CO2018009969A2 - Sistema modulador de planeo y método para un paracaídas ram-air - Google Patents

Sistema modulador de planeo y método para un paracaídas ram-air

Info

Publication number
CO2018009969A2
CO2018009969A2 CONC2018/0009969A CO2018009969A CO2018009969A2 CO 2018009969 A2 CO2018009969 A2 CO 2018009969A2 CO 2018009969 A CO2018009969 A CO 2018009969A CO 2018009969 A2 CO2018009969 A2 CO 2018009969A2
Authority
CO
Colombia
Prior art keywords
ram
cap
central section
parachute
planning
Prior art date
Application number
CONC2018/0009969A
Other languages
English (en)
Inventor
Jean C Berland
Original Assignee
Airborne Systems Na Inc
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 Airborne Systems Na Inc filed Critical Airborne Systems Na Inc
Publication of CO2018009969A2 publication Critical patent/CO2018009969A2/es

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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
    • B64D17/343—Load suspension adapted to control direction or rate of descent by reefing means
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS 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; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/02—Canopy arrangement or construction
    • B64D17/18—Vent arrangement or construction
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/22—Load suspension
    • B64D17/24—Rigging lines
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D17/00—Parachutes
    • B64D17/22—Load suspension
    • B64D17/24—Rigging lines
    • B64D17/26—Rigging lines attached to hem of canopy

Abstract

RESUMEN DE LA DIVULGACIÓN Se proporciona un sistema y un método para acortar líneas de suspensión específicas cerca del centro de un paracaídas Ram-Air con el fin de deformar la sección del perfil aerodinámico solo en la sección central del casquete. Esta deformación de la sección central lleva a una alteración significativa de la relación de planeo del paracaídas al reducir simultáneamente la velocidad de avance y aumentar la relación de descenso. Mientras tanto, debido a que el casquete solo está deformado en la sección central, las puntas del ala permanecen extendidas y presurizadas de modo que el aparato de dirección en el borde de salida del casquete permanece completamente funcional para dirigir el rumbo.
CONC2018/0009969A 2016-03-04 2018-09-21 Sistema modulador de planeo y método para un paracaídas ram-air CO2018009969A2 (es)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US15/061,804 US20170253339A1 (en) 2016-03-04 2016-03-04 Glide modulator system and method for a ram air parachute
PCT/US2017/019627 WO2017151483A1 (en) 2016-03-04 2017-02-27 Glide modulator system and method for a ram air parachute

Publications (1)

Publication Number Publication Date
CO2018009969A2 true CO2018009969A2 (es) 2019-02-08

Family

ID=59723249

Family Applications (1)

Application Number Title Priority Date Filing Date
CONC2018/0009969A CO2018009969A2 (es) 2016-03-04 2018-09-21 Sistema modulador de planeo y método para un paracaídas ram-air

Country Status (14)

Country Link
US (1) US20170253339A1 (es)
EP (1) EP3423355B1 (es)
JP (1) JP2019507059A (es)
KR (1) KR102587139B1 (es)
AU (1) AU2017225669B2 (es)
BR (1) BR112018067800A2 (es)
CA (1) CA3016194A1 (es)
CO (1) CO2018009969A2 (es)
ES (1) ES2918129T3 (es)
IL (1) IL261435A (es)
PL (1) PL3423355T3 (es)
RU (1) RU2018134775A (es)
WO (1) WO2017151483A1 (es)
ZA (1) ZA201805903B (es)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CH711520B1 (it) * 2015-09-15 2019-05-15 Enea Tumazzo Dario Paracadute-parapendio a coda.
US11040778B2 (en) * 2018-11-16 2021-06-22 Goodrich Corporation Multi-staged suspension line attenuator
US11084580B2 (en) * 2018-12-11 2021-08-10 Steven R Gay Adjustable shape kite
KR102186467B1 (ko) * 2018-12-14 2020-12-03 (주)다빈치프로덕츠 패러글라이더
RU2714988C1 (ru) * 2019-07-08 2020-02-21 ФЕДЕРАЛЬНОЕ ГОСУДАРСТВЕННОЕ КАЗЕННОЕ ВОЕННОЕ ОБРАЗОВАТЕЛЬНОЕ УЧРЕЖДЕНИЕ ВЫСШЕГО ОБРАЗОВАНИЯ "Военная академия Ракетных войск стратегического назначения имени Петра Великого" МИНИСТЕРСТВА ОБОРОНЫ РОССИЙСКОЙ ФЕДЕРАЦИИ Крепление клевант к свободным концам парашютной системы при помощи магнитов
CN112051860B (zh) * 2020-09-07 2022-04-19 中国航空工业集团公司成都飞机设计研究所 一种空滑迫降动态空滑比稳定方法
CN117480093A (zh) 2020-11-24 2024-01-30 薄雾移动集成系统科技有限公司 滑翔降落伞/风筝的操作装置和方法
CN114162333B (zh) * 2021-12-23 2023-07-21 航宇救生装备有限公司 利用翼肋控制冲压翼伞开伞性能的方法

