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Patent Searching and Data


Matches 101 - 150 out of 923

Document Document Title
WO/2009/038586A1
A hybrid parachute, method of deploying a parachute and method of landing a payload. The hybrid parachute utilizes a reefing system that provides for the initial deployment of a deceleration stage that is configured to withstand the stre...  
WO2007096689B1
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/2008/093924A2
The present invention relates to a lifesaving parachute, for moving people in clanger to the ground safety in the case of accidents causing the loss of lives, such as fire of a high-storied building, earthquake and the like, which includ...  
WO/2008/092968A1
The recovery and rescue system includes a sail (5) with rigging (10) fitted around a spreader conduit (4), with an intake and outlet nozzle, wherein a starting system (6) is provided, including mechanical (12-13) and electromechanical (1...  
WO/2008/093924A3
The present invention relates to a lifesaving parachute, for moving people in clanger to the ground safety in the case of accidents causing the loss of lives, such as fire of a high-storied building, earthquake and the like, which includ...  
WO/2008/086602A1
The present invention relates to a parachute ground disconnecting device. The device comprises a lock/release mechanism for keeping a link assembly connected to a parachute in a holding position during a predetermined time interval and a...  
WO/2008/037030A1
An aircraft advertising display system includes an emergency drop arrangement, including a ballast release mechanism for releasing ballast which will actuate after the system has been released from an aircraft but prior to the deployment...  
WO/2008/014524A3
A towable lift system and components and accessories therefore, particularly for use in sports and recreational activities coupling the airfoil to a rider.  
WO/2007/107018A1
The present invention relates to an autonomous stratosphere platform which is preferably intended to be positioned in the stratosphere, is carried by a carrying shield (1) and is controlled by a control and drive unit (3) which can use c...  
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 ...  

Matches 101 - 150 out of 923