• Title/Summary/Keyword: Aircraft Brake System

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Commentary Study on Automatic Speedbrake Control System of B747-8 (B747-8 Automatic Speedbrake Control System에 대한 해석적 연구)

  • Moon, Bong Sup;Nam, MyongKwan;Choi, Youn Chul
    • Journal of the Korean Society for Aviation and Aeronautics
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    • v.26 no.3
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    • pp.40-47
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    • 2018
  • Reducing aircraft speed is the important task in the Rejected Takeoff and/or landing process. It is known that the effect of the Speedbrake is most important factor during the rejected takeoff maneuver in particular near V1 on the critical field length runway. The B747 designer created Automatic Speedbrake Control System to relieve pilot workload, improves brake operation and ensures proper Speedbrake operation for rejected take off. However, those who make the Rejected Takeoff procedure ignored the Automatic function and made it does all manual operations. This lets procedures difficult, complicated, and a cause of confusion and pilot error. This study was conducted to commentary the mechanism and function of the Automatic Speedbrake Control System of B747-8 and to propose appropriate B747-8 Rejected Take off procedures for its function to reduce the workload of pilots and contribute to reduce the possibility of pilot error during Rejected Takeoff.

On the Performance Test of the Piezoelectric-Hydraulic Pump (압전유압펌프 성능실험에 대한 연구)

  • Joo, Yong-Hwi;Hwang, Jai-Hyuk;Yang, Ji-Youn;Bae, Jae-Sung;Lee, Jong-Hoon;Kwon, Jun-Yong
    • Journal of the Korean Society for Aeronautical & Space Sciences
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    • v.43 no.9
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    • pp.822-829
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    • 2015
  • In this paper, the piezoelectric-hydraulic pump with a piezostack actuator as a driving source has been designed, fabricated, and evaluated for its application to UAV's brake system. The performance requirements of the piezoelectric-hydraulic pump were decided based on the requirements analysis of the target aircraft brake system. The geometric design of the piezoelectric-hydraulic pump to meet the performance requirements of the pump was conducted, and all components of the pump including the spring sheet type check valves were machined with close tolerance. By constructing a test apparatus for the performance check of the piezoelectric-hydraulic pump, the performance characteristics of the pump, such as the outlet flow rate for load-free condition and the outlet oil pressure for closed loop condition, have been evaluated. It has been found by the performance test result that the developed piezoelectric-hydraulic pump satisfies the design requirements effectively.