AbstractOne approach based on AC20-128A is presented in order to assess the risk caused by uncontained engine rotor failure (UERF). In this approach, the risk assessment procedure includes hazard identification and hazard quantification. In the step of hazard identification, the catastrophic functional hazards, derived from the functional hazard analysis (FHA) results for the airplane, are used as the top events to construct the fault trees. The minimal cut sets (MSCs) of the fault trees are the hazards to be identified exactly. In the step of hazard quantification, the probability of one hazard triggered by some uncontained debris is evaluated. After the probabilities of all the identified hazards are quantified, the risk assessment of the...
Failure mode and effects analysis is an important methodology, which has been extensively used to ev...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Sections of the U.S. Airworthiness Standards which contribute to rotor integrity are explored. Repor...
AbstractThe safety design is very important to civil aircraft. In order to verify the civil aircraft...
AbstractThis paper sets forth a method of compliance with the requirements of CCAR 25.901(d) and 25....
Throughout the life cycle of an aircraft, it is likely that it may encounter an uncontained engine r...
AbstractThe potential hazard resulting from uncontained turbine engine rotor blade failure has alway...
AbstractThe risk simulation model of aero engine failure has been developed based on Monte Carlo met...
More realistic guideline data must be developed for use in aircraft design in order to comply with r...
Risk assessment methods are widely used in aviation, but have not been demonstrated for visual inspe...
Presented at AIAA Aviation 2019 Forum (AIAA 2019-3123)Novel architectures and technologies carry wit...
FAA Technical Library2021PDFTech ReportPhifer, EllenSURVICE EngineeringNaval Air Warfare Center (U.S...
Airworthiness certification of commercial transport aircraft requires a safety analysis of the prop...
An airplane is a highly engineered system incorporating control- and feedback-loops which often, and...
AbstractThe potential hazard resulting from an uncontained turbine engine rotor blade failure has al...
Failure mode and effects analysis is an important methodology, which has been extensively used to ev...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Sections of the U.S. Airworthiness Standards which contribute to rotor integrity are explored. Repor...
AbstractThe safety design is very important to civil aircraft. In order to verify the civil aircraft...
AbstractThis paper sets forth a method of compliance with the requirements of CCAR 25.901(d) and 25....
Throughout the life cycle of an aircraft, it is likely that it may encounter an uncontained engine r...
AbstractThe potential hazard resulting from uncontained turbine engine rotor blade failure has alway...
AbstractThe risk simulation model of aero engine failure has been developed based on Monte Carlo met...
More realistic guideline data must be developed for use in aircraft design in order to comply with r...
Risk assessment methods are widely used in aviation, but have not been demonstrated for visual inspe...
Presented at AIAA Aviation 2019 Forum (AIAA 2019-3123)Novel architectures and technologies carry wit...
FAA Technical Library2021PDFTech ReportPhifer, EllenSURVICE EngineeringNaval Air Warfare Center (U.S...
Airworthiness certification of commercial transport aircraft requires a safety analysis of the prop...
An airplane is a highly engineered system incorporating control- and feedback-loops which often, and...
AbstractThe potential hazard resulting from an uncontained turbine engine rotor blade failure has al...
Failure mode and effects analysis is an important methodology, which has been extensively used to ev...
A program to develop criteria for the design of devices that will be used on aircraft to protect pas...
Sections of the U.S. Airworthiness Standards which contribute to rotor integrity are explored. Repor...