IL130116A0 - STOL/VTOL aircraft with improved control during transition - Google Patents

STOL/VTOL aircraft with improved control during transition

Info

Publication number
IL130116A0
IL130116A0 IL13011697A IL13011697A IL130116A0 IL 130116 A0 IL130116 A0 IL 130116A0 IL 13011697 A IL13011697 A IL 13011697A IL 13011697 A IL13011697 A IL 13011697A IL 130116 A0 IL130116 A0 IL 130116A0
Authority
IL
Israel
Prior art keywords
stol
control during
improved control
during transition
vtol aircraft
Prior art date
Application number
IL13011697A
Original Assignee
Freewing Aerial Robotics Corp
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 Freewing Aerial Robotics Corp filed Critical Freewing Aerial Robotics Corp
Publication of IL130116A0 publication Critical patent/IL130116A0/en

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
    • B64C29/0033—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 tiltable relative to the fuselage

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Toys (AREA)
IL13011697A 1996-11-26 1997-11-25 STOL/VTOL aircraft with improved control during transition IL130116A0 (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US75582296A 1996-11-26 1996-11-26
PCT/US1997/021660 WO1998023482A1 (en) 1996-11-26 1997-11-25 Stol/vtol aircraft with improved control during transition

Publications (1)

Publication Number Publication Date
IL130116A0 true IL130116A0 (en) 2000-06-01

Family

ID=25040792

Family Applications (1)

Application Number Title Priority Date Filing Date
IL13011697A IL130116A0 (en) 1996-11-26 1997-11-25 STOL/VTOL aircraft with improved control during transition

Country Status (3)

Country Link
AU (1) AU5589598A (en)
IL (1) IL130116A0 (en)
WO (1) WO1998023482A1 (en)

Families Citing this family (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN106275389A (en) * 2016-10-19 2017-01-04 吴瑞霞 A kind of control aircraft pitch, the system turned on one's side, go off course
TWI643790B (en) * 2017-12-06 2018-12-11 林瑤章 Thrust vector controller
CN109131834A (en) * 2018-07-20 2019-01-04 中国空空导弹研究院 Wing formula aircraft
DE102018212611A1 (en) * 2018-07-27 2020-01-30 SilentWings GmbH Aircraft and method for operating an aircraft

Family Cites Families (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1726558A (en) * 1926-12-31 1929-09-03 Randolph F Hall Airplane
US2750133A (en) * 1951-03-28 1956-06-12 Lockheed Aircraft Corp Alighting gear for vertically arising aircraft
EP0070578B1 (en) * 1979-05-01 1989-02-01 Brooklands Aerospace Group Plc Ducted propeller
US5340057A (en) * 1991-11-20 1994-08-23 Freewing Aerial Robotics Corporation Thrust vectoring free wing aircraft
US5395073A (en) * 1992-03-13 1995-03-07 Freewing Aerial Robotics Corporation STOL/VTOL free wing aircraft with articulated tail boom

Also Published As

Publication number Publication date
AU5589598A (en) 1998-06-22
WO1998023482A1 (en) 1998-06-04

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