검색연산자 | 기능 | 검색시 예 |
---|---|---|
() | 우선순위가 가장 높은 연산자 | 예1) (나노 (기계 | machine)) |
공백 | 두 개의 검색어(식)을 모두 포함하고 있는 문서 검색 | 예1) (나노 기계) 예2) 나노 장영실 |
| | 두 개의 검색어(식) 중 하나 이상 포함하고 있는 문서 검색 | 예1) (줄기세포 | 면역) 예2) 줄기세포 | 장영실 |
! | NOT 이후에 있는 검색어가 포함된 문서는 제외 | 예1) (황금 !백금) 예2) !image |
* | 검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색 | 예) semi* |
"" | 따옴표 내의 구문과 완전히 일치하는 문서만 검색 | 예) "Transform and Quantization" |
국가/구분 | United States(US) Patent 등록 |
---|---|
국제특허분류(IPC7판) | B64D-037/12 |
미국특허분류(USC) | 244/135R ; 244/140 |
출원번호 | US-0253087 (1981-04-13) |
발명자 / 주소 | |
인용정보 | 피인용 횟수 : 10 인용 특허 : 1 |
A dropable main fuel tank that comprises a portion of an aircrafts lower fuselage or part of the wing structure contains all nonessential fuel for takeoff or landing. Airfoils, parachute, or rocket motor built into the main fuel tank will separate the main fuel tank from the aircraft quickly when dropped or released in a possible crash situation, thus preventing the aircraft from being consumed by its own nonessential fuel in a crash. A nondroppable auxiliary fuel tank on the aircraft will sustain the aircraft after the main fuel tank has been dropped. T...
An aircraft comprising wings, fuselage, auxiliary fuel tanks on the wings and a main dropout fuel tank releasably mounted on and forming a portion of said aircraft and having catapulting means mounted on said main dropout fuel tank; horizontal track means on said aircraft for mounting said main dropable tank and running longitudinally of said aircraft, said catapulting means mounted on said main tank for ejecting said main tank rearwardly along said track means, said catapulting means being operated from the pilot\s cabin and comprising airfoils pivotall...