Patent ID: 11932424
Assignee: ROMAN NAWOJCZYK
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 3:
4. The system according to claim 1,
wherein each pushing mechanism comprises:
a C-shaped beam;
a linear actuator;
a vertical low bar; and
the blocking bar having the T-groove;
wherein each pushing mechanism is installed inside the space rocket fuselage, and over each spreadable-arm;
wherein inside each C-shaped beam is slidingly installed the blocking bar;
wherein each blocking bar is permanently fastened by the vertical low bar with the linear actuator;
wherein each linear actuator is adapted for pushing and pulling the blocking bar;
wherein each blocking bar has the T-groove which is adapted to fit with the T-bar on the middle beam in the spreadable arm;
wherein said blocking bar is configured to block the middle beam in all directions once the spreadable arm is entirely lifted;
wherein the blocking bar fulfills blocking function when it is maximally slid outside the fuselage;
wherein the blocking bar causes that the middle beam after its blocking gains possibility of carrying burdens in all directions.