DE60232509D1 - Insbesondere als senkrechtstarter geeignete mantelgebläsefahrzeuge - Google Patents

Insbesondere als senkrechtstarter geeignete mantelgebläsefahrzeuge

Info

Publication number
DE60232509D1
DE60232509D1 DE60232509T DE60232509T DE60232509D1 DE 60232509 D1 DE60232509 D1 DE 60232509D1 DE 60232509 T DE60232509 T DE 60232509T DE 60232509 T DE60232509 T DE 60232509T DE 60232509 D1 DE60232509 D1 DE 60232509D1
Authority
DE
Germany
Prior art keywords
duct
vehicle
longitudinal axis
vehicles
particularly suitable
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
DE60232509T
Other languages
English (en)
Inventor
Rafi Yoeli
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.)
Urban Aeronautics Ltd
Original Assignee
Romeo Yankee 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 Romeo Yankee Ltd filed Critical Romeo Yankee Ltd
Application granted granted Critical
Publication of DE60232509D1 publication Critical patent/DE60232509D1/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C29/00Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0016Aircraft 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
    • B64C29/0025Aircraft 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
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64CAEROPLANES; HELICOPTERS
    • B64C27/00Rotorcraft; Rotors peculiar thereto
    • B64C27/20Rotorcraft characterised by having shrouded rotors, e.g. flying platforms

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Mechanical Engineering (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Polyethers (AREA)
  • Holo Graphy (AREA)
  • Paints Or Removers (AREA)
  • Vehicle Body Suspensions (AREA)
  • Body Structure For Vehicles (AREA)
  • Treatment Of Sludge (AREA)
  • Braking Systems And Boosters (AREA)
  • Sewage (AREA)
DE60232509T 2001-05-29 2002-05-28 Insbesondere als senkrechtstarter geeignete mantelgebläsefahrzeuge Expired - Lifetime DE60232509D1 (de)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US09/865,678 US6464166B1 (en) 2001-05-29 2001-05-29 Ducted fan vehicles particularly useful as VTOL aircraft
PCT/IL2002/000417 WO2002096750A2 (en) 2001-05-29 2002-05-28 Ducted fan vehicles particularly useful as vtol aircraft

Publications (1)

Publication Number Publication Date
DE60232509D1 true DE60232509D1 (de) 2009-07-16

Family

ID=25346013

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60232509T Expired - Lifetime DE60232509D1 (de) 2001-05-29 2002-05-28 Insbesondere als senkrechtstarter geeignete mantelgebläsefahrzeuge

Country Status (10)

Country Link
US (3) US6464166B1 (de)
EP (2) EP2070815B1 (de)
JP (1) JP2004526630A (de)
AT (2) ATE553997T1 (de)
AU (1) AU2002309217A1 (de)
CA (1) CA2448679C (de)
DE (1) DE60232509D1 (de)
IL (1) IL159106A0 (de)
SG (1) SG162608A1 (de)
WO (1) WO2002096750A2 (de)

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EP1390259A2 (de) 2004-02-25
SG162608A1 (en) 2010-07-29
ATE553997T1 (de) 2012-05-15
EP2070815A3 (de) 2009-06-24
US20090140102A1 (en) 2009-06-04
AU2002309217A1 (en) 2002-12-09
US7918416B2 (en) 2011-04-05
US20040149857A1 (en) 2004-08-05
ATE432871T1 (de) 2009-06-15
WO2002096750B1 (en) 2003-11-20
WO2002096750A2 (en) 2002-12-05
EP1390259A4 (de) 2005-11-02
EP1390259B1 (de) 2009-06-03
JP2004526630A (ja) 2004-09-02
EP2070815A2 (de) 2009-06-17
EP2070815B1 (de) 2012-04-18
CA2448679C (en) 2010-11-23
US6817570B2 (en) 2004-11-16
US6464166B1 (en) 2002-10-15
WO2002096750A3 (en) 2003-10-02
IL159106A0 (en) 2004-05-12
CA2448679A1 (en) 2002-12-05

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