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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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 ...
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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...
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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...
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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...
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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 ...
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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 ...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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...
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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...
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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...
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