FIELD: aircraft and rocket equipment.
SUBSTANCE: invention relates to the field of aircraft and rocket equipment, and more specifically to the docking compartments of aircraft compartments. Method of compartment joining includes installation of sealing seal on flanges of mating compartments. Parts to be jointed are made in the form of rig frames. Flange with the possibility of rotation relative to the longitudinal axis is installed on one of the frames and is made in the form of a disk with grippers distributed along the diameter. It is possible to fix slides from displacement in direction of disc grips at inclined surfaces thrust.
EFFECT: enabling higher reliability.
1 cl, 7 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| ASSEMBLY FOR COMPARTMENTS JOINING | 2020 |
|
RU2738623C1 |
| METHOD FOR MANUFACTURING A MULTI-LINK COMPARTMENT DOCKING UNIT | 2022 |
|
RU2778585C1 |
| MULTI-LEVER COMPARTMENT DOCKING SYSTEM | 2022 |
|
RU2792950C1 |
| PAYLOAD RESET SYSTEM | 2021 |
|
RU2771907C1 |
| METHOD FOR MANUFACTURING A SYSTEM OF SEPARATION OF STRUCTURAL ELEMENTS | 2021 |
|
RU2763219C1 |
| METHOD FOR SECURING AND DETACHING PAYLOAD | 2021 |
|
RU2769847C1 |
| HYDRODYNAMIC SYSTEM OF SEPARATION OF STRUCTURAL ELEMENTS | 2021 |
|
RU2754611C1 |
| PAYLOAD ATTACHMENT AND SEPARATION SYSTEM | 2021 |
|
RU2764879C1 |
| METHOD FOR SEPARATING ROCKET SECTIONS | 2021 |
|
RU2754612C1 |
| METHOD FOR MANUFACTURING THE ROCKET STAGE SEPARATION SYSTEM | 2021 |
|
RU2763222C1 |
