ES1020652U - Paracaidas. - Google Patents

Paracaidas.

Info

Publication number
ES1020652U
ES1020652U ES19909001318U ES9001318U ES1020652U ES 1020652 U ES1020652 U ES 1020652U ES 19909001318 U ES19909001318 U ES 19909001318U ES 9001318 U ES9001318 U ES 9001318U ES 1020652 U ES1020652 U ES 1020652U
Authority
ES
Spain
Prior art keywords
parachute
tapes
translation
machine
legally binding
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.)
Granted
Application number
ES19909001318U
Other languages
English (en)
Other versions
ES1020652Y (es
Inventor
Cue Carlos Sintora
Fernandez Domingo Moratilla
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.)
Expal Systems SA
Original Assignee
Explosivos Alaveses SA
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 Explosivos Alaveses SA filed Critical Explosivos Alaveses SA
Priority to ES9001318U priority Critical patent/ES1020652Y/es
Priority to AR31865790A priority patent/AR247859A1/es
Publication of ES1020652U publication Critical patent/ES1020652U/es
Application granted granted Critical
Publication of ES1020652Y publication Critical patent/ES1020652Y/es
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

Links

Landscapes

  • Professional, Industrial, Or Sporting Protective Garments (AREA)

Abstract

PARACAIDAS, QUE TENIENDO COMO FINALIDAD PROVEER UN ALTO COEFICIENTE DE ARRASTRE A VEHICULOS LANZADOS A BAJA COTA Y GRANDES VELOCIDADES, ASI COMO UNA RAPIDA AMORTIGUACION DE LAS ALTERACIONES DE TRAYECTORIA CUANDO EL VEHICULO ES EXPULSADO SOBRE EL MEDIO AMBIENTE, SE CARACTERIZA PORQUE ESTA CONFORMADO POR UN VELAMEN CRUCIFORME (2, 3) Y DOCE CINTAS DE SUSPENSION (4), FORMANDOSE EL VELAMEN POR DOS PAÑOS SUPERPUESTOS (2, 3), EN CRUZ, SOBRE LA CONFLUENCIA DE SUS EJES, CON LAS CINTAS DE SUSPENSION (4) ENVOLVIENDO EL VELAMEN PARA DEFINIR LA ESTRUCTURA RESISTENTE DEL PARACAIDAS, CONVERGIENDO EN CUATRO GRUPOS DE TRES CINTAS SOBRE UNA ARNES (5) INDEPENDIENTE PARA CADA ALA DEL VELAMEN, HABIENDOSE PREVISTO QUE LA CUPULA (6) POSEA DOS CINTAS (7) COSIDAS EN DIAGNAL, QUE ADEMAS DE REFORZAR LA ESTRUCTURA DE LA ZONA, CONTROLAN LAS DEFORMACIONES PRODUCIDAS POR LA PRESION EN EL MOMENTO DE APERTURA Y LLENADO DEL VELAMEN.
ES9001318U 1990-04-23 1990-04-23 Paracaidas. Expired - Fee Related ES1020652Y (es)

Priority Applications (2)

Application Number Priority Date Filing Date Title
ES9001318U ES1020652Y (es) 1990-04-23 1990-04-23 Paracaidas.
AR31865790A AR247859A1 (es) 1990-04-23 1990-12-18 Paracaidas

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
ES9001318U ES1020652Y (es) 1990-04-23 1990-04-23 Paracaidas.

Publications (2)

Publication Number Publication Date
ES1020652U true ES1020652U (es) 1992-08-01
ES1020652Y ES1020652Y (es) 1993-06-16

Family

ID=8267255

Family Applications (1)

Application Number Title Priority Date Filing Date
ES9001318U Expired - Fee Related ES1020652Y (es) 1990-04-23 1990-04-23 Paracaidas.

Country Status (2)

Country Link
AR (1) AR247859A1 (es)
ES (1) ES1020652Y (es)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109466768A (zh) * 2018-10-31 2019-03-15 航宇救生装备有限公司 空投物资减速飘带

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109466768A (zh) * 2018-10-31 2019-03-15 航宇救生装备有限公司 空投物资减速飘带
CN109466768B (zh) * 2018-10-31 2021-11-16 航宇救生装备有限公司 空投物资减速飘带

Also Published As

Publication number Publication date
ES1020652Y (es) 1993-06-16
AR247859A1 (es) 1995-04-28

Similar Documents

Publication Publication Date Title
CA2116565A1 (en) Low Speed Model Following Velocity Command System for Rotary Wing Aircraft
CA2117098A1 (en) Dirigible airship
AU585243B2 (en) Aerodynamic device with reversible, flexible and lowerable concavity for the propulsion by the force of the wind
GB1314579A (en) Aerofoils
ATE43114T1 (de) Fallschirmanordnung.
DE3566654D1 (en) A parachute
ES1020652U (es) Paracaidas.
CA2183279A1 (en) Missile Having Non-Cylindrical Propulsion Section
GB1186631A (en) A Parachute
GB1018077A (en) Improvements in or relating to aircraft
Colucci Rotorcraft Pilot's Associate update- The Army's largest science and technology program
GB1075314A (en) Improvements in or relating to parachutes
GB1287755A (en) Improvements in or relating to gliding-type parachutes
GB860032A (en) Improvements in and relating to buoys
GB1443196A (en) Parachutes
EP0209171A3 (en) A device for yawing moment control for aircraft
GB2019335A (en) Rocket vehicles
RU1773804C (ru) Парашютна система
Kershner The student pilot's flight manual(Book)
SKRIPNICHENKO Classification of the principal fuel saving methods in flight operations(Klassifikatsiya osnovnykh metodov ehkonomii aviatopliva v letnoj ehkspluatatsii)
SU1378259A1 (ru) Система реактивного управления
MANTLE Air cushion craft development, first revision[Final Report]
KELLEY Pitch attitude stabilization system utilizing engine pressure ratio feedback signals[Patent]
SOLNECHNYI Problems in the synthesis of dynamic control systems satisfying given constraints on the state of the controlled system(Zadachi sinteza dinamicheskikh sistem upravleniia, udovletvoriaiushchikh zadannym ogranicheniiam na sostoianie ob'ekta)
SCHMIDT The aerodynamics range: A national historic mechanical engineering landmark[Final Report]

Legal Events

Date Code Title Description
FD1K Utility model lapsed

Effective date: 20000503