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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...
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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 ...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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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...
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WO/2001/034464 |
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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...
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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...
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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, ...
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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...
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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...
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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...
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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...
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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 ...
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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...
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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 (...
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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...
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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...
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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 ...
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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 ...
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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...
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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, ...
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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...
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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...
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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...
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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...
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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...
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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...
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WO/1996/025062 |
The invention concerns an actuating device (5") which comprises a rotatable pot-shaped closure head (11) in which at least one finger recess (13) is provided. The finger recess (13) has flanks (14, 14') for the application of rotational ...
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WO/1995/014610 |
This invention relates to annular canopy parachutes (10) having a central cap canopy (30) in critically spaced arrangement at the central main vent (15), which assists in providing rapid controlled inflation and decreasing oscillation up...
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WO/1994/018071 |
The body described has a flexible outer skin (10) inside which are flexible intermediate walls (12) connected to the outer skin (10), said walls dividing the body into a plurality of chambers (14). At least one part of the outer skin (10...
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WO/1993/015956 |
A pin puller (10) for use in an automatic activation system for initiating the deployment of a parachute includes a small pyrotechnic actuator comprised essentially of a piston (44) and cylinder (42). The cylinder (42) includes a bracket...
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WO/1993/013982 |
An environmentally-sealed parachute deployment system for bail-out parachutes comprising a spring-loaded pilot parachute (36), an environmentally sealed vacuum bag (22), a deployment bag (21) having one or two elastic closure loops (65),...
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WO/1993/011999 |
The present invention relates to a leisure air sport device which is characterized in that it is comprised of the combinaison of a parachute (1), a balloon (2) housed in said parachute (1) and the wing (3) of a hang-glider made integral ...
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WO/1993/001089 |
The parachute proposed has a chute-opening device in the form of a tubular hose extending along at least one edge or seam of the parachute and inflated by compressed air. In order to improve the opening behaviour of the parachute, while ...
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WO/1992/006004 |
A paraglider has a lifting surface formed by an upper sail (5) and by a lower sail mutually linked by ribs (7) made of a fabric laid diagonally to the profile chord and provided with struts (18) at the suspension points of the bearing ro...
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WO/1991/010591 |
An anti-release device for two parts under load, which are interconnected by a releasable connecting device (2), consists of a combination of the following parts : a connecting device (21) which can be undone by a release mechanism (3), ...
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WO/1991/008948 |
The belt device for a paraglider (1) with a seat (2) comprises a shock-reducing absorber (3) arranged on the seat (2) in the form of inflatable mattress-like air-cushions (4) fitted in fabric pockets (5) which can be integrated into the ...
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WO/1991/007316 |
A device for supplying air to a double-surfaced aerodynamic shape having an upper or suction surface (1) and a lower surface (2), characterized in that the lower surface is air permeable over at least a substantial portion of its surface...
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WO/1991/005703 |
The invention relates to the field of aeronautical drogues. The prior art aeronautical drogues require a tanker aircraft to use different drogues to enable the tanker to refuel aircraft having widely differing speeds such as helicopters ...
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WO/1991/004909 |
A parachute with a canopy and shroud lines secured thereto to hold a person or load and with a hose-like opening aid fitted on the lower hem of the canopy and guided at least partially along the base, in which the hose-like opening aid i...
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WO/1990/005664 |
Automatic mechanical device comprising a casing (1), fitted inside the equipment to be released, from which two cables (3) in sheaths (2) run to two controls holding the cords of the equipment in the harness worn by the parachutist. The ...
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