Patent ID: 11891026
Assignee: KING FAISAL UNIVERSITY
Field: Transport (Mechanical engineering)
Classification: CPC B | IPC B

Claim 8:
9. A reverse thrust braking method, comprising:
receiving air at an inlet of a system having propeller fan blades;
accelerating the air coming into the system with the propeller fan blades;
receiving the air accelerated by the propeller fan blades through a plurality of linearly arranged chambers, wherein each of the plurality of linearly arranged chambers is downstream of the system having the propeller fan blades;
receiving air from at least one of the plurality of chambers at an exit point; and
exhausting the air from the exit point at an angle to create a reverse thrust without combustion,
wherein the air is accelerated through a plurality of bars, each of the plurality of bars located between any adjacent two chambers of the plurality of chambers.