[특허]Spacecraft radiator panels

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

Spacecraft radiator panels

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64G-001/50 F28D-015/02
출원번호	US-0490833 (2012-06-07)
등록번호	US-9403606 (2016-08-02)
발명자 / 주소	Aston, Richard William Langmack, Michael J.
출원인 / 주소	The Boeing Company
대리인 / 주소	DASCENZO Intellectual Property Law, P.C.
인용정보	피인용 횟수 : 0 인용 특허 : 7

초록
▼

Spacecraft, radiator panels for spacecraft, kits for radiator panels, inserts associated with radiator panels, heat pipes associated with radiator panels, external structural reinforcement members associated with radiator panels, and methods of assembling radiator panels are disclosed herein. Some radiator panels include at least one insert that is positioned adjacent to a heat pipe between two spaced-apart face-sheets, with the insert being configured to secure a package to the inside face-sheet opposite of the heat pipe. Some radiator panels include at...

대표
청구항
▼

1. A radiator panel for a spacecraft, the radiator panel comprising: two spaced-apart face-sheets including an inside face-sheet and an outside face-sheet;at least one heat pipe positioned between the two spaced-apart face-sheets and operatively engaged and in thermal communication with the two spaced-apart face-sheets, wherein the at least one heat pipe includes a side extension with a substantially planar extension surface that is perpendicular to the two spaced-apart face-sheets;a core positioned between the two spaced-apart face-sheets;an insert positioned adjacent to the at least one heat pipe, wherein the insert includes a substantially planar insert surface that is perpendicular to the two spaced-apart face-sheets and that is operatively engaged with the substantially planar extension surface of the at least one heat pipe, wherein the insert is configured with at least one feature useful in the operative securing of a package to the inside face-sheet opposite the at least one heat pipe and the insert so that heat from the package may operatively conduct from the package through the inside face-sheet to the at least one heat pipe, wherein the insert extends from the inside face-sheet to the outside face-sheet, wherein the insert engages the inside face-sheet and the outside face-sheet, wherein the insert includes a positioning structure extending adjacent to the substantially planar insert surface, wherein the positioning structure includes a lip that wraps around a first edge of the side extension of the at least one heat pipe, and wherein the insert includes a retaining structure extending adjacent to the substantially planar insert surface opposite the positioning structure relative to the planar extension surface and that includes a clip that engages a second edge of the side extension of the at least one heat pipe; andat least one external structural reinforcement member extending across an external side of the outside face-sheet and substantially spanning an entire width of the radiator panel, wherein the at least one external structural reinforcement member defines a void between the at least one external structural reinforcement member and the outside face-sheet, wherein each of the at least one external structural reinforcement member has a longitudinal axis;wherein the radiator panel is free of heat pipes that are directly opposite, relative to the outside face-sheet, and longitudinally aligned with the longitudinal axis of at least one of the at least one external structural reinforcement member. 2. The radiator panel of claim 1, wherein the at least one structural reinforcement member includes a plurality of spaced-apart structural reinforcement members. 3. The radiator panel of claim 1, wherein the at least one external structural reinforcement member includes an outer reflective surface that generally faces away from the outside face-sheet, wherein the outer reflective surface has means for reflecting 30%-90% of all incident light on the outer reflective surface away from the outside face-sheet. 4. The radiator panel of claim 3, wherein the outer surface includes at least two planar surfaces. 5. The radiator panel of claim 3, wherein the outer surface includes at least two planar surfaces that are angled greater than 180 degrees relative to each other. 6. The radiator panel of claim 3, wherein the outer surface includes a first surface that is angled 120 degrees relative to the outside face-sheet, a second surface that is angled 210 degrees relative to the first surface and that is parallel to the outside face-sheet, and a third surface that is angled 210 degrees relative to the second surface and 120 degrees relative to the outside face-sheet. 7. The radiator panel of claim 3, wherein the outer surface includes at least one curved surface. 8. The radiator panel of claim 1, wherein a perpendicular cross-sectional profile of the void is a trapezoid. 9. The radiator panel of claim 1, wherein the radiator panel has a natural frequency in the range of 30-40 hertz. 10. The radiator panel of claim 1, wherein the radiator panel is free of internal structural reinforcement members coupled to the inside face-sheet. 11. The radiator panel of claim 1, wherein the at least one heat pipe is sized to have a predetermined heat transfer rate associated with the radiator panel, wherein the predetermined heat transfer rate is no more than 120% of a requisite heat transfer rate for the radiator panel. 12. The radiator panel of claim 1, wherein the void has a thickness that is greater than a thickness of the core. 13. A radiator panel for a spacecraft, the radiator panel comprising: two spaced-apart face-sheets including an inside face-sheet and an outside face-sheet;at least one heat pipe positioned between the two spaced-apart face-sheets and operatively engaged and in thermal communication with the two spaced-apart face-sheets, wherein the at least one heat pipe includes a side extension with a substantially planar extension surface that is perpendicular to the two spaced-apart face-sheets;a core positioned between the two spaced-apart face-sheets;an insert positioned adjacent to the at least one heat pipe, wherein the insert includes a substantially planar insert surface that is perpendicular to the two spaced-apart face-sheets and that is operatively engaged with the substantially planar extension surface of the at least one heat pipe, wherein the insert is configured with at least one feature useful in the operative securing of a package to the inside face-sheet opposite the at least one heat pipe and the insert so that heat from the package may operatively conduct from the package through the inside face-sheet to the at least one heat pipe, wherein the insert extends from the inside face-sheet to the outside face-sheet, wherein the insert engages the inside face-sheet and the outside face-sheet, wherein the insert includes a positioning structure extending adjacent to the substantially planar insert surface, wherein the positioning structure includes a lip that wraps around a first edge of the side extension of the at least one heat pipe, and wherein the insert includes a retaining structure extending adjacent to the substantially planar insert surface opposite the positioning structure relative to the planar extension surface and that includes a clip that engages a second edge of the side extension of the at least one heat pipe; anda plurality of spaced-apart and parallel external structural reinforcement members extending across an external side of the outside face-sheet, wherein each of the external structural reinforcement members include an outer reflective surface that generally faces away from the outside face-sheet and that includes at least two planar surfaces that are angled greater than 180 degrees relative to each other, wherein the spacing of the external structural reinforcement members and the configuration of the outer reflective surfaces of the external structural reinforcement members define means for reflecting 30%-90% of all incident light on the outer reflective surfaces away from the outside face-sheet, wherein at least one of the plurality of spaced-apart and parallel external structural reinforcement members substantially spans an entire width of the radiator panel, wherein each of the plurality of spaced-apart and parallel external structural reinforcement members has a longitudinal axis;wherein the radiator panel is free of heat pipes that are directly opposite, relative to the outside face-sheet, and longitudinally aligned with the longitudinal axis of at least one of the plurality of spaced-apart and parallel external structural reinforcement members.

이 특허에 인용된 특허 (7)

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

Spacecraft radiator panels

초록
▼

대표
청구항
▼

이 특허에 인용된 특허 (7)

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

Spacecraft radiator panels

초록 ▼

대표청구항 ▼

이 특허에 인용된 특허 (7)

IPC 상위 출원인

과제정보

상세정보조회

원문조회

IPC 상세정보(version : 201201)

연구과제 성과물(0)

참여연구원의 다른 문헌(0)

처리중입니다.

잠시만 기다려주세요.

초록
▼

대표
청구항
▼