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) | B64C-001/16 B64C-009/12 |
미국특허분류(USC) | 244/13 ; 244/90R ; 244/135R ; 244/130 |
출원번호 | US-0613862 (1984-05-23) |
발명자 / 주소 | |
출원인 / 주소 | |
인용정보 | 피인용 횟수 : 20 인용 특허 : 0 |
A fixed wing powered light aircraft has a fuselage formed by laterally spaced longitudinal tubular booms supporting a twin vertical stabilizer and rudder assembly and a horizontal stabilator. A tubular framework pylon structure is secured to the fuselage booms for supporting a propulsion engine driving a propeller arranged in a pusher configuration. An open cockpit is partially shrouded by a streamlined nose cowl and longitudinal cockpit side panels which meet along the longitudinal center line aft of the pylon. Two piece removable wing root fairings min...
A fixed wing powered light aircraft characterized by: a fuselage including two elongated spaced apart tubular booms extending from a forward end of said fuselage to an aft end and interconnected by spaced apart laterally extending brace members; a pylon structure secured to said booms and constructed for supporting a propulsion engine and propellar means drivenly connected to said propulsion engine, said pylon structure comprising a tubular frame and including engine mount means secured to said frame for supporting said engine; a cockpit disposed forward...