Patent application number | Description | Published |
20110049295 | REUSABLE ROTORCRAFT BUMPER, AND A ROTORCRAFT HAVING SUCH A BUMPER - A reusable bumper ( | 03-03-2011 |
20110127377 | TAIL SKID FOR PROTECTING A STRUCTURAL ELEMENT OF AN AIRCRAFT, AN AIRCRAFT PROVIDED WITH SUCH A TAIL SKID, AND AN ANTI-OVERTURNING METHOD IMPLEMENTED BY SAID TAIL SKID - The present invention relates to a tail skid ( | 06-02-2011 |
20110155848 | AIRCRAFT UNDERCARRIAGE HAVING A ROCKER LEVER WITH A SWIVEL AND A HINGED TWIN WHEELS - The invention relates to an aircraft undercarriage ( | 06-30-2011 |
20110204182 | ROTARY WING AIRCRAFT PROVIDED WITH AN EMERGENCY UNDERCARRIAGE - A rotary wing aircraft ( | 08-25-2011 |
20110260001 | LANDING GEAR PROVIDED WITH ENERGY ABSORBER MEANS, AN AIRCRAFT PROVIDED WITH SAID LANDING GEAR, AND A METHOD OF LANDING - Aircraft landing gear ( | 10-27-2011 |
20120006934 | METHOD AND A ROTARY WING AIRCRAFT THAT ARE OPTIMIZED SO AS TO MINIMIZE THE CONSEQUENCES FOR THE OCCUPANTS OF SAID AIRCRAFT OF AN OFF-SPECIFICATION EMERGENCY LANDING - A method of minimizing the consequences for the occupants of a rotary wing aircraft ( | 01-12-2012 |
20120043420 | SKID UNDERCARRIAGE AND A METHOD OF PREVENTING A ROTORCRAFT PROVIDED WITH SUCH AN UNDERCARRIAGE FROM TILTING - An undercarriage ( | 02-23-2012 |
20120221235 | METHOD OF OPTIMIZING THE LOADING OF LOADS IN A VEHICLE - A method of determining the locations of loads in a vehicle in such a manner as to ensure mission safety in terms of loads being retained in the aircraft. On the basis of vehicle parameters, the anchor points available in this type of vehicle for retaining the loads are identified. As a function of the available loading volume(s), a possible loading configuration is calculated using at least some of the available anchor points, at least some of the retaining means, and the characteristics of the loads. The forces that might be exerted on the selected anchor points are verified as being less than maximum limits. The calculated loading configuration is confirmed, otherwise a new loading configuration is calculated. | 08-30-2012 |
20130078049 | SURFACE-AREA SAFETY MEANS AND A VEHICLE - Surface-area safety means ( | 03-28-2013 |
20130146706 | METHOD AND A ROTARY WING AIRCRAFT OPTIMIZED FOR MINIMIZING THE CONSEQUENCES OF A RUNNING OFF-SPECIFICATION EMERGENCY LANDING - A method of minimizing the consequences of an off-specification landing for the occupants of an aircraft ( | 06-13-2013 |
20140084109 | LANDING GEAR PROVIDED WITH A STIFFENER FOR INCREASING ITS STIFFNESS IN ROLL, AND AN AIRCRAFT - Aircraft landing gear ( | 03-27-2014 |
20140252169 | SYSTEM FOR FASTENING A LOAD TO A ROTORCRAFT, AND A ROTORCRAFT - A fastener system ( | 09-11-2014 |
20140252170 | DEVICE FOR PROTECTING A ROTORCRAFT AGAINST A PYRAMID-SHAPED STRUCTURE FOR CARRYING A LOAD - A protection device ( | 09-11-2014 |
20140353419 | ROTARY WING ROTORCRAFT HAVING A PLURALITY OF PROPELLERS - A hybrid aircraft ( | 12-04-2014 |
20140353420 | ROTARY WING ROTORCRAFT HAVING A PLURALITY OF PROPELLERS - A hybrid aircraft ( | 12-04-2014 |
20150014485 | SUSPENSION SYSTEM FOR CARRYING AN EXTERNAL LOAD WITH AN AIRCRAFT, AND AN AIRCRAFT - A suspension system ( | 01-15-2015 |