EP 2499042 A2 20120919 - AIRCRAFT
Title (en)
AIRCRAFT
Title (de)
LUFTFAHRZEUG
Title (fr)
AÉRONEF
Publication
Application
Priority
- PL 38950209 A 20091109
- PL 2010000110 W 20101105
Abstract (en)
[origin: WO2011056082A2] 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).
IPC 8 full level
B64C 5/04 (2006.01)
CPC (source: EP)
B64C 5/04 (2013.01); B64C 9/10 (2013.01); B64C 39/12 (2013.01)
Citation (search report)
See references of WO 2011056082A2
Designated contracting state (EPC)
AL AT BE BG CH CY CZ DE DK EE ES FI FR GB GR HR HU IE IS IT LI LT LU LV MC MK MT NL NO PL PT RO RS SE SI SK SM TR
DOCDB simple family (publication)
WO 2011056082 A2 20110512; WO 2011056082 A3 20110825; EP 2499042 A2 20120919; PL 389502 A1 20110523
DOCDB simple family (application)
PL 2010000110 W 20101105; EP 10788157 A 20101105; PL 38950209 A 20091109