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NTIS 바로가기국가/구분 | United States(US) Patent 등록 |
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국제특허분류(IPC7판) |
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출원번호 | US-0450116 (1999-11-26) |
발명자 / 주소 |
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인용정보 | 피인용 횟수 : 46 인용 특허 : 16 |
The system and method of this invention determines stress within the load bearing members of an aircraft, machine or structure in order to improve their design, safety and efficiency as well as enhancing their operation. Load or stress is calculated from signals generated in fasteners fitted with pi
1. In combination, an aircraft and a system for measuring dynamic stresses in the structure of said aircraft, said aircraft comprising a fuselage and a pair of wings attached thereto, said system comprising a plurality of fixed elements embedded in predetermined locations of said fuselage and said w
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