FIELD: aircraft engineering.
SUBSTANCE: claimed parachute consists of two blades arranged at the angle of attack to the flow running from below and connected with the cargo by slings interconnected by the permanent flexible fasteners and by one controlled unfastening joint. Every blade is symmetric about its centre while the length of slings arranged in symmetric about said centre are equal in pairs. After opening said parachute lowers neutrally with the revolution of blades. The parachute can be changed into gliding by unlocking of said controlled joint. In compliance with the other version, the parachute is provided with two unlocking fasteners.
EFFECT: higher safety of landing.
9 cl, 5 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| SPINNING PARACHUTE WITH TWO-STAGE BRAKING | 2014 |
|
RU2569991C1 |
| TWO-POSITION ELECTROTHERMOMECHANICAL LOCKING CARABINER FOR PARACHUTES WITH ADJUSTABLE DESCENT RESISTANCE | 2016 |
|
RU2634890C1 |
| ROTATING PARACHUTE CONTROL SYSTEM | 2013 |
|
RU2526113C1 |
| PARACHUTING SYSTEM - 4 AND METHOD FOR OPERATION THEREOF | 2014 |
|
RU2576852C1 |
| PARACHUTING SYSTEM AND METHOD OF ITS OPERATION | 2013 |
|
RU2527633C1 |
| AIRCRAFT HIGH-SPEED PARACHUTE RESCUE SYSTEM | 2023 |
|
RU2807767C1 |
| INTERPOSITION CARABINER (VERSIONS) | 2015 |
|
RU2611332C1 |
| AIRCRAFT RESCUE SYSTEM | 1990 |
|
RU2018466C1 |
| SEPARATE CARABINER - 3 | 2018 |
|
RU2679877C1 |
| GLIDING-TYPE PARACHUTE | 1996 |
|
RU2094324C1 |
