[특허]Method and apparatus for liquid containment, such as for aircraft fuel vessels

Method and apparatus for liquid containment, such as for aircraft fuel vessels 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	B64C-003/26 B64C-003/00 B64D-037/05
출원번호	US-0165933 (2005-06-24)
발명자 / 주소	Friddell,Stephen D. Prichard,Alan K.
출원인 / 주소	The Boeing Company
대리인 / 주소	Perkins Coie LLP
인용정보	피인용 횟수 : 5 인용 특허 : 98

초록 ▼

A vessel, such as a wing-integrated aircraft fuel tank. The vessel can include a first surface portion, a second surface portion spaced apart from the first surface portion, and a core positioned between the first and second surface portions. The core can be sealably connected to the first and second surface portions and can be positioned to carry a load from at least one of the first and second surface portions to the other. The core can include a plurality of cells separated by cell walls, at least some of which have wall openings positioned to provide liquid communication between adjacent cells.

대표청구항 ▼

We claim: 1. A method for forming an airfoil, comprising: positioning a first surface portion spaced apart from a second surface portion; positioning a core between the first and second surface portions and outboard a collection chamber in the airfoil, the core including a plurality of cells separated by cell walls, at least some of the cell walls having wall openings to provide liquid communication between adjacent cells and between the collection chamber and the core; and sealably connecting the core to the first and second surface portions to form at least part of a fluid-tight volume between the first and second surface portions, with the core positioned to carry a load from at least one of the first and second surface portions to the other. 2. The method of claim 1 wherein sealably connecting the core to the first and second surface portions includes adhesively bonding the core to the first and second surface portions. 3. The method of claim 1, further comprising perforating the cell walls to form the wall openings. 4. The method of claim 1, further comprising expanding the core from an initially collapsed state to an expanded state after perforating the cell walls and before positioning the core between the first and second surface portions. 5. The method of claim 1 wherein the core includes cells having cell openings elongated along corresponding cell axes, and wherein positioning the core includes positioning the core with the cell axes extending generally transverse to at least one of the first and second surface portions. 6. The method of claim 1 wherein positioning a core includes positioning a core that is generally rigid in a direction generally transverse to at least one of the first and second surface portions. 7. The method of claim 1, further comprising disposing a fuel port in liquid communication with the fuel-tight volume. 8. The method of claim 1 wherein positioning a core includes positioning a core having wall openings with a diameter of approximately 0.125 inch or greater. 9. The method of claim 1 wherein positioning a core includes positioning a core having cells with a width generally transverse to at least one of the first and second surface portions, and wherein the wall openings have a diameter of approximately one quarter of the width or greater. 10. A method for forming aircraft components, comprising: positioning a first wing portion having a first external surface and a first internal surface to be proximate to a second wing portion having a second external surface and a second internal surface, with at least part of the second internal surface being spaced apart from at least part of the first internal surface; positioning a core between the first and second wing portions, the core including an outboard portion, an inboard portion, and a plurality of at least generally similarly sized and shaped cells separated by cell walls, at least some of the cell walls having wall openings positioned to provide liquid communication between adjacent cells, the wall openings being sized and configured such that fuel flow through the wall openings from the outboard portion to the inboard portion provides sufficient fuel for operation of an aircraft engine; sealably connecting the core to the first and second wing portions to form at least part of a fuel-tight volume, the core being positioned to carry a load from at least one of the first and second wing portions to the other; and coupling a fuel port in liquid communication with the fuel volume, the fuel port being coupleable to the aircraft engine. 11. The method of claim 10, further comprising connecting the first and second wing portions to an aircraft fuselage. 12. The method of claim 10, further comprising: sealably coupling a first intermediate panel between the first and second wing portions; and sealably coupling a second intermediate panel between the first and second surface portions, with the second intermediate panel spaced apart from the first intermediate panel, and with at least a portion of the core positioned between the first and second intermediate panels. 13. The method of claim 10, further comprising coupling a fuel conduit in liquid communication with the fuel volume.

이 특허에 인용된 특허 (98)

Arcas Noe (Plainview NY) Parente Charles A. (Oyster Bay NY), Acoustic liner.
상세보기
Kraft Robert E. (Cincinnati OH) Kontos Karen B. (Loveland OH), Active acoustic liner.
상세보기
Pla Frederic G. (Clifton Park NY), Active noise control using an array of plate radiators and acoustic resonators.
상세보기
Pla Frederic G. (Schenectady NY) Rajiyah Harindra (Clifton Park NY) Renshaw Anthony A. (Albany NY) Hedeen Robert A. (Clifton Park NY), Active noise control using noise source having adaptive resonant frequency tuning through stress variation.
상세보기
Pla Frederic G. (Schenectady NY) Rajiyah Harindra (Clifton Park NY) Renshaw Anthony A. (Albany NY) Hedeen Robert A. (Clifton Park NY), Active noise control using noise source having adaptive resonant frequency tuning through variable ring loading.
상세보기
Michie Terry K. (Olathe KS), Airborne weather radar system with icing detection capabiliy.
상세보기
Cook Leonard J. (Canoga Park CA) Rosenthal Herman A. (San Diego CA), Aircraft anti-icing plenum.
상세보기
Spiro Clifford Lawrence (Niskayuna NY) Fric Thomas Frank (Niskayuna NY) Leon Ross Michael (Cincinnati OH), Aircraft anti-insect system.
상세보기
Schulze Wallace M. (West Chester OH), Aircraft engine inlet cowl anti-icing system.
상세보기
McKillip Robert M., Aircraft icing detection system.
상세보기
Bragg Michael B. ; Gurbacki Holly M., Aircraft surface contamination sensing system using control surface hinge moment measurements.
상세보기
Danninger Karl (P.O. Box 3125 Boulder CO 80307), Aircraft temperature probe.
상세보기
Rauckhorst ; III Richard Lawrence ; Sweet David Bert, Airfoil low ice adhesion surface.
상세보기
Goto, Kenichi; Fujii, Toshiaki, Airplane fuel supply system and airplane wing pipeline assembly method.
상세보기
Rudolph Peter K. C. (Seattle WA) Georgefalvy Dezso (Mercer Island WA), Anti-icing system for aircraft.
상세보기
Gerardi Joseph J. ; Hickman Gail A. ; Khatkhate Ateen A. ; Pruzan Dan A., Apparatus and method for determining the existence of ice or water on a surface from the capacitance between electrodes.
상세보기
Blackwood Carl I. R. (Campbell CA), Apparatus and method for ice detection.
상세보기
Dougherty Robert P. (Bellevue WA), Apparatus and method for reducing noise emissions from a gas turbine engine inlet.
상세보기
Gagnon Robert E. (St. John\s CAX), Apparatus and method for remote detection of ice or other birefringent material on a surface.
상세보기
Sokolean Helmuth,CHX ; Roschmann Klaus,CHX ; Ender Josef,CHX, Apparatus for cooling a room.
상세보기
Gerardi Joseph J. (Dryden NY) Hickman Gail A. (Dryden NY) Khatkhate Ateen A. (Ithaca NY) Pruzan Dan A. (Ithaca NY