ANALISIS KEMAMPUAN SISTEM HIDROLIK PADA FLIGHT
CONTROL PESAWAT TM-13 DENGAN KAPASITAS PENUMPANG 85-
189
Total View This Week0
Total View This Week0
Institusion
INSTITUT TEKNOLOGI DIRGANTARA ADISUTJIPTO
Author
RIYAMIRAD, YONGKY
Subject
T Technology (General)
Datestamp
2024-07-02 04:00:22
Abstract :
The hydraulic system of an aircraft or hydraulic power system is a system on aircraft that uses the pressure of liquid (hydraulic) as a medium. Hydraulic systems are used to drive the system associated with other components, such as driving ground spoilers, flight spoilers, leanding gear, nose gear steering, trailing edge flaps, leading edge devices, ailerons, elevators, leanding gear brakes, rudder and thrust reversers. The study was conducted to find out the hydraulic power produced and the hydraulic minimum pressure needed for the flight control on TM13 aircraft. This research was conducted using the literature study method by collecting data from the A340 aircraft to be applied in the TM13 aircraft. Load calculation was done on ailerons, elevators, and rudder. The results showed that the load produced in the aileron was 36.93 KW, elevator was 373.8 KW, and rudder was 77.27 KW. The minimum hydraulic pressure required by the aileron actuator was 1960 psi, elevator actuator was 1964 psi, and rudder actuator was 1785 psi.
The hydraulic system of an aircraft or hydraulic power system is a system on aircraft that uses the pressure of liquid (hydraulic) as a medium. Hydraulic systems are used to drive the system associated with other components, such as driving ground spoilers, flight spoilers, leanding gear, nose gear steering, trailing edge flaps, leading edge devices, ailerons, elevators, leanding gear brakes, rudder and thrust reversers. The study was conducted to find out the hydraulic power produced and the hydraulic minimum pressure needed for the flight control on TM13 aircraft. This research was conducted using the literature study method by collecting data from the A340 aircraft to be applied in the TM13 aircraft. Load calculation was done on ailerons, elevators, and rudder. The results showed that the load produced in the aileron was 36.93 KW, elevator was 373.8 KW, and rudder was 77.27 KW. The minimum hydraulic pressure required by the aileron actuator was 1960 psi, elevator actuator was 1964 psi, and rudder actuator was 1785 psi.
Download
book
BibTex
Latex, Jabref
cloud_download
Original Resource
url resource Institution
