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Patent Searching and Data


Matches 101 - 150 out of 905

Document Document Title
WO/2007/100601A3
A door pod assembly includes a housing that defines a cavity for emergency equipment, a pod door, and a latch retaining the pod door in a closed position relative to the housing. The assembly is configured such that the latches, upon act...  
WO/2007/100601A2
A door pod assembly includes a housing that defines a cavity for emergency equipment, a pod door, and a latch retaining the pod door in a closed position relative to the housing. The assembly is configured such that the latches, upon act...  
WO/2007/099022A1
The present invention describes a method and an apparatus for preventing damage to an apparatus resulting from the consequences of a free fall. In this case, first of all, a free fall of the apparatus is identified and a measure is then ...  
WO/2007/096689A1
Emergency system of Airplane parachute with cusion means if air plane needs make a stop on the way or need . temporary Landing on the way, This system work for Airplane can landing at Emergency on flying tinm. This parachute system are b...  
WO/2007/089231A1
A novel parachute design is presented that is distinguished by having trapezoidal gores, producing a parachute having a unique shape, which can be, selectively, either ballistic or gliding and steerable, in addition to having a selective...  
WO/2007/086055A1
The invention provides a system, method and landing device for landing an aircraft (50) with respect to a predetermined landing location (P). The aircraft is configured for powered flight at least when the parafoil (60) is deployed, and ...  
WO/2007/076725A1
A parachute-landing device of aircraft is provided. The device includes at least a parachute compartment (4) in aircraft (1). A parachute (2) with a pilot parachute (3) is contained within the compartment. The compartment (4) has a cover...  
WO/2007/066895A1
The present invention relates to a vertical landing device for a radio control multi-purpose aircraft having a body part and a wing part, wherein the vertical landing device has a chute having at least one pair of high- flexible guide co...  
WO/2007/038863A3
The present invention relates to a heavy payload parachute ground disconnecting device. The device comprises an actuator (102) for keeping a holding mechanism (128) in a locked position during a predetermined time interval and after elap...  
WO/2007/038863A2
The present invention relates to a heavy payload parachute ground disconnecting device. The device comprises an actuator (102) for keeping a holding mechanism (128) in a locked position during a predetermined time interval and after elap...  
WO/2007/034468A1
The disclosure provides a parachute release device which may include a connecting element capable of connecting to an aircraft and to a parachute and a locking mechanism capable of releasing the connecting element from the aircraft upon ...  
WO/2007/004018A1
The invention relates to a parachute of which the canopy is configured in its deployed/inflated configuration to define an inner/upper segment (20) equivalent to that of a round inflated canopy and an outer/lower segment (22) equivalent ...  
WO/2006/137909A3
An illustrative embodiment of the invention includes an apparatus and method for making air and space inflatables and deployables using three dimensionally reinforced (3DR) membranes. A 3DR process preferably takes plural substantially f...  
WO/2006/137909A2
An illustrative embodiment of the invention includes an apparatus and method for making air and space inflatables and deployables using three dimensionally reinforced (3DR) membranes. A 3DR process preferably takes plural substantially f...  
WO/2006/135870A3
A parachute package including a harness, a reserve parachute container attached to the harness, a main parachute container releasably secured to the harness, and means for releasably fastening together the main and reserve parachute cont...  
WO/2006/135870A2
A parachute package including a harness, a reserve parachute container attached to the harness, a main parachute container releasably secured to the harness, and means for releasably fastening together the main and reserve parachute cont...  
WO2006063198B1
A parachute webbing severing system and method (10) includes a heater (12), such as a nichrome wire, an etched foil heater, and a resistance heater or the like, disposed proximate the webbing (14). Upon activation, the heater (12) heats ...  
WO2006063198A8
A parachute webbing severing system and method (10) includes a heater (12), such as a nichrome wire, an etched foil heater, and a resistance heater or the like, disposed proximate the webbing (14). Upon activation, the heater (12) heats ...  
WO/2006/098787A2
The present invention features a parachute retraction mechanism 10 including a tether 24 is connected to a winch 30 and a parachute 12. The winch 30 retracts the parachute 12 into a cavity 20 where the parachute 12 is either be stored or...  
WO/2006/098787A3
The present invention features a parachute retraction mechanism 10 including a tether 24 is connected to a winch 30 and a parachute 12. The winch 30 retracts the parachute 12 into a cavity 20 where the parachute 12 is either be stored or...  
WO2004080797A3
A parachute is adapted for deployment at low altitudes and low air speeds, such as for use in emergency evacuations from buildings. A canopy of the parachute includes a conical portion with a top polar opening. The canopy also includes a...  
WO2006063198A3
A parachute webbing severing system and method (10) includes a heater (12), such as a nichrome wire, an etched foil heater, and a resistance heater or the like, disposed proximate the webbing (14). Upon activation, the heater (12) heats ...  
WO/2006/077315A1
The invention relates to a multi-purpose aircraft comprising, on the one hand, at least one cockpit (1) equipped with at least one motor-driven propeller (3) capable of ensuring the displacement of this aircraft through the air and, on t...  
WO/2006/065406A2
A release device, and in particular a release device for use in parachute systems in place of pyrotechnic cutters. The inventive systems utilize a severable structural member of low melting point, high strength polymer that is severed by...  
WO/2006/065406A3
A release device, and in particular a release device for use in parachute systems in place of pyrotechnic cutters. The inventive systems utilize a severable structural member of low melting point, high strength polymer that is severed by...  
