FIELD: aerospace technology.
SUBSTANCE: invention relates to the field of aviation and rocket technology. The system of attachment and separation of the payload contains a frame (1) of the supporting structure (2) and a frame (3) of the payload (4), mechanical locks (8). Each lock (8) has a rotary link mounted on the axis of rotation, separating the rotary link into the grip shoulder and the stop shoulder, and a locking link. The rod of the locking link and the body of each lock are equipped with stops with springs between them. The locking device is made in the form of a threaded hole in the grip arm and a bolt screwed into the threaded hole. The device for fixing mechanical locks contains metal cables (14), corresponding with the number of mechanical locks (8).
EFFECT: increase in the operability of the system under heavy loads is achieved, as well as simplification of the manufacture and layout of the aircraft and the reduction of aerodynamic drag.
9 cl, 10 dwg
Title | Year | Author | Number |
---|---|---|---|
METHOD FOR SECURING AND DETACHING PAYLOAD | 2021 |
|
RU2769847C1 |
DEVICE FOR SPACE APPARATUS SEPARATION | 2010 |
|
RU2453481C1 |
CARRIER ROCKET LARGE-SIZE DETACHABLE NOSE CONE | 2010 |
|
RU2424953C1 |
HYDRODYNAMIC SYSTEM OF SEPARATION OF STRUCTURAL ELEMENTS | 2021 |
|
RU2754611C1 |
METHOD OF FASTENING AND AUTOMATIC SEPARATION OF PAYLOAD OF UNMANNED AERIAL VEHICLE | 2023 |
|
RU2818007C1 |
METHOD FOR MANUFACTURING A SYSTEM OF SEPARATION OF STRUCTURAL ELEMENTS | 2021 |
|
RU2763219C1 |
DEVICE FOR FASTENING AND AUTOMATIC SEPARATION OF PAYLOAD OF UNMANNED AERIAL VEHICLE | 2023 |
|
RU2817228C1 |
METHOD FOR UAV PAYLOAD MOUNT | 2022 |
|
RU2784846C1 |
PAYLOAD SEPARATION SYSTEM | 2009 |
|
RU2396191C1 |
CREW SEAT WITH PARACHUTE PAN (VERSIONS) | 2014 |
|
RU2583102C2 |
Authors
Dates
2022-01-24—Published
2021-04-09—Filed