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Patent Searching and Data


Matches 101 - 150 out of 1,017

Document Document Title
WO/2015/080614A1
A recovery system used primarily for recovering liquid rocket engines for the purpose of reusing or repeatedly reusing same in the first stage (stage-and-a-half) of a rocket. The technical result of the claimed invention consists in i...  
WO/2015/059703A1
The present invention relates to a parachute deploying apparatus, comprising: a )a manifold with which is releasably coupled a single vessel within which pressurized gas is generated; b) a gas generator which cooperates with said vessel;...  
WO/2015/012969A3
Disclosed herein are systems and methods for using computer vision for parafoil flight control. According to an aspect, a method includes capturing an image of a parafoil including multiple indicator points distributed thereon. The metho...  
WO/2015/027041A1
A trap system is presented for deployment of a reserve parachute. The trap system includes a trap line with a first end coupled to a main parachute and a trap attached to a surface of the container. The trap includes an outer perimeter t...  
WO/2015/012969A2
Disclosed herein are systems and methods for using computer vision for parafoil flight control. According to an aspect, a method includes capturing an image of a parafoil including multiple indicator points distributed thereon. The metho...  
WO/2014/094870A1
An autogyro (1) comprises a support structure (2) having a rotor mast (3), a rotor head (4), which is attached to the rotor mast (3) and has a rotor mount (420) having rotor articulation means (410, 411), to which a rotor (5) is attached...  
WO/2014/080409A1
The present invention provides safety apparatus for a multi-blade aircraft, comprising an expandable and collapsible parachute assembly having a plurality of inflatable tubes, a plurality of electrically triggered gas generators connecte...  
WO/2012/159118A3
A separating mechanism for releasing an equipment bag. The mechanism includes a base assembly, a removable soft loop assembly, an attachment ring, and a retention member. The base assembly includes a base member, an aperture, and one or ...  
WO/2011/011708A3
A system and method of deploying a parachute system (10, 110), wherein the system functions with a timed delay or without a timed delay. The system can include a primary static line (12) and a release-away line (14), wherein the primary ...  
WO/2013/181722A3
The Road-and-air transport vehicle is intended to transport people (from 1 to 4 people] on the roads, as a light passenger vehicle, and in the air - as a small aircraft. It has a body (1] with a cabin (13), 4 wheels: 2 front wheels, cont...  
WO/2014/009931A1
A parachute device is provided with a bag containing a main parachute and a reserve parachute and with a propulsion assembly (14) having a frame (15) to which two arms (16) are coupled; the two arms can be opened laterally by operating a...  
WO/2014/012122A1
An inflatable parachute having a canopy (3) of parachute fabric and an airtight inflatable tube (2) around the edge of the canopy, an inflating device in communication with the tube (2) and a means (5) for triggering the inflating device...  
WO/2014/010601A1
[Problem] The purpose of the present invention is to provide a method for creating tracking data and a program for creating tracking data that are able to easily create tracking data containing a large amount of information. [Solution] T...  
WO/2013/166596A1
A safety system for a traction kite comprises a central load bearing line and sliding control bar arrangement comprising a connection loop for connection to a harness hook, a system hub connecting the loop to the central load bearing lin...  
WO/2013/156004A1
Parachute rescue system, destined for aircrafts with a rotating blade, as are especially helicopters or gyroplanes, consists at least from one rescue parachute (1), located before the activation of the system in a mounting box (2) and is...  
WO/2013/138703A1
A cost-effective pack adapted to be distributed from an aircraft in the event of a natural, military, political, or other disaster includes an outer package, at least one item in the outer package for aerial delivery, and at least one ae...  
WO/2013/120357A1
An airplane anti-falling and self-rescuing device. An upper connection plate (8, 9) is connected to the outer wall of the upper end of an airplane body (1). The upper connection plate (8) is connected to a hot-air parachute column (2), a...  
WO/2013/118112A1
Wind parameter indication device and method for providing an indication of wind speed and wind direction. The device is deployed along an aerial trajectory toward a ground surface, such as after being ejected from an aircraft in flight. ...  
WO/2013/103775A1
A parachute canopy release comprising a harness strap and a parachute riser. The parachute riser has a terminal end connected to a riser ring. The harness strap has a connector assembly comprising a ring assembly and a latch assembly. Th...  
WO/2013/049805A1
A harness container for a parachutist has a bio-contoured support cradle or load distributing vest. The load distributing vest, which is generally U-shaped and includes an upper yoke and two straps integral with the yoke, has a multi-lay...  
WO/2012/069863A1
The present invention relates to an aircraft with an emergency landing system comprising a parachute (5) with 4 parachute strings (2) attached to the wings of the plane and to the fuselage. At the upper side of the fuselage there is a pa...  
WO/2012/045929A1
The present invention relates to the field of devices for airdropping a load from a flying vehicle, wherein specifically the aim of the invention is to provide a device for securing/releasing a first element (65) capable of supporting a ...  
WO/2012/003285A1
Disclosed is a system for the airborne deployment and delivery of palletized cargo. The system includes a cargo pallet, one or more risers connected to the pallet, and an associated rigging. The risers are used in both stabilizing the ca...  
WO/2011/156370A1
A ground impact cargo parachute release mechanism includes a pair of interlocking release elements, one for connection to the parachute the other the cargo; each release element has a pawl and a notch for engaging the pawl of the other r...  
WO/2011/146349A2
An unmanned air module includes one or more rotors, engines, a transmission and avionics. Any of several different ground modules may be attached to the air module. The air module may fly with and without the ground module attached. The ...  
