Matches 1 - 25 out of 25


Match Document Document Title
US20120043420 SKID UNDERCARRIAGE AND A METHOD OF PREVENTING A ROTORCRAFT PROVIDED WITH SUCH AN UNDERCARRIAGE FROM TILTING  
An undercarriage (1) having a first skid (11) provided with a first longitudinal bearing portion (110) and a second skid (12) provided with a second longitudinal bearing portion (120), the first...
US20100243798 SKID RAIL FOR AIRCRAFTS AND ITS PRODUCTION METHOD  
A skid rail for aircrafts comprising (i) a base member comprising a long board fixed to a bottom surface of an aircraft fuselage, and bosses integrally projecting from an outer surface of the long...
US20150041588 Skid Stabilizer for Use With a Radio Controlled Helicopter  
A skid stabilizer for use with a radio controlled model helicopter is disclosed. The skid stabilizer comprises a pair of substantially longitudinal skid protectors disposed parallel to one another...
US20140224928 Helicopter Skid Landing Gear  
A cross tube for a helicopter skid landing gear, including a monolithic metallic tube having a central portion extending transversely between two end portions with longitudinal central axes of the...
US20140084109 LANDING GEAR PROVIDED WITH A STIFFENER FOR INCREASING ITS STIFFNESS IN ROLL, AND AN AIRCRAFT  
Aircraft landing gear (5) having a first skid (6) and a second skid (7), together with two cross-members, each having a first branch (16) secured to the first skid (6) and a second branch (17)...
US20090084895 Aircraft Skid Shoes with Wear-Resistant Cladding Layers  
Aircraft skid shoes are provided with wear-resistant cladding layers. Powders of hard particles and braze material are impregnated into at least one cloth which is applied to the wear surface of a...
US20070181744 Rotorcraft skid undercarriage and a rotorcraft including such an undercarriage  
The invention relates to a rotorcraft (21) comprising a fuselage (22) and an undercarriage (20) having skids (24, 25) interconnected by at least one cross-member (26, 27), together with connection...
US20070007387 Strut extender for landing gear snow skis  
A landing gear strut extender apparatus and its method of use adjust the length of a shock absorbing strut to facilitate the attachment of the strut between an aircraft landing gear and a snow...
US20130264419 LANDING GEAR VIBRATION ABSORBER AND METHOD OF OPERATING SAID LANDING GEAR VIBRATION ABSORBER  
A landing gear vibration absorber (1) of a helicopter (2) with a landing gear (3) comprising a pair of skids (4, 5) and at least one cross tube (6, 7) for mounting the skids (4, 5) to a...
US20150151836 SKID LANDING GEAR HAVING AT LEAST ONE CROSS-MEMBER WITH ROCKERS, AND AN AIRCRAFT  
The present invention relates to landing gear having a first skid, a second skid, a front cross-member, and a rear cross-member. The landing gear includes at least one stiffener arranged on a...
US20130248650 HELICOPTER SKID TYPE LANDING GEAR  
A helicopter with a fuselage and a skid-type landing gear mounted to said fuselage. Said landing gear comprises pivotable cross beams and skids, said skids being each disposed in an essentially...
US20130341461 Lightweight Helicopter Skid Shoes  
A lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material; and a structure coupling mechanism; wherein the body prevents friction-related...
US20100237190 Undercarriage with anticrash and antiresonance skids for a rotary wing aircraft, and an aircraft  
An undercarriage (2) having anticrash and antiresonance skids (6) for a rotary wing aircraft (1), the undercarriage including in particular: two landing skids (6) that are elastically deformable...
US20130146706 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 (1) having a rotary wing (10) and a fuselage (7) extending along a longitudinal...
US20120080560 SKID LANDING GEAR AND AN AIRCRAFT PROVIDED WITH SUCH LANDING GEAR  
A landing gear (3) provided with first and second longitudinal bearing skids (4, 5) and with first and second transverse crossbars (6, 7). The landing gear includes at least one resilient fastener...
US20130112810 SKID LANDING GEAR SYSTEM  
A skid landing gear assembly is provided. One embodiment of the landing gear assembly may include a first and a second skid member, and a forward and an aft cross member. The forward and aft...
US20110210201 Fiber-Reinforced, Composite, Structural Member Exhibiting Non-Linear Strain-to-Failure and Method of Making Same  
A fiber-reinforced, organic matrix, composite structural member includes a plurality of layers of fiber-reinforced, organic matrix, composite material in which adjacent layers are bonded to one...
US20170113789 AERIAL VEHICLE AND A SIGNAL LINE PROTECTION ASSEMBLY THEREOF  
A signal line protection assembly for an aerial vehicle includes a foot stand and a protection sleeve configured to receive a signal line. The foot stand includes a foot stand sleeve. At least a...
US20160280362 AIRCRAFT AND LANDING GEAR PROVIDED WITH AT LEAST ONE PAIR OF SHOCK ABSORBERS, AND A METHOD PERFORMED BY SAID LANDING GEAR  
Landing gear for an aircraft, the landing gear having at least one pair of shock absorbers comprising a first shock absorber and a second shock absorber, each shock absorber comprising a cylinder...
US20160244155 HELICOPTER SKID LANDING GEAR  
A landing gear for an aircraft can include a skid tube having an inboard flat side wall and an outboard flat side wall, the skid tube having a skid tube centerline plane that is parallel to at...
US20160167773 SKID LANDING GEAR HAVING AT LEAST ONE DAMPER, AND AN AIRCRAFT  
The invention relates to landing gear of an aircraft, the landing gear having skids and cross-members. The landing gear has at least one damper device arranged on at least one of the cross-members...
US20160144982 UAV DOCKING SYSTEM AND METHOD  
An aerial vehicle docking system includes a landing pad and an aerial vehicle. The landing pad has a concave landing surface and a depression. The aerial vehicle has landing gear and a protrusion....
US20160052625 IMPACT ABSORBER DEVICE, PARTICULARLY FOR AIRCRAFT  
An impact absorber device (10) of a fixed landing skid of an aircraft (1) is described. The device comprises a female element (20), a male element (30) and a core (40) arranged between said female...
US20150336661 LIGHTWEIGHT HELICOPTER SKID SHOES  
A lightweight skid shoe assembly comprises a body of wear resistant, non-metallic or partially metallic material; and a structure coupling mechanism; wherein the body prevents friction-related...
US20150329203 LINKING DAMPER SYSTEM FOR A ROTORCRAFT LANDING GEAR  
A linking system for attaching a cross tube to a skid of a landing gear of a rotorcraft, the linking system comprising a hinge element, means for connecting the hinge element to the cross tube and...

Matches 1 - 25 out of 25