[특허]Vertical takeoff and landing aircraft

The Boeing Company

검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
검색연산자

검색도움말
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"

과학기술 지식인프라 ScienceON

연합인증

연합인증 가입 기관의 연구자들은 소속기관의 인증정보(ID와 암호)를 이용해 다른 대학, 연구기관, 서비스 공급자의 다양한 온라인 자원과 연구 데이터를 이용할 수 있습니다.

이는 여행자가 자국에서 발행 받은 여권으로 세계 각국을 자유롭게 여행할 수 있는 것과 같습니다.

연합인증으로 이용이 가능한 서비스는 NTIS, DataON, Edison, Kafe, Webinar 등이 있습니다.

한번의 인증절차만으로 연합인증 가입 서비스에 추가 로그인 없이 이용이 가능합니다.

다만, 연합인증을 위해서는 최초 1회만 인증 절차가 필요합니다. (회원이 아닐 경우 회원 가입이 필요합니다.)

연합인증 절차는 다음과 같습니다.

최초이용시에는
ScienceON에 로그인 → 연합인증 서비스 접속 → 로그인 (본인 확인 또는 회원가입) → 서비스 이용

그 이후에는
ScienceON 로그인 → 연합인증 서비스 접속 → 서비스 이용

연합인증을 활용하시면 KISTI가 제공하는 다양한 서비스를 편리하게 이용하실 수 있습니다.

특허 상세정보

MyON담기

내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Vertical takeoff and landing aircraft

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64D-027/20
미국특허분류(USC)	244/023.B; 244/023.A; 244/055; 244/058
출원번호	US-0829743 (2004-04-22)
발명자 / 주소	Ouellette, Richard P. Kutzmann, Aaron J.
출원인 / 주소	The Boeing Company
대리인 / 주소	Harness Dickey &
인용정보	피인용 횟수 : 0 인용 특허 : 12

초록
▼

A flight capable mobile platform adapted for covert deployment is provided. The mobile platform is additionally adapted to have a reduced vulnerability to hostile detection and aggression. The mobile platform includes a fuselage having a pair of sidewalls and a bottom. The sidewalls and bottom form an armored payload bay. The mobile platform additionally includes a pair of wings connected to the fuselage. The wings have a fixed wingspan constructed such that the mobile platform can be transported by a larger second mobile platform. This allows for the mobile platform to be aerial deployed from the larger second mobile platform. Each of the sidewalls include at least one pulse ejector thrust augmentor (PETA) bank that is canted outward. Therefore, thrust exhaust produced by each PETA bank is directed down and away from a centerline of the payload bay. Furthermore, the bottom of the mobile platform is adapted to allow ingress and egress of cargo, e.g. military troops, from the payload bay.

