Invention Grant
US07658669B2 Aircraft cabin pressure controls with an open-loop motor control system: non-linear control law logic to compensate for excessive motor loads or motor degradation 有权
飞机舱压力控制与开环电机控制系统:非线性控制律逻辑,以补偿过大的电机负载或电机退化

  • Patent Title: Aircraft cabin pressure controls with an open-loop motor control system: non-linear control law logic to compensate for excessive motor loads or motor degradation
  • Patent Title (中): 飞机舱压力控制与开环电机控制系统:非线性控制律逻辑,以补偿过大的电机负载或电机退化
  • Application No.: US11673100
    Application Date: 2007-02-09
  • Publication No.: US07658669B2
    Publication Date: 2010-02-09
  • Inventor: Gerard L. McCoy
  • Applicant: Gerard L. McCoy
  • Applicant Address: US NJ Morristown
  • Assignee: Honeywell International Inc.
  • Current Assignee: Honeywell International Inc.
  • Current Assignee Address: US NJ Morristown
  • Agent Oral Caglar, Esq.
  • Main IPC: B64D13/02
  • IPC: B64D13/02
Aircraft cabin pressure controls with an open-loop motor control system: non-linear control law logic to compensate for excessive motor loads or motor degradation
Abstract:
A cabin pressure control system (CPCS) software control logic modification may boost the voltage applied to a motor when conditions are sensed indicating a combination of larger than normal cabin pressure and cabin rate error conditions. The motor may be part of an open-loop system for operating a butterfly valve that may regulate outflow from the aircraft cabin. The larger than normal cabin pressure and cabin rate error conditions may be an indication that the outflow valve is not responding in a normal manner, potentially caused by excessive loading to the motor or motor degradation. By boosting the motor voltage during excessive load conditions or with a degraded motor, CPCS performance and robustness may be improved.
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