FIELD: aircraft engineering.
SUBSTANCE: proposed method consists in detention of compartment fastener and making push-off device act on contact surface of thrust element of separable compartment towards its centre of gravity. Compartment is acted upon with free fluctuation displacement of contact spot of interaction between push rod and thrust element contact surface at fluctuation change of the angle of compartment frame inclination to push rod. Note here that before separation hardness of thrust element material is higher than that of push rod. Note also that in separation separable compartment thrust element represents a section of sphere with geometrical centre located at the separable compartment centre of gravity.
EFFECT: decreased dynamic load on separable compartment.
2 cl, 1 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AIRCRAFT COMPARTMENT SEPARATION SYSTEM (VERSIONS) | 2012 |
|
RU2524755C2 |
| AIRCRAFT COMPARTMENT SEPARATION SYSTEM | 2016 |
|
RU2651780C1 |
| SYSTEM AND METHOD FOR AERIAL VEHICLE COMPARTMENT SEPARATION | 2020 |
|
RU2762186C1 |
| DEVICE TO FASTEN CARGO IN AND DROP FREE IT FROM AIRCRAFT | 2009 |
|
RU2402460C1 |
| METHOD OF SEPARATION OF THE GROUP OF UNMANNED AERIAL VEHICLES FROM THE AIRCRAFT PLANER | 2017 |
|
RU2664812C1 |
| DEVICE FOR SEPARATING UNMANNED AERIAL VEHICLES FROM CARRIER AIRCRAFT | 2017 |
|
RU2672706C1 |
| SYSTEM FOR SEPARATING ROCKET STAGES | 2021 |
|
RU2771868C1 |
| HYDRODYNAMIC SYSTEM OF SEPARATION OF STRUCTURAL ELEMENTS | 2021 |
|
RU2754611C1 |
| UNMANNED AERIAL VEHICLE | 2020 |
|
RU2727770C1 |
| METHOD FOR UNMANNED AERIAL VEHICLE FLIGHT TO ALTITUDE FLIGHT PATH | 2020 |
|
RU2727363C1 |
