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公开(公告)号：EP1463663A4
公开(公告)日：2009-08-05
申请号：EP02797214
申请日：2002-12-09
申请人： ATAIR AEROSPACE INC
发明人： PRESTON DANIEL
IPC分类号： B64D17/34 , B64C31/036 , B64D1/14 , B64D17/02 , B64D17/04 , B64D17/08 , B64D17/38 , B64D17/54
CPC分类号： F42B10/56 , B64D1/08 , B64D1/14 , B64D17/025 , B64D17/04 , B64D17/08 , B64D17/34 , B64D17/38 , B64D17/54 , B64D17/74 , F42B4/28 , F42B10/58 , G05D1/105
摘要： 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 parachute for soft landing, a harness/container system, flight computer, position sensors and actuation system. The system is dropped from an airplane, a predetermined period of drogue fall ensures a stable position prior to deploying the guidance parachute. The flight controller determines a heading to intersect with an area substantially above the desired target and controls the guidance parachute via pneumatic actuators connected to the parachutes steering lines to fly on that heading. At a minimum altitude prior to the systems impact with the ground the flight computer transitions the system from the fast high performance guidance parachute to a larger landing parachute by releasing the guidance parachute to static line extract and deploy the landing parachute. If the system reaches a position substantially above target area prior to the parachute transition altitude flight computer controls the system into a spiral dive or other rapid altitude dropping maneuver until the transition altitude is reached. Once transitioned to the landing parachute the system descends for a brief period unguided under the landing parachute until touchdown.
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公开(公告)号：EP0984886A1
公开(公告)日：2000-03-15
申请号：EP98918381.9
申请日：1998-04-21
CPC分类号： B64D17/343 , B64D17/08 , B64D17/36 , B64D17/62
摘要： 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 vent at the apex, and suspension lines descend from the lower edge or skirt of the canopy to risers or harness. The small auxiliary canopy is slidably attached to the suspension lines between the main canopy and the harness. The auxiliary canopy includes a generally hemispherical central inner section made of a low air permeable material and a generally annular flat outer section made of a high air permeable material, preferably one offering little or no resistance to air flow therethrough. The outer section is provided with spaced fittings around the periphery to slidably receive individual suspension lines therethrough. When packed, the auxiliary canopy is located near the mouth of the main canopy to control the shape of the mouth of the main canopy during opening but slides down the suspension lines as the main canopy fully inflates thereby controlling the opening sequence. By controlling the inflation characteristics of the parachute with the auxiliary canopy, the opening forces and/or the time to full open can be reduced, or increased, for a given speed.
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公开(公告)号：EP4424600A1
公开(公告)日：2024-09-04
申请号：EP24160844.7
申请日：2024-03-01
CPC分类号： B64D17/36
摘要： A shock load attenuation device is provided. The shock load attenuation device includes a crushable material; a first compartment (316) in the crushable material surrounding a first line; and a second compartment (318) in the crushable material surrounding a second line. In response to the first line being acted upon by a first force and the second line being acted upon by a second force, a first loop in the first line is configured to slide along the second line and a first loop in the second line is configured to slide along the first line, crushing the crushable material.
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公开(公告)号：EP0984886B1
公开(公告)日：2004-08-04
申请号：EP98918381.9
申请日：1998-04-21
CPC分类号： B64D17/343 , B64D17/08 , B64D17/36 , B64D17/62
摘要： 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 vent at the apex, and suspension lines descend from the lower edge or skirt of the canopy to risers or harness. The small auxiliary canopy is slidably attached to the suspension lines between the main canopy and the harness. The auxiliary canopy includes a generally hemispherical central inner section made of a low air permeable material and a generally annular flat outer section made of a high air permeable material, preferably one offering little or no resistance to air flow therethrough. The outer section is provided with spaced fittings around the periphery to slidably receive individual suspension lines therethrough. When packed, the auxiliary canopy is located near the mouth of the main canopy to control the shape of the mouth of the main canopy during opening but slides down the suspension lines as the main canopy fully inflates thereby controlling the opening sequence. By controlling the inflation characteristics of the parachute with the auxiliary canopy, the opening forces and/or the time to full open can be reduced, or increased, for a given speed.
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5.发明公开AIR IMPERMEABLE PARACHUTE CANOPY WITH OPENING ASSIST 失效LUFTUNDURCHLÄSSIGERFALLSCHIRM MITÖFFNUNGSHILFE
公开(公告)号：EP0757648A4
公开(公告)日：1997-12-10
申请号：EP95904085
申请日：1994-11-21
发明人： WEBB DAVID B , WRIGHT DAVID A
CPC分类号： B64D17/62
摘要： 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 upon inflation as to allow incorporation of high drag coeeficient, generally air impermeable canopy fabric.
摘要翻译： 本发明涉及具有在中央主通风口（15）上以紧密间隔布置的中央盖罩（30）的环形伞面降落伞（10），其有助于提供快速控制的充气并减少充气时的振动，从而允许并入高阻力 系数，通常不透气的篷面料。
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