RU1773804C - Parachute system - Google Patents
Parachute systemInfo
- Publication number
- RU1773804C RU1773804C SU904791434A SU4791434A RU1773804C RU 1773804 C RU1773804 C RU 1773804C SU 904791434 A SU904791434 A SU 904791434A SU 4791434 A SU4791434 A SU 4791434A RU 1773804 C RU1773804 C RU 1773804C
- Authority
- RU
- Russia
- Prior art keywords
- control lines
- cargo
- parachute system
- control
- silt
- Prior art date
Links
Landscapes
- Emergency Lowering Means (AREA)
Abstract
Изобретение относитс к авиационной технике и может быть использовано при создании средств десантировани грузов, обладающих собственным флюгерным, моментом , и спасени летательных аппаратов в аварийной ситуации. Целью изобретени вл етс повышение надежности управлени куполом за счет исключени защепле- ни строп управлени . В управл емом парашютной системе, содержащей купол- крыло 1, подвесную систему 2 груза 3, основные стропы 4 и стропы 5 управлени , введена кинематическа пара 7 с вращательной степенью свободы и отверстием 8 вдоль оси 9 вращени , через которое проход т стропы 5 управлени . 4 ил,The invention relates to aeronautical engineering and can be used to create means of airborne cargo possessing its own weather vane, moment, and rescue aircraft in an emergency. The aim of the invention is to increase the reliability of control of the dome by eliminating the clogging of the control lines. In a controlled parachute system comprising a canopy 1, a suspension system 2 of cargo 3, main slings 4 and control lines 5, a kinematic pair 7 with a rotational degree of freedom and a hole 8 along the axis of rotation 9 through which control lines 5 pass is introduced. 4 silt
Description
®fctf®fctf
flfcfcJflfcfcJ
№4Number 4
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU904791434A RU1773804C (en) | 1990-02-14 | 1990-02-14 | Parachute system |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SU904791434A RU1773804C (en) | 1990-02-14 | 1990-02-14 | Parachute system |
Publications (1)
Publication Number | Publication Date |
---|---|
RU1773804C true RU1773804C (en) | 1992-11-07 |
Family
ID=21496233
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SU904791434A RU1773804C (en) | 1990-02-14 | 1990-02-14 | Parachute system |
Country Status (1)
Country | Link |
---|---|
RU (1) | RU1773804C (en) |
-
1990
- 1990-02-14 RU SU904791434A patent/RU1773804C/en active
Non-Patent Citations (1)
Title |
---|
1. Крыль родины, № 3, 1989, с.9 2. Рекламный проспект фирмы Пзра- флайт (US) Система Пара-Пойнт - управл ема парашютна система, 1985. * |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
CA2392734A1 (en) | Multi-mode tiltrotor nacelle control system with integrated envelope protection | |
WO2000020273A3 (en) | Aircraft with removable structural payload module | |
CA2156510A1 (en) | Sequential selective operation of aircraft brakes | |
WO2000000387A3 (en) | Balloon trajectory control system | |
CA2113731A1 (en) | Automatic Turn Coordination Trim Control for Rotary Wing Aircraft | |
EP0092500A3 (en) | Helicopter engine torque compensator | |
RU1773804C (en) | Parachute system | |
CA2144453A1 (en) | Helicopter integrated fire and flight control having coordinated area bombing control | |
EP0273466A3 (en) | Aircraft | |
Key | Analysis of army helicopter pilot error mishap data and the implications for handling qualities | |
FR2379432A1 (en) | LANDING DEVICE FOR AUTOMATICALLY LANDING LOADS TO THE GROUND FROM AN AIRPLANE FLYING AT LOW ALTITUDE | |
RU1677982C (en) | Parachute | |
RU1821417C (en) | Helicopter system | |
CA2260960A1 (en) | Landing and take-off assembly for vertical take-off and landing and horizontal flight aircraft | |
RU1819797C (en) | Airship | |
RU93032526A (en) | MULTI-PUPPING PARASHCLE SYSTEM | |
RU1837035C (en) | Carrier system of vertical take-off and landing flying vehicle | |
EP0372660A3 (en) | Flight path angle command, flight control system for landing flare | |
Klass | Plans change on F-16 communications. | |
SEAGRAVES | Engineering and instrumentation support of GL Research Balloon Program(Final Report, 1 Dec. 1987- 10 Dec. 1989) | |
Reichert | Helicopter aeromechanics: Introduction and historical review | |
MAASS et al. | Flight control factors for a full-scale remotely piloted rotary wing target | |
Paccini | Air traffic control's application to vertical flight- An international perspective. | |
DIEKMANN et al. | Preliminary airworthiness evaluation of the Rutan Aircraft Factory(RAF), Incorporated LONG-EZ airplane[Final Report, 14 Jan.- 1 Apr. 1983] | |
ZIEMBA et al. | The SKY SHARK: An RPV designed to investigate the pressure distribution on a lifting surface(Final Design Proposal) |