2000-02-01 Wingless, personal air transport

Applications Claiming Priority (8)

Application Number Priority Date Filing Date Title
US24716399A 1999-02-09 1999-02-09
US09/247,163 1999-02-09
US10309399A 1999-04-08 1999-04-08
US29/103,093 1999-04-08
US09/352,522 1999-07-13
US09/352,522 US6179247B1 (en) 1999-02-09 1999-07-13 Personal air transport
US11525599A 1999-12-09 1999-12-09
US29/115,255 1999-12-09

Publications (3)

Publication Number Publication Date
WO2000047470A2 WO2000047470A2 (fr) 2000-08-17
WO2000047470A3 true WO2000047470A3 (fr) 2000-12-14
WO2000047470B1 WO2000047470B1 (fr) 2001-01-18

Family

ID=27493318

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/US2000/002456 Ceased WO2000047470A2 (fr) 1999-02-09 2000-02-01 Systeme de transport aerien personnel sans ailes

Country Status (2)

Country Link
AU (1) AU4639800A (fr)
WO (1) WO2000047470A2 (fr)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB0911667D0 (en) * 2009-07-06 2009-08-12 Aesir Ltd Improvements to controlling spin of an aircraft
US11541999B2 (en) 2021-06-01 2023-01-03 Hoversurf, Inc. Methods of vertical take-off/landing and horizontal straight flight of aircraft and aircraft for implementation
US11383831B1 (en) * 2021-06-01 2022-07-12 Hoversurf, Inc. Methods of vertical take-off/landing and horizontal straight flight of aircraft and aircraft for implementation
US11377220B1 (en) 2021-09-27 2022-07-05 Hoversurf, Inc. Methods of increasing flight safety, controllability and maneuverability of aircraft and aircraft for implementation thereof

Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2282612A (en) * 1941-09-25 1942-05-12 Kermath Mfg Company Marine power transmission system
US3082977A (en) * 1960-07-06 1963-03-26 Arlin Max Melvin Plural rotor sustained aircraft
US3614030A (en) * 1969-12-10 1971-10-19 Paul S Moller Aircraft
US3640489A (en) * 1968-07-26 1972-02-08 Karl Jaeger Vertical takeoff and landing aircraft
US3933325A (en) * 1973-09-25 1976-01-20 Kaelin J R Disc-shaped aerospacecraft
US4457476A (en) * 1981-11-20 1984-07-03 Frank Andresevitz Wingless aircraft
US5239830A (en) * 1992-03-05 1993-08-31 Avco Corporation Plural engine power producing system

Patent Citations (7)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2282612A (en) * 1941-09-25 1942-05-12 Kermath Mfg Company Marine power transmission system
US3082977A (en) * 1960-07-06 1963-03-26 Arlin Max Melvin Plural rotor sustained aircraft
US3640489A (en) * 1968-07-26 1972-02-08 Karl Jaeger Vertical takeoff and landing aircraft
US3614030A (en) * 1969-12-10 1971-10-19 Paul S Moller Aircraft
US3933325A (en) * 1973-09-25 1976-01-20 Kaelin J R Disc-shaped aerospacecraft
US4457476A (en) * 1981-11-20 1984-07-03 Frank Andresevitz Wingless aircraft
US5239830A (en) * 1992-03-05 1993-08-31 Avco Corporation Plural engine power producing system

Also Published As

Publication number Publication date
AU4639800A (en) 2000-08-29
WO2000047470B1 (fr) 2001-01-18
WO2000047470A2 (fr) 2000-08-17

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