대표
청구항
▼

1. A flight capable said mobile platform, said mobile platform comprising:a fuselage adapted to form an armored payload bay including a portion adapted to allow at least one of ingress and egress of cargo into, or from, the payload bay, the fuselage being constructed to reduce the vulnerability of cargo in the armored payload bay to hostile detection of and aggression;a pair of wings connected to the fuselage; anda pulse ejector thrust augmentor (PETA) bank disposed within the fuselage, the PETA bank including a plurality of interconnected pulsejets and oriented such that a thrust exhaust produced by the bank is directed downwardly and laterally outward from a centerline of the payload bay.2. The mobile platform of claim 1, wherein the fight capable mobile platform comprises a vertical take off and landing (VTOL) aircraft.3. The mobile platform of claim 1, wherein the wings comprise a non-alterable wingspan such that the mobile platform can be transported by and deployed from a second mobile platform when the second mobile platform is airborne.4. The mobile platform of claim 1, wherein the wings are adapted to be moved between a first position and a second position such that the mobile platform forms a reduced cross sectional footprint with the wings in the second position.5. The mobile platform of claim 1, wherein the fuselage comprises a pair of sidewall including a plurality of layers adapted to provide an interior area of the payload bay protection from infiltration by flying objects.6. The mobile platform of claim 5, wherein the plurality of layers include an outer skin of each sidewall.7. The mobile platform of claim 5, wherein the plurality of layers include an integral storage compartment formed in each sidewall.8. The mobile platform of claim 5, wherein the plurality of layers include an outer side panel of the PETA bank.9. The mobile platform of claim 5, wherein the plurality of layers include a plurality of pulsejet engines included in the PETA bank.10. The mobile platform of claim 5, wherein the plurality of layers include an inner side panel of the PETA bank.11. The mobile platform of claim 5, wherein the plurality of layers include a layer of acoustical insulation included in each sidewall.12. The mobile platform of claim 5, wherein the plurality of layers include a payload bay panel included in each sidewall.13. The mobile platform of claim 5, wherein an exterior surface of each sidewall is adapted to be canted to reduce radar cross section side sector returns.14. The mobile platform of claim 1, wherein the fuselage includes long, aligned edges adapted to reduce radar cross section returns.15. The mobile platform of claim 1, further comprising a cruise propulsion system disposed within an interior portion of the fuselage to reduce radar cross section returns and acoustical detection.16. The mobile platform of claim 15, wherein the cruise propulsion system includes a high efficiency, high bypass turbofan adapted to cool an exhaust from the cruise propulsion system to reduce infrared detection.17. The mobile platform of claim 1, wherein the fuselage includes a lower aft deck adapted to reduce infrared detection.18. The mobile platform of claim 1, wherein the PETA bank includes at least one absorber adapted to narrow an acoustical bandwidth of noise generated by the PETA bank and thereby reduce acoustical detection.19. The mobile platform of claim 1, wherein the fuselage and wings include a camouflage scheme adapted to reduce visual detection.20. A flight capable mobile platform adapted for enhanced protection against hostile detection and aggression, said mobile platform comprising:a pair of wings adapted to allow the mobile platform to be transported within a larger airborne second mobile platform;an armored payload bay formed within a fuselage of the mobile platform, the armored payload bay including:a pair of armored sidewall, each armored sidewall including an exterior surface canted such that top portions of the exterior surfaces are in closer proximity to each other than bottom portions of the exterior surfaces to reduce radar cross section returns, andan armored bottom adapted to allow ingress and egress of cargo from the payload bay; andat least one pulse ejector thrust augmentor (PETA) bank disposed within each sidewall, each PETA bank including a plurality of interconnected pulsejets and adapted to cant outward such that a thrust exhaust produced by each PETA bank is directed down and outwardly away from a centerline of the payload bay.21. The mobile platform of claim 20, wherein the flight capable mobile platform comprises a vertical take off and landing (VTOL) aircraft.22. The mobile platform of claim 20, wherein the wings are adapted to have a fixed wingspan to allow the mobile platform to be transported within, and deployed from, the larger second mobile platform while the larger second mobile platform is airborne.23. The mobile platform of claim 20, wherein the wings are adapted to be moved between a first position and a second position so that the mobile platform can be transported within the larger second mobile platform to a remote ground location with the wings in the second position.24. The mobile platform of claim 20, wherein each armored wall comprises a plurality of protective layers adapted to protect an interior area of the payload bay from infiltration by flying objects, the protective layers including at least two of the following:an outer skin of each sidewall;an integral storage compartment formed in each sidewall;a protective outer side panel of each PETA bank;a plurality of PETA propulsion devices included in each PETA bank;a protective inner side panel of each PETA bank;a layer of acoustical insulating included in each sidewall; anda payload bay panel included in each sidewall.25. The mobile platform of claim 20, wherein the fuselage includes long, aligned edges adapted to reduce radar cross section returns.26. The mobile platform of claim 20 further comprising a cruise propulsion system disposed within an interior portion of the fuselage to reduce radar cross section returns and acoustical detection.27. The mobile platform of claim 26, wherein the cruise propulsion system includes a high efficiency, high bypass turbofan adapted to cool an exhaust from the cruise propulsion system to reduce infrared detection.28. The mobile platform of claim 20, wherein the fuselage includes a lower aft deck adapted to reduce infrared detection.29. The mobile platform of claim 20, wherein each PETA bank includes at least one absorber adapted to narrow an acoustical bandwidth of noise generated by each pulsejets and thereby reduce acoustical detection.30. The mobile platform of claim 20, wherein the fuselage and wings include a camouflage scheme adapted to reduce visual detection.31. A flight capable mobile platform adapted for reduced vulnerability to hostile detection of and aggression, said mobile platform comprising:a fuselage having an armored bottom and a pair of armored sidewalls that include a plurality of protective layers adapted to protect an interior area of a payload bay from infiltration by flying objects, the armored bottom adapted to allow ingress and egress of cargo from the payload bay;a pair of fixed wings connected to the fuselage, the wings having a non-alterable wingspan adapted to allow the mobile platform to be transported within, and deployed from, a larger airborne second mobile platform; anda plurality of pulse ejector thrust augmentor (PETA) banks including a plurality of interconnected pulsejets, wherein at least one PETA bank is disposed within each sidewall and canted outward such that a thrust exhaust produced by each bank is directed down and outwardly away from a centerline of the payload bay;wherein an exterior surface of each sidewall is canted such that top portions of the exterior surfaces are in closer proximity to each other than bottom portions of the exterior surfaces to reduce radar cross section returns.32. The mobile platform of claim 31, wherein the flight capable mobile platform comprises a vertical take off and landing (VTOL) aircraft.33. The mobile platform of claim 31, wherein the plurality of layers includes at least two of:an outer skin of each sidewall;an integral storage compartment disposed in each sidewall;an outer side panel of each PETA bank;a plurality of PETA propulsion devices included in each PETA bank;an inner side panel of each PETA bank;a layer of acoustical insulating included in each sidewall; anda payload bay panel included in each sidewall.34. The mobile platform of claim 31, wherein a plurality of major break lines in an exterior surface of the mobile platform includes long, aligned edges adapted to reduce radar cross section returns.35. The mobile platform of claim 31 further comprising a cruise propulsion system located within an interior portion of the fuselage to reduce radar cross section returns and acoustical detection.36. The mobile platform of claim 35, wherein the cruise propulsion system includes a high efficiency, high bypass turbofan to cool exhaust from the cruise propulsion system and thereby reduce infrared detection.37. The mobile platform of claim 31, wherein the fuselage includes a lower aft deck adapted to reduce infrared detection.38. The mobile platform of claim 31, wherein each PETA bank includes at least one absorber adapted to narrow an acoustical bandwidth of noise generated by each pulsejets and thereby reduce acoustical detection.39. The mobile platform of claim 31, wherein the fuselage and wings include a camouflage scheme to reduce visual detection.

