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Patent Searching and Data


Matches 101 - 150 out of 846

Document Document Title
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/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...  
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...  
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 ...  
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/2003/099655A2
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...  
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/2003/100261A2
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...  
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/2003/095304A2
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...  
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/2003/095305A1
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...  
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/2003/053777A2
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/2003/053779A2
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/2003/045781A1
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/2003/033078A1
The invention relates to a parachute (Survival Air Guard), preferably applicable in an extreme life-threatening emergency situation. The parachute is particularly embodied as a round parachute and comprises a canopy which is connected to...  
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...  
WO2002024528A9
A flexible linkage system (20) for connecting an environmentally sealed apparatus (40) such as a parachute system to an external apparatus such as a parachute harness, said system comprising an internal link (10) and an external link (21...  
WO/2003/010440A1
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/2003/004354A1
The invention relates to apparatus adapted to assist the exit of a parachutist from an aircraft in flight, and in particular to apparatus adapted to impart lateral movement to said parachutist during freefall and before parachute deploym...  
WO/2003/000548A1
The invention provides a device for closing parachute packs, each of which has a plurality of flaps and a closing cord (36), the device (10) being characterised by a base (12) for bearing on a flap in one direction during the packing ope...  
WO/2002/102661A2
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/2002/076828A1
This invention provides a parachute (10) provided with a retardation device (12), for retarding the downward velocity of a load (14) carried by the parachute (10). The retardation device (12) includes means for increasing the effective s...  
WO2002040342A3
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/2002/040342A2
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/2002/024528A1
A flexible linkage system (20) for connecting an environmentally sealed apparatus (40) such as a parachute system to an external apparatus such as a parachute harness, said system comprising an internal link (10) and an external link (21...  
WO/2002/022441A1
An improved cruciform or cross parachute is formed by attaching the adjacent edges of the lateral arms (14, 16, 18, 20) to each other to form a three-dimensional canopy (10), when inflated, which is substantially square at the top and su...  
WO/2002/004291A1
The invention concerns a wing with membrane rigidified by the pressure of its inflatable armature. The wing consists of a leading edge and inflatable strips designed and arranged so that the pressure generates tension over the whole asse...  
WO/2001/083296A1
A support which resiliently supports at least one of an upper wing and a lower wing constituting a canopy of a paraglider. A plurality of support rods are installed such that the are arranged at predetermined lengths from the front end t...  
WO/2001/074659A1
An aircraft with a detachable cabin (1) that serves to rescue its passengers as a result of the aircraft's sudden fall either due to its malfunction or fire. The cabin escapes either smoothly or by means of fast ejection and descends slo...  
WO/2001/070571A1
A flying device comprises a wing parachute (101), having a double layer canopy (102), shroud lines (103) and a double pontoon float (104) with a seat (105) for an aviator A, engine (106) with a propeller (107). Shroud points (108) are pr...  
WO/2001/058755A1
A wing for a traction kite, etc comprises a plurality of cells formed by chordwise-extending ribs (3), valved openings (6) to the cells allowing ram air to inflate the wing. By changing the initial cut-out of the material forming the cel...  
WO/2001/054977A1
A soft connector link (fig 1) is disclosed for connecting a first item to a second item such as canopy suspension lines to a canopy riser. In a first embodiment, the soft link preferably includes a flexible body member (21) having a firs...  

Matches 101 - 150 out of 846