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Patent Searching and Data


Matches 101 - 150 out of 870

Document Document Title
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...  
WO2003095304A3
An automatic controlled parachute includes a parachute canopy, a flight controller (110) and risers (131) connecting the canopy to the flight controller (110). Pneumatic actuators (20) are connected along the risers (131). The flight con...  
WO/2004/018288A2
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...  
WO2003068596A3
The airwing structure (100) according to the present invention comprises of an airfoil structure (105), a main frame (110), and a means for providing a downward and a forward tension (115) on the airfoil structure. The airfoil structure ...  
WO2003010440A9
The invention concerns a jettisoning system, for numerous uses, in particular different types of fastening tips when practising gliding sports. A ring (4) is wedged by a force fold (8) against a central part (7). Said fold is itself wedg...  
WO/2004/014728A1
A parachute canopy comprising a plurality of gores (12) wherein at least one of the gores comprises an inflation pocket (25) and a method for making said parachute canopy comprising the steps of folding a plurality of rectangular gones i...  
WO2003053777A9
An autonomous guided parachute system for cargo drops that divides the requirements of guidance and soft landing into separate parachutes. Said invention includes a high wing-loaded ram air parachute for guidance, a larger round parachut...  
WO/2003/106262A1
The invention concerns a flexible box wing, characterized in that it comprises means for receiving a user's arms at least partly inside the box structure wing (10), such that the user's arms control the deployment of the wing (10), and i...  
WO2003033072A3
The invention relates to a rescue and survival case comprising at least three integrated compartments in which appliances or tools required for an emergency are arranged according to the function thereof. A round-canopy parachute compris...  
WO/2003/100261A2
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...  
WO/2003/099656A1
The aim of the invention is to reduce the rate of vertical descent of an aircraft in distress at the moment it touches the ground, such that people and equipment are protected as far as possible. To this end, a parachute (7) and at least...  
WO/2003/099655A2
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...  
WO2003053778A3
A ram air parachute of the present invention includes specific cross porting of the ribs between certain cells to create a two-stage or multi-stage deployments. Cross ports between certain sets of cells have reduced or no conductance. In...  
WO/2003/095305A1
A device for the automatic opening of a parachute, comprising a casing (1) closed with a lid (2), in which are located the means (13, 14) for electronically sensing the altitude of the parachute during the jump and the time and falling s...  
WO2003053779A3
The ram air parachute has a number of novel features which limit distortions to the canopy and improve performance. Restrictions on the inlets (25a, 25b) to the cells (42, 43, ) operate reduce drag during flight and to reduce opening for...  
WO2002040342A9
Short-haul escape system (10) includes line (12) for detechable suspension from support member (20) on airborne vehicle (22), load-carrying receptacle (24) attached to end (12B) of line (12), container (16) attachable to airborne vehicle...  
WO/2003/095304A2
An automatic controlled parachute includes a parachute canopy, a flight controller (110) and risers (131) connecting the canopy to the flight controller (110). Pneumatic actuators (20) are connected along the risers (131). The flight con...  
WO2003053777A3
An autonomous guided parachute system for cargo drops that divides the requirements of guidance and soft landing into separate parachutes. Said invention includes a high wing-loaded ram air parachute for guidance, a larger round parachut...  
WO/2003/089298A2
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/2003/068596A2
The airwing structure (100) according to the present invention comprises of an airfoil structure (105), a main frame (110), and a means for providing a downward and a forward tension (115) on the airfoil structure. The airfoil structure ...  
WO/2003/053778A2
A ram air parachute of the present invention includes specific cross porting of the ribs between certain cells to create a two-stage or multi-stage deployments. Cross ports between certain sets of cells have reduced or no conductance. In...  
WO2002102661A3
The disclosed integrated parachute harness system (100) has multiple points of resistance, thereby securing a wearer in three directions. The system further relates to an integrated system including a parachute harness (110), a survival ...  
WO/2003/053779A2
The ram air parachute has a number of novel features which limit distortions to the canopy and improve performance. Restrictions on the inlets (25a, 25b) to the cells (42, 43, ) operate reduce drag during flight and to reduce opening for...  
WO/2003/053777A2
An autonomous guided parachute system for cargo drops that divides the requirements of guidance and soft landing into separate parachutes. Said invention includes a high wing-loaded ram air parachute for guidance, a larger round parachut...  
WO/2003/045781A1
The invention relates to a pneumatic gliding wing (1) for a freefall jumper (2), comprising a rigid part (3) which is made of, for example, a composite material such as GFK or CFK. Said rigid part is provided with a recess (5) for a para...  
WO/2003/033072A2
The invention relates to a rescue and survival case comprising at least three integrated compartments in which appliances or tools required for an emergency are arranged according to the function thereof. A round-canopy parachute compris...  

Matches 101 - 150 out of 870