이 특허에 인용된 특허 (12)

IPC 상위 출원인

내보내기

상세정보
내보내기 구분	파일저장 인쇄 메일전송
구성항목	관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표IPC 관리번호, 국가코드, 자료구분, 상태, 출원번호, 출원일자, 공개번호, 공개일자, 공고번호, 공고일자, 등록번호, 등록일자, 발명명칭(한글), 발명명칭(영문), 출원인(한글), 출원인(영문), 출원인코드, 대표출원인, 출원인국적, 출원인주소, 발명자, 발명자E, 발명자코드, 발명자주소, 발명자 우편번호, 발명자국적, 대표IPC, IPC코드, 요약, 미국특허분류, 대리인주소, 대리인코드, 대리인(한글), 대리인(영문), 국제공개일자, 국제공개번호, 국제출원일자, 국제출원번호, 우선권, 우선권주장일, 우선권국가, 우선권출원번호, 원출원일자, 원출원번호, 지정국, Citing Patents, Cited Patents
저장형식	Text(ASCII format) Excel format PIAS분석(.xls)
메일정보	받는사람 (필수) @ 보내는사람 (선택) @ 제목 내용 KISTI 검색결과 이메일 서비스
안내	> 총 건의 자료가 검색되었습니다. > 다운받으실 자료의 인덱스를 입력하세요. (1-10,000) > 검색결과의 순서대로 최대 10,000건 까지 다운로드가 가능합니다. > 데이타가 많을 경우 속도가 느려질 수 있습니다.(최대 2~3분 소요) > 다운로드 파일은 UTF-8 형태로 저장됩니다. 파일의 내용이 제대로 보이지 않을실 때는 웹브라우저 상단의 보기 -> 인코딩 -> 자동선택 여부를 확인하십시오 > ~ > Text(ASCII format) Excel format

과학기술 지식인프라 ScienceON

ScienceON Chatbot

연합인증

특허 상세정보

Vertical takeoff and landing aircraft

초록
▼

대표
청구항
▼

이 특허에 인용된 특허 (12)

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

ScienceON Chatbot

연합인증

특허 상세정보

Vertical takeoff and landing aircraft

초록 ▼

대표청구항 ▼

이 특허에 인용된 특허 (12)

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

초록
▼

대표
청구항
▼