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WO2011056082A3 - Aircraft - Google Patents

Aircraft Download PDF

Info

Publication number
WO2011056082A3
WO2011056082A3 PCT/PL2010/000110 PL2010000110W WO2011056082A3 WO 2011056082 A3 WO2011056082 A3 WO 2011056082A3 PL 2010000110 W PL2010000110 W PL 2010000110W WO 2011056082 A3 WO2011056082 A3 WO 2011056082A3
Authority
WO
WIPO (PCT)
Prior art keywords
aircraft
axis
control
rotation
control surface
Prior art date
Application number
PCT/PL2010/000110
Other languages
French (fr)
Other versions
WO2011056082A2 (en
Inventor
Edward MARGAŃSKI
Original Assignee
Marganski Edward
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 Marganski Edward filed Critical Marganski Edward
Priority to EP10788157A priority Critical patent/EP2499042A2/en
Publication of WO2011056082A2 publication Critical patent/WO2011056082A2/en
Publication of WO2011056082A3 publication Critical patent/WO2011056082A3/en

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/04—Noseplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/10—Adjustable control surfaces or members, e.g. rudders one surface adjusted by movement of another, e.g. servo tabs

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Control Of Position, Course, Altitude, Or Attitude Of Moving Bodies (AREA)
  • Toys (AREA)

Abstract

The object of the invention is an aircraft provided with a device for creating a constant moment in relation to the axis of rotation of an additional control surface placed at the front of the aircraft at an as large as possible distance from the centre of gravity of the aircraft. The aircraft is characterised in that the control of the aerodynamic vertical force (7) is effected by deflecting control elements (3) pivotably mounted on the rotation axis (4), the deflection of said control elements causing rotation of a balance and control surface (1) mounted rotatably on axis (2), wherein the axis (2) is mounted perpendicularly to the plane of symmetry (5) of aircraft (6) forward of the resultant aerodynamic vertical force (7) generated by the balance and control surface (1).
PCT/PL2010/000110 2009-11-09 2010-11-05 Aircraft WO2011056082A2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
EP10788157A EP2499042A2 (en) 2009-11-09 2010-11-05 Aircraft

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
PLP.389502 2009-11-09
PL389502A PL389502A1 (en) 2009-11-09 2009-11-09 Aircraft

Publications (2)

Publication Number Publication Date
WO2011056082A2 WO2011056082A2 (en) 2011-05-12
WO2011056082A3 true WO2011056082A3 (en) 2011-08-25

Family

ID=43970605

Family Applications (1)

Application Number Title Priority Date Filing Date
PCT/PL2010/000110 WO2011056082A2 (en) 2009-11-09 2010-11-05 Aircraft

Country Status (3)

Country Link
EP (1) EP2499042A2 (en)
PL (1) PL389502A1 (en)
WO (1) WO2011056082A2 (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US7767121B2 (en) 2008-11-10 2010-08-03 Kryron Global, Llc Solid composition having enhanced physical and electrical properties
PL414124A1 (en) * 2015-09-23 2017-03-27 Edward Margański Vertical takeoff and landing aircraft

Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR943005A (en) * 1942-03-27 1949-02-24 Miles Aircraft Ltd Improvements to aircraft
US2747816A (en) * 1950-05-11 1956-05-29 Ben O Howard Canard type airplane and controls therefor
EP0680877A1 (en) * 1994-05-03 1995-11-08 AEROSPATIALE Société Nationale Industrielle Transport aircraft with forward mounted stabilizer
US20040140394A1 (en) * 2002-10-21 2004-07-22 Bath David L. Method and apparatus for installing and actuating movable airfoils, including canards

Family Cites Families (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
PL201911A1 (en) 1977-11-03 1979-07-02 Wytwornia Sprzetu Komunikacyjn AIR TEMPERATURE REGULATOR

Patent Citations (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR943005A (en) * 1942-03-27 1949-02-24 Miles Aircraft Ltd Improvements to aircraft
US2747816A (en) * 1950-05-11 1956-05-29 Ben O Howard Canard type airplane and controls therefor
EP0680877A1 (en) * 1994-05-03 1995-11-08 AEROSPATIALE Société Nationale Industrielle Transport aircraft with forward mounted stabilizer
US20040140394A1 (en) * 2002-10-21 2004-07-22 Bath David L. Method and apparatus for installing and actuating movable airfoils, including canards

Also Published As

Publication number Publication date
PL389502A1 (en) 2011-05-23
EP2499042A2 (en) 2012-09-19
WO2011056082A2 (en) 2011-05-12

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