The part 23 airworthiness standards for small airplanes states minimal standards of the emergency condition for the occupant protection. Under this regulation, the airplane must be designed and certified about static ...The part 23 airworthiness standards for small airplanes states minimal standards of the emergency condition for the occupant protection. Under this regulation, the airplane must be designed and certified about static strength of the fuselage and seats, horizontal and vertical dynamic strength of seats. Human injuries in dynamic crash tests and the survivability in the turnover condition should be also evaluated. The most important part among injuries of human is a head and the head injury is evaluated by Head Injury Criterion （HIC）. KC-100, 4 seats airplane that is manufactured by KAI, was conducted seat dynamic tests. The HIC from tests was well within criteria limits 1,000 and the occupant compartment for head protection provided hazard-free spaces in the occupant＇s head strike envelope for the frontal-horizontal crash impacts. The airplane also was conducted a turnover static test and analysis to especially show living spaces of the head. The airframe could sustain living spaces for occupants in the turnover condition and occupants could escape and be protected. The results of tests and analysis corresponded to the criteria and proved the retention of survivable space in emergency landing condition.展开更多
Mars is one of the most valuable planets for space exploration.After entering the entry descent and landing(EDL)phase,the spacecraft would carry out a series of procedural deceleration operations and achieve soft land...Mars is one of the most valuable planets for space exploration.After entering the entry descent and landing(EDL)phase,the spacecraft would carry out a series of procedural deceleration operations and achieve soft landing on the surface of Mars.In the process of EDL,the landing platform would encounter a series of irreversible incidents within environmental unpredictability,making this process highly risky.The emergency communication device plays an important role if in the Mars Exploration Program.It can capture and store key dynamic parameters during EDL phase,enabling a high probability of survival in the occurrence of a faulty condition.It can also send the stored data to the Mars obit probe when the communication condition is met.This paper presents a scheme design for the emergency communication device based on its functionality and performance requirements.It includes the design proposal,simulation results,reliability analysis,technical risks and control measures,inheritance and performance compliance which verifies the rationality and correctness of the design.展开更多
文摘The part 23 airworthiness standards for small airplanes states minimal standards of the emergency condition for the occupant protection. Under this regulation, the airplane must be designed and certified about static strength of the fuselage and seats, horizontal and vertical dynamic strength of seats. Human injuries in dynamic crash tests and the survivability in the turnover condition should be also evaluated. The most important part among injuries of human is a head and the head injury is evaluated by Head Injury Criterion （HIC）. KC-100, 4 seats airplane that is manufactured by KAI, was conducted seat dynamic tests. The HIC from tests was well within criteria limits 1,000 and the occupant compartment for head protection provided hazard-free spaces in the occupant＇s head strike envelope for the frontal-horizontal crash impacts. The airplane also was conducted a turnover static test and analysis to especially show living spaces of the head. The airframe could sustain living spaces for occupants in the turnover condition and occupants could escape and be protected. The results of tests and analysis corresponded to the criteria and proved the retention of survivable space in emergency landing condition.
文摘Mars is one of the most valuable planets for space exploration.After entering the entry descent and landing(EDL)phase,the spacecraft would carry out a series of procedural deceleration operations and achieve soft landing on the surface of Mars.In the process of EDL,the landing platform would encounter a series of irreversible incidents within environmental unpredictability,making this process highly risky.The emergency communication device plays an important role if in the Mars Exploration Program.It can capture and store key dynamic parameters during EDL phase,enabling a high probability of survival in the occurrence of a faulty condition.It can also send the stored data to the Mars obit probe when the communication condition is met.This paper presents a scheme design for the emergency communication device based on its functionality and performance requirements.It includes the design proposal,simulation results,reliability analysis,technical risks and control measures,inheritance and performance compliance which verifies the rationality and correctness of the design.
