[특허]Method and system for flying an aircraft

Northrop Grumman Corporation

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*	검색어의 *란에 0개 이상의 임의의 문자가 포함된 문서 검색	예) semi*
""	따옴표 내의 구문과 완전히 일치하는 문서만 검색	예) "Transform and Quantization"

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Method and system for flying an aircraft

국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64D-011/00
미국특허분류(USC)	244/001.R; 244/001.R; 244/075.R; 244/118.5
출원번호	US-0406047 (2003-04-02)
발명자 / 주소	Clark, Walter D.
출원인 / 주소	Northrop Grumman Corporation
대리인 / 주소	Fulbright & Jaworski LLP
인용정보	피인용 횟수 : 5 인용 특허 : 10

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A method for flying an aircraft includes flying the aircraft at a first approximately level position and changing the flight of the aircraft from the first approximately level position to a climbing position. The method includes changing the flight of the aircraft from the climbing position to a second approximately level position to achieve a weightless state during the change to the second approximately level position and rolling the aircraft during the weightless state using one or more rolling control surfaces of the aircraft to establish a bank for ...

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1. A method for flying an aircraft, comprising:flying the aircraft at a first approximately level position;changing the flight of the aircraft from the first approximately level position to a climbing position;changing the flight of the aircraft from the climbing position to a second approximately level position to achieve a weightless state during the change to the second approximately level position;rolling the aircraft during the weightless state using one or more rolling control surfaces of the aircraft to establish a bank for a turn without creating adverse yaw; andwherein the aircraft does not include a deflectable spoiler, fin or rudder to counter adverse yaw. 2. The method of claim 1, wherein changing the flight of the aircraft from the first approximately level position to a climbing position comprises positively changing a pitch control device associated with the aircraft. 3. The method of claim 1, wherein changing the flight of the aircraft from the climbing position to a second approximately level position comprises negatively changing a pitch control device associated with the aircraft. 4. The method of claim 1, wherein the rolling control surfaces of the aircraft comprise elevons of the aircraft. 5. The method of claim 1, wherein the aircraft does not include a deflectable yaw device to counter adverse yaw. 6. A method for flying an aircraft, wherein each turn during flight comprises:flying the aircraft at a first approximately level position;changing the flight of the aircraft from the first approximately level position to a climbing position;changing the flight of the aircraft from the climbing position to a second approximately level position to achieve a weightless state during the change to the second approximately level position;rolling the aircraft during the weightless state using one or more rolling control surfaces of the aircraft to establish a bank for the turn without creating adverse yaw. 7. The method of claim 6, wherein the aircraft does not include a deflectable spoiler, fin or rudder. 8. The method of claim 6, wherein the aircraft does not include a deflectable yaw device to counter adverse yaw. 9. The method of claim 6, wherein changing the flight of the aircraft from the first approximately level position to a climbing position comprises positively changing a pitch control device associated with the aircraft. 10. The method of claim 6, wherein changing the flight of the aircraft from the climbing position to a second approximately level position comprises negatively changing a pitch control device associated with the aircraft. 11. The method of claim 6, wherein the rolling control surfaces of the aircraft comprise elevons of the aircraft. 12. A method for flying an aircraft, comprising:flying the aircraft at a first approximately level position;changing the flight of the aircraft from the first approximately level position to a descending position to achieve a weightless state during the change to the descending position;rolling the aircraft during the weightless state using one or more rolling control surfaces of the aircraft to establish a bank for a turn without creating adverse yaw;changing the flight of the aircraft from the descending position to a second approximately level position; andwherein the aircraft does not include a deflectable spoiler, fin or rudder to counter adverse yaw. 13. The method of claim 12, wherein changing the flight of the aircraft from the first approximately level position to a descending position comprises negatively changing a pitch control device associated with the aircraft. 14. The method of claim 12, wherein changing the flight of the aircraft from the descending position to a second approximately level position comprises positively changing a pitch control device associated with the aircraft. 15. The method of claim 12, wherein the rolling control surfaces of the aircraft comprise elevons of the aircraft. 16. The method of claim 12, wherein the aircraft does not include a deflectable yaw device to counter adverse yaw. 17. A system for flying an aircraft, comprising:a control module coupled to one or more control surfaces of the aircraft, the control module operable to:change the flight of the aircraft from a first approximately level position to a climbing position;change the flight of the aircraft from the climbing position to a second approximately level position to achieve a weightless state during the change to the second approximately level position;roll the aircraft during the weightless state using the one or more rolling control surfaces to establish a bank for a turn without creating adverse yaw; andwherein the aircraft does not include a deflectable spoiler, fin or rudder to counter adverse yaw. 18. The system of claim 17, wherein the rolling control surfaces of the aircraft comprise elevons of the aircraft.

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Method and system for flying an aircraft

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Method and system for flying an aircraft

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이 특허에 인용된 특허 (10)

이 특허를 인용한 특허 피인용횟수: 5

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