WO/2006/063198A2
A parachute webbing severing system and method (10) includes a heater (12), such as a nichrome wire, an etched foil heater, and a resistance heater or the like, disposed proximate the webbing (14). Upon activation, the heater (12) heats ...  
WO/2006/053196A2
A fastening system particularly suited for removably securing a first component of a parachute system to a second component. The fastening system includes a first and at least a second magnetic element secured to the first and second com...  
WO/2006/053196A3
A fastening system particularly suited for removably securing a first component of a parachute system to a second component. The fastening system includes a first and at least a second magnetic element secured to the first and second com...  
WO/2006/011236A1
In order to reduce the deaths in a falling accident of parachute, frames for fixing hooks of moderate size are attached, along with hooks, to the front and rear of a person equipped with a parachute. Furthermore, weight is reduced by mak...  
WO2005039972A3
A vehicle including a fuselage having a longitudinal axis and a transverse axis, two Ducted Fan lift-producing propellers carried by the fuselage on each side of the transverse axis, a pilot's compartment formed in the fuselage between t...  
WO2005102837A3
This invention relates to a parachute supported aircraft having a frame and a seat for supporting at least a pilot. A parachute is coupled to the frame by a plurality of riser lines for allowing the parachute to inflate and form a wing f...  
WO/2005/120947A1
The invention relates to a device for releasing under load that is primarily comprised of a self-tightening mesh (3) placed around a mandrel (2), characterized in that a pulling force (F) exerted upon an end (1) and the mandrel (2) posit...  
WO/2005/112572A3
An adaptive guidance system (AGS) regulates the altitude and heading of a parasail to arrive at a target at a prescribed altitude. Since the altitude profile depends both on unknown wing loading, and wind magnitude and direction, the AGS...  
WO/2005/102837A2
This invention relates to a parachute supported aircraft having a frame and a seat for supporting at least a pilot. A parachute is coupled to the frame by a plurality of riser lines for allowing the parachute to inflate and form a wing f...  
WO2005012086A3
A rescue parachute device and method, which fully deploys the canopy (20) of the parachute prior to the jump and maintains it in the proper position. The device comprises: an inflatable canopy with inflation sleeves, housed in an initial...  
WO/2005/058698A1
A towing winch apparatus for paragliders and hang-gliders (4,6) is provided which comprises a line (3) and a towing winch mechanism (5) adapted to apply tension to said line (3) during towing, where one end (15) of the line (3) is releas...  
WO/2005/039972A2
A vehicle including a fuselage having a longitudinal axis and a transverse axis, two Ducted Fan lift-producing propellers carried by the fuselage on each side of the transverse axis, a pilot's compartment formed in the fuselage between t...  
WO2003089298A3
The invention concerns a bag for a parachute with at least one canopy (2) which is connected to a harness via lines (3), whereby this bag (1) has at least one fastening element (4, 5, 16, 17, 21, 22, 23, 24) so as to form a whole compris...  
WO/2005/012087A1
The invention concerns a machine (1) which receives a parachute in semi-bulk state after a jump and performs a primary check, verifies its condition and inserts it in a cloth bag wherein it is packaged for another jump. Said machine comp...  
WO/2005/012086A2
A rescue parachute device and method, which fully deploys the canopy (20) of the parachute prior to the jump and maintains it in the proper position. The device comprises: an inflatable canopy with inflation sleeves, housed in an initial...  
WO/2005/002964A1
A parachute (10) is formed using a non-woven composite material. The non-woven composite material (100) is formed by fusing a plurality of mono-filament fibers between thin layers of plastic (126,128). The non-woven material may be used ...  
WO/2005/000678A1
A device, system and method of reserve parachute deployment comprised of a body (18) with a top and bottom end (16, 18), a hook-slot (5) and releasable means of attachment in communication with the hook-slot (5). The system and method di...  
WO/2005/000677A1
A parachute is formed from a non-woven composite material (30). The non-woven composite material (30) is formed by fusing a plurality of mono-filament fibers between thin layers of plastic (40,42). The fibers (38) are positioned in direc...  
WO/2004/082765A1
An escape parachute for emergency includes a capsule having an air filling area therein and forming a user receiving space when being filled with air and expanded, a canopy having an air filling area therein and expanded by air to spread...  
WO/2004/080797A2
A parachute is adapted for deployment at low altitudes and low air speeds, such as for use in emergency evacuations from buildings. A canopy of the parachute includes a conical portion with a top polar opening. The canopy also includes a...  
WO/2004/063688A3
A low force release mechanism suitable for use in applications including but not limited to pinatas and dispersion devices comprising an interactive distribution of the load force to the main structure and the structure of a trap employe...  
WO2003099655A3
A hydraulic mechanism is positioned within the drogue bridle of a parachute system (10). The hydraulic link is slowly moved by tension on the drogue bridle to operate a release. The release operates to release the drogue chute (20) and t...  
WO2004018288A3
A parachute riser system (10) for decreasing the velocity of a payload (16) attached to a parachute (14) is provided. The parachute riser system (10) comprises a pressure vessel (12) mounted between the payload (16) and the parachute (14...  
WO/2004/043784A1
A protection system for aircraft comprises two parachutes (1,2) mounted to the upper part of the aircraft body. A third parachute (3) is mounted at the tail of the aircraft. The lower part of the aircraft comprises containers (4,5) holdi...  
WO2003100261A3
An automated quick release mechanism (10) for a three ring release (40) includes a pneumatic or hydraulic cylinder (20) with a hardened metal pin (21). The pin (21) engages a string loop of the three ring release (40). An internal spring...  

Matches 101 - 150 out of 905