ES2668493T3 - Sistema de soporte para la implementación de maniobras de interceptación de un parapente de carga y procedimiento para el ajuste del borde posterior de un parapente de carga - Google Patents

Sistema de soporte para la implementación de maniobras de interceptación de un parapente de carga y procedimiento para el ajuste del borde posterior de un parapente de carga Download PDF

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Publication number
ES2668493T3
ES2668493T3 ES15200309.1T ES15200309T ES2668493T3 ES 2668493 T3 ES2668493 T3 ES 2668493T3 ES 15200309 T ES15200309 T ES 15200309T ES 2668493 T3 ES2668493 T3 ES 2668493T3
Authority
ES
Spain
Prior art keywords
support
load
paraglider
maximum load
cargo
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Active
Application number
ES15200309.1T
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English (en)
Inventor
Jukka BIEHL
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Airbus Defence and Space GmbH
Original Assignee
Airbus Defence and Space GmbH
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Airbus Defence and Space GmbH filed Critical Airbus Defence and Space GmbH
Application granted granted Critical
Publication of ES2668493T3 publication Critical patent/ES2668493T3/es
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/22—Load suspension
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/02—Canopy arrangement or construction
    • B64D17/025—Canopy arrangement or construction for gliding chutes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/22—Load suspension
    • B64D17/34—Load suspension adapted to control direction or rate of descent

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Structure Of Belt Conveyors (AREA)
  • Tires In General (AREA)
  • Transmissions By Endless Flexible Members (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)

Abstract

Sistema de soporte para soportar una carga máxima (9) mediante un parapente de carga (1) con un ala (3) con borde posterior (4) que se puede unir con el sistema de soporte por medio de líneas de suspentaje (5'), estando fijada al borde posterior, para la implementación de maniobras de interceptación, al menos una línea de suspentaje o de recogida (5); caracterizado por que el sistema de soporte presenta un soporte (2) que se puede unir con las líneas de suspentaje (5'); al menos una unidad de carga máxima (6) que se puede unir con la carga máxima (9); y una primera correa corta de soporte de carga (7) y una segunda correa más larga de soporte de carga (8), que unen respectivamente la unidad de carga máxima (6) con el soporte y están diseñadas de tal forma que en situaciones de deslizamiento fuera de maniobras de interceptación el soporte de una carga máxima (9) unida con la unidad de carga máxima (6) se efectúe por medio de la primera correa corta de soporte de carga (7); pudiendo unirse la línea de suspentaje o la línea de recogida (5) con la unidad de carga máxima (6) de tal forma que la línea de suspentaje o la línea de recogida (5), para la implementación de una maniobra de interceptación, cause el ajuste del borde posterior (4) por la inercia de la carga máxima (9), efectuándose una separación de la primera correa corta de soporte de carga (7) y efectuándose el soporte de la carga máxima (9) por medio de la segunda correa más larga de soporte de carga (8).

Description

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Claims (1)

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    imagen2
ES15200309.1T 2014-12-18 2015-12-16 Sistema de soporte para la implementación de maniobras de interceptación de un parapente de carga y procedimiento para el ajuste del borde posterior de un parapente de carga Active ES2668493T3 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
DE102014018702 2014-12-18
DE102014018702.0A DE102014018702B4 (de) 2014-12-18 2014-12-18 Tragesystem zur Durchführung von Abfangmanövern eines Lastengleitschirms und Verfahren zum Verstellen der Hinterkante eines Lastengleitschirms

Publications (1)

Publication Number Publication Date
ES2668493T3 true ES2668493T3 (es) 2018-05-18

Family

ID=54979426

Family Applications (1)

Application Number Title Priority Date Filing Date
ES15200309.1T Active ES2668493T3 (es) 2014-12-18 2015-12-16 Sistema de soporte para la implementación de maniobras de interceptación de un parapente de carga y procedimiento para el ajuste del borde posterior de un parapente de carga

