FIELD: parachute technique. SUBSTANCE: device has rod 1 made in form of polymer shaft 2 or tube; one end of shaft or tube is cut at angle of 45 deg and other end is connected with metal adapter bush 4 by means of thread, for example. Adapter bush 4 is pressed in ear 5 which is provided with hole 6 for mounting pins 7 securing rod 1. Line 8 is secured to ear 5. When line 8 is loaded, force is transmitted to rod 1 through ear 5 and pressed-in adapter bush 4. Rod 1 gets disengaged from balance of device, thus placing it in operation. EFFECT: enhanced reliability and facilitated manufacture. 2 cl, 2 dwg
Title | Year | Author | Number |
---|---|---|---|
DEVICE FOR PARACHUTE DEPLOYMENT | 1992 |
|
RU2040440C1 |
PARACHUTE DEPLOYMENT DEVICE | 1997 |
|
RU2112709C1 |
PARACHUTE DEPLOYMENT DEVICE | 1992 |
|
RU2033946C1 |
PARACHUTE OPENING DEVICE | 1991 |
|
RU2024420C1 |
ELECTRONIC PARACHUTE ACCIDENT PREVENTION SYSTEM | 2020 |
|
RU2741151C1 |
ELECTRONIC SAFETY PARACHUTE DEVICE | 2019 |
|
RU2719700C1 |
DEVICE TO OPEN PARACHUTE | 1988 |
|
RU2023632C1 |
PARACHUTE DEPLOYMENT DEVICE | 1990 |
|
RU1793646C |
METHOD TO EJECT A PILOT FROM AN AIRCRAFT AND DEVICE FOR ITS IMPLEMENTATION | 2016 |
|
RU2621133C1 |
AUTOMATIC UNCOUPLER | 0 |
|
SU1773805A1 |
Authors
Dates
1995-07-25—Published
1991-10-14—Filed