Family Cites Families (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR585513A (fr) * 1924-09-09 1925-03-03 Parachute planeur dirigeable
US2973928A (en) * 1958-09-15 1961-03-07 Pino G Turolla Parachute construction
US3285546A (en) * 1964-10-01 1966-11-15 Space Recovery Res Ct Inc Multi-cell wing type aerial device
US3412963A (en) * 1965-05-24 1968-11-26 Arthur D. Struble Jr. Method and apparatus for supporting an object
US3524613A (en) 1968-04-08 1970-08-18 Pioneer Parachute Co Inc Flexible gliding wing
US3589654A (en) * 1969-02-06 1971-06-29 Snyder Stephen Louis Glide control system for controlled descent parachute
FR2624828B1 (fr) * 1987-12-21 1990-05-11 Laser Lab Sarl Harnais sellette pour parachute du type a aile souple
FR2731202B1 (fr) 1995-03-02 1997-06-27 Pascal Gerard Dispositif de reduction de surface pour ailes souples double surface
FR2816584B1 (fr) * 2000-11-16 2004-10-08 Rene Fejan Parapente bionique a voilure modulable

Also Published As

Publication number Publication date
KR102587139B1 (ko) 2023-10-06
ES2918129T3 (es) 2022-07-13
KR20190002441A (ko) 2019-01-08
IL261435A (en) 2018-10-31
US20170253339A1 (en) 2017-09-07
AU2017225669A1 (en) 2018-09-20
EP3423355A4 (en) 2019-09-11
CA3016194A1 (en) 2017-09-08
RU2018134775A (ru) 2020-04-06
AU2017225669B2 (en) 2022-03-31
ZA201805903B (en) 2019-07-31
BR112018067800A2 (pt) 2019-01-15
WO2017151483A1 (en) 2017-09-08
JP2019507059A (ja) 2019-03-14
EP3423355B1 (en) 2022-04-13
PL3423355T3 (pl) 2022-09-05
EP3423355A1 (en) 2019-01-09

Similar Documents

Publication Publication Date Title
CO2018009969A2 (es) Sistema modulador de planeo y método para un paracaídas ram-air
BR212017011290U2 (pt) degrau retrátil que tem uma função de rampa e de elevação
CN103847954B (zh) 伸缩式机翼
EP4292921A3 (en) Aerial vehicle with deployable components
ES2512915A1 (es) Ala deformable con extradós móvil
MX2016011265A (es) Faldon aerodinamico de tren de aterrizaje.
BR112015020484A2 (pt) aeronave
CO2018005937A2 (es) Plataforma más ligera que el aire
IL239606B (en) A method and system for controlling hovering flight for a rotary-wing aircraft, which allows maintaining a course or direction depending on its forward speed
IL239605B (en) A flight control system and method for a rotary-wing aircraft, which allows maintaining a course or direction depending on its forward speed
BR112016018274A2 (pt) Conjunto de elevação para uso durante uma inflação de um envelope de balão, método e sistema
ES2585283R1 (es) Morro de aeronave provisto de una cuaderna de conexión entre el alojamiento del tren de aterrizaje y el revestimiento exterior del fuselaje
EP3492374A3 (en) Retrofit flight control surface
WO2014163724A3 (en) An aircraft wing
BR112015025381A2 (pt) dispositivo para controlar a velocidade de um avião espacial durante a transição de uma fase de voo espacial para uma fase de voo aeronáutico e método de transição associado
EA201500683A1 (ru) Аэродинамическое устройство
RU2015149094A (ru) Применение способа полёта с несимметричной тягой для посадки самолёта при боковом ветре
CN204250359U (zh) 一种固定翼航测无人机尾翼
ES1144743Y (es) Sistema sustentador, propulsor y estabiliador para aeronaves de despegue y aterrizaje vertical
ES1291568Y (es) Disposición sustentadora, estabilizadora y propulsora para aeronaves de despegue y aterrizaje vertical
PL406606A1 (pl) Sposób zapewniania sterowalności statków powietrznych typu VTOL
ES2538595B1 (es) Estructura neumática de rigidización de la lona de un globo aerostático y aerostatos en general y operación de presurizado de dicha estructura
MX2015011331A (es) Faldon aerodinamico de tren de aterrizaje.
RU2010153792A (ru) Способ посадки самолета при боковом ветре и устройство для его осуществления
ES2693899R1 (es) Sistema contra-accidentes, control y mejora en aeronaves