Country Status (5)

Country Link
US (1) US10207811B2 (es)
EP (1) EP3034406B1 (es)
KR (1) KR20160074428A (es)
DE (1) DE102014018702B4 (es)
ES (1) ES2668493T3 (es)

Families Citing this family (11)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US9694910B2 (en) 2013-02-22 2017-07-04 World View Enterprises Inc. Near-space operation systems
US10787268B2 (en) 2015-03-09 2020-09-29 World View Enterprises Inc. Rigidized assisted opening system for high altitude parafoils
EP3150486B1 (en) * 2015-10-01 2018-03-14 Airbus Operations GmbH Vortex generator arrangement, flow control system and method for controlling a flow on a rudder surface
ES2750683T3 (es) * 2015-12-01 2020-03-26 Airbus Operations Gmbh Dispositivo generador de torbellinos para un avión
US9540091B1 (en) 2016-02-11 2017-01-10 World View Enterprises Inc. High altitude balloon systems and methods
US9868537B2 (en) * 2016-04-13 2018-01-16 World View Enterprises Inc. Riser release flaring system for parafoils
US10124875B1 (en) 2017-01-09 2018-11-13 World View Enterprises Inc. Continuous multi-chamber super pressure balloon
US10336432B1 (en) 2017-01-09 2019-07-02 World View Enterprises Inc. Lighter than air balloon systems and methods
US11434011B1 (en) * 2018-08-05 2022-09-06 Earthly Dynamics, LLC One-time flare mechanism
AU2022254765A1 (en) * 2021-04-08 2023-11-16 Space Balloon Technologies Corp. Apparatus, method and system for balloon altitude control by in-situ characterization and active energy management
CN117401165B (zh) * 2023-11-24 2026-07-07 航宇救生装备有限公司 重装空投出机翻转控制方法及系统

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4729530A (en) * 1985-10-02 1988-03-08 Jalbert Domina C Control flaps for a multi-cell wing type canopy
DE19610052C2 (de) 1996-03-14 1998-07-09 Ulrich Dipl Ing Rieger Gleitschirmgerät für Springer
DE19634017C2 (de) * 1996-08-23 1999-08-26 Lfk Gmbh Gleitschirm-Fluggerät
DE19960332C1 (de) 1999-12-15 2001-02-15 Daimler Chrysler Ag Stellantriebssystem und Verfahren für einen Lastengleitschirm
EP1359091B1 (de) 2002-05-03 2007-12-26 EADS Deutschland GmbH Lastenabsetz-System mit einem Lastenschirm
DE10303788B4 (de) * 2002-05-03 2009-04-09 Eads Deutschland Gmbh Lastenabsetz-System mit einem Lastenschirm
DE10241585B4 (de) * 2002-09-05 2005-07-28 Eads Deutschland Gmbh Lastengleitfallschirm-System
US20090026319A1 (en) * 2004-04-20 2009-01-29 Edward Strong Aerial delivery system
US7448577B2 (en) * 2005-08-23 2008-11-11 The United States Of America As Represented By The Secretary Of The Army Apparatus for providing velocity differential between parachute and payload to reduce shock load
JP4945752B2 (ja) 2006-11-07 2012-06-06 国立大学法人九州工業大学 パラフォイルの飛行制御装置
US7648105B2 (en) * 2006-12-26 2010-01-19 Airborne Systems North America Of Nj Inc. Deployment brake release for a parachute
US8123171B2 (en) * 2008-07-02 2012-02-28 S.E., Inc. Load assisted release system

Also Published As

Publication number Publication date
US20160176531A1 (en) 2016-06-23
US10207811B2 (en) 2019-02-19
KR20160074428A (ko) 2016-06-28
EP3034406B1 (de) 2018-02-07
EP3034406A1 (de) 2016-06-22
DE102014018702B4 (de) 2021-06-24
DE102014018702A1 (de) 2016-06-23

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