WO/2011/119164A1
In various examples, a speed limiting apparatus (100, 200) includes a garment (102, 202)) configured to be worn by a user (10). The garment includes an enclosure (110, 220). A speed limiting assembly (120, 220) is coupled to the garment....  
WO/2011/087785A1
A system i s provided for the force decay triggered release of a device, the system compris ing: a base; a plural ity of retention rods extend ing from the base; a rotationa l ly movabl e actuator, to wh ich a l i n ear force is confi gu...  
WO/2011/082775A1
The invention relates to a parachute composed of a plurality of individual textile strips (11) separated from one another, at least two groups of individual strips in each case comprising a plurality of individual strips running parallel...  
WO/2011/029851A3
The invention relates to a sail (2) including a fabric made of continuous warp and weft yarns. When the sail is in flight, first yarns, which are either warp yarns or weft yarns, extend in the anteroposterior direction (AP) of the sail, ...  
WO/2011/043753A1
The mechanically opening parachute (10) is a parachute that may be opened quickly at low altitudes, such as during an emergency exit from an office building, for example. The mechanically opening parachute (10) includes a telescopic tube...  
WO/2010/143810A3
The present invention relates to life preserver parachute equipment, and more particularly, to life preserver parachute equipment designed to be stored in a secure location on the veranda of every household in an apartment building, hote...  
WO/2011/029851A2
The invention relates to a sail (2) including a fabric made of continuous warp and weft yarns. When the sail is in flight, first yarns, which are either warp yarns or weft yarns, extend in the anteroposterior direction (AP) of the sail, ...  
WO/2011/011708A2
A system and method of deploying a parachute system (10, 110), wherein the system functions with a timed delay or without a timed delay. The system can include a primary static line (12) and a release-away line (14), wherein the primary ...  
WO/2011/002305A1
A wingrig comprising an integrated harness and wingsuit is presented. The wingrig gives improved ergonomic conditions compared to the state of art today. The wing suit comprises leading structures which can receive parts of the harness. ...  
WO/2010/143810A2
The present invention relates to life preserver parachute equipment, and more particularly, to life preserver parachute equipment designed to be stored in a secure location on the veranda of every household in an apartment building, hote...  
WO/2010/138714A1
According to certain embodiments, an aerial delivery system configured to be deployed from an aircraft comprises a base, a sleeve generally configured to be positioned on the base, a bag configured to receive at least one liquid and a li...  
WO/2010/130043A1
An apparatus for supporting a parachute flight controller from a parachute comprises a bearing member, for example a pulley, a load-bearing coupling, for example a harness, connected to the bearing member and including a connector for co...  
WO/2010/106310A1
The invention relates to an improved ram air inflating lifting body (1) such as a para-foil. The lifting body (l) being configured so as to be controllable by changing the effective chord length ( 5) of at least one of the surfaces (2, 3...  
WO/2010/047534A3
The present invention relates to an umbrella type parachute and particularly to an umbrella type emergency parachute, wherein parachute ribs supporting the canopy are allowed to be folded in 2 steps or 3 steps or more so that the parachu...  
WO/2009/138188A3
A parachute system is disclosed for especially ballistically deployed systems. Said parachute system comprises an unopened parachute (20), the canopy (1) of which is enclosed by a packsack (11) that has predetermined breaking points (12)...  
WO/2010/078295A1
A parachute seat includes a saddle formed by an ergonomically shaped saddle base member with a cushioning layer thereon that covers and conforms with the shape of the upper surface of the saddle base member. The saddle is preferably rece...  
WO/2010/031377A3
The invention relates to a flying object comprising at least one brake parachute (2), said flying object (1; 1') being provided with at least one fixing device (3; 3', 3") for the brake parachute (2) and with a drag line (4) between the ...  
WO/2010/047534A2
The present invention relates to an umbrella type parachute and particularly to an umbrella type emergency parachute, wherein parachute ribs supporting the canopy are allowed to be folded in 2 steps or 3 steps or more so that the parachu...  
WO/2010/042335A1
The present invention provides a two layer polyolefin film including a polymer barrier layer, and an adhesive layer including a polyolefin grafted with maleic anhydride and ungrafted polyolefins. The adhesive layer has a maleic anhydride...  
WO/2010/031377A2
The invention relates to a flying object comprising at least one brake parachute (2), said flying object (1; 1') being provided with at least one fixing device (3; 3', 3") for the brake parachute (2) and with a drag line (4) between the ...  
WO/2009/149713A1
The invention relates to controlling the shape of a flexible element (11). The invention is especially advantageous under conditions wherein the gravitational force is small and the atmospheric pressure is low, such as onboard a spacecra...  
WO/2009/138188A2
A parachute system is disclosed for especially ballistically deployed systems. Said parachute system comprises an unopened parachute (20), the canopy (1) of which is enclosed by a packsack (11) that has predetermined breaking points (12)...  
WO/2009/129642A1
A parachute rescue device (3) has parachutes (13) whose lines are formed by parachute rods (37) or arrangements of rods and cords (92). These spring-elastic rods (37) serve for deploying the parachutes (13) at standstill already. The can...  
WO/2009/127026A1
A device for locating the main canopy from a parachute, after said canopy has been disconnected by the parachutist as a result of the need to use the reserve parachute (reserve canopy) in an emergency situation. The device consists of a ...  
WO/2009/112875A1
The system for ejection of a safety parachute from a paraplane seat comprises an ejection device (17, 25), fixed on one side to an outer side of the seat (21) and equipped with a locking tool (11, 23), connected to a cord (10), and a par...  

Matches 101 - 150 out of 1,017