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Matches 101 - 150 out of 383

Document Document Title
WO/2003/099656
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/2003/100261
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/2003/095304
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/2003/095305
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...  
WO/2003/089298
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/2003/068596
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/2003/053778
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/2003/053777
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/2003/053779
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/2003/045781
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/2003/033078
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/2003/033072
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/2003/010440
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/2003/004354
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/2003/000548
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/2002/102661
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/2002/076828
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...  
WO/2002/040342
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/2002/024528
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/2002/022441
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/2002/004291
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/2001/083296
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/2001/074659
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/2001/070571
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/2001/058755
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/2001/054977
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...  
WO/2001/052225
An emergency drop system allows ballasted advertising banner (14) if disconnected from an aircraft to descend slowly to the ground. Banner (14) is suspended below an aircraft by line (4) held taut by ballasted container (24). Static line...  
WO/2001/034464  
WO/2001/028876
A parachute system (10) includes a drogue parachute (12) connected to a deployment bag (32) by a drogue bridle (42) and drogue kill line (100). The bridle (42) includes a stop (44) carried within the container (14) for suspension thereof...  
WO/2001/000489
The invention relates to a paraglider or a stunt kite that resembles a paraglider. Said paraglider or kite is provided with one cell (1) that essentially extends across the entire surface of the canopy and that is essentially not sub-div...  
WO/2000/071416
Disclosed is a low-drag/high-speed pilot chute (50) which is attached to a bridle cord (80), and a high-drag/low-speed pilot chute (20) which is attached with a weak link (36) to the bridle cord (80). In a low-speed deployment scenario, ...  
WO/2000/040867
The invention relates to a locking element (9) made of spring wire. The locking element is built up of at least one bent portion (10), which ends in two intersecting legs (11, 12), which join said bent portion at least substantially tang...  
WO/2000/020277
A safety device for low-altitude fall adapted to reduce the rate of falling even from a low altitude and absorb a shock upon landing. An auxiliary parachute device (5) includes a parachute body (8) having a sheet material (7) spread over...  
WO/2000/009394
An automatic parachute opening device provides the possibility of opening main and reserve parachutes at predetermined heights above the ground. A microcontroller within the device monitors the rate of descent and height above ground lev...  
WO/1999/061315
A parafoil assembly includes a canopy (20) having a plurality of generally parallel inflatable cells (22, etc.) and suspension lines (36, etc.) extending from opposite sides of each of the cells (22, etc.) toward a central area beneath t...  
WO/1999/050142
The invention relates to a method for rapidly deploying an emergency parachute. According to said method, at the latest at the end of the blast-off path the parachute (1) is jerked backward in the direction of the object which has to be ...  
WO/1999/043546
The invention relates to a parachute consisting of a parachute canopy comprising an apex and a base, as well as rigging lines attached to the base for holding the object to be decelerated by means of the parachute. The parachute is prepa...  
WO/1999/037538
A gas-powered landing velocity attenuator for reducing the final descent velocity (and consequent ground impact load) of a parachutist or parachuted cargo. Immediately prior to impact, the gas source powers a means for drawing the load (...  
WO/1999/028186
The present invention relates to a method for slowing down a load attached to a parachute during the end phase of the jettison or parachuting so that the landing speed during the landing phase is close to zero. To this end and during the...  
WO/1999/007602
The 'A' harness, attachable to a paragliding wing by two M closure connectors (inserted in 'S' adjustable shoulder straps), is equipped on both sides (or on appendages coming from the shoulder straps) with 'G2' parts of two buckles, whos...  
WO/1998/052821
The invention concerns the problem of eliminating a parachute after its inert load has landed so that the load is not discovered. The device consists in a balloon (8) inflated by the contents of a helium cylinder (7) opened by a control ...  
WO/1998/052820
A round conventional parachute is shown with a small auxiliary canopy for controlling the inflation characteristics of the main canopy, especially large generally axisymmetrical canopies for heavy payloads. The main canopy has a central ...  
WO/1998/029305
The invention concerns a glider comprising a wing unit capable of taking the form of a streamlined wing, the wing unit including an upper surface (4) and a lower surface (6) defining a leading edge (8) and a trailing edge (10), the glide...  
WO/1997/048603
A pressure-sensitive locking device comprises a housing (2, 20) having an opening therein, and an insertable member (1, 21) adapted to be inserted into the opening whereupon it can enter into locking engagement with a locking member (4, ...  
WO/1997/048602
The invention discloses in particular a method for controlling the direction of movement of an air carrier comprising a source of energy (10), at least one rudder unit (9), at least one actuator (13) acting on these rudder units (9), and...  
WO/1997/044242
An improved cruciform or cross parachute, especially for personnel use. The central section (12) and canopy arms (14, 16, 18, 20) are made from a zero or near zero porosity fabric, and air from underneath the canopy is vented as air vent...  
WO/1997/038901
The object of this invention is a device where the canopy of a lighter-than-air craft can, at the demand of the operator, transform itself into a convex surface that will enable the occupant or occupants of the aerostat to parachute down...  
WO/1997/025245
A load securing and releasing system (10) for releasably attaching two objects together, one of the objects preferably being a parachute. The secure and release system (10) having a main load carrying component (12) with a first end port...  
WO/1997/014611
A parachute assembly comprising a primary parachute (8) and an auxiliary parachute (18) coupled to the primary parachute (8) via a bridle (22). A pre-loaded ejection spring (26) is provided in the parachute pack (2) between the primary p...  
WO/1997/000810
An apparatus including a square sail (ABCD) consisting of eight cells (1-8) made of a translucent fabric (14) on the outside and of a coloured fabric (18) between the cells, four square air inlets (13) being provided therein and connecte...  

Matches 101 - 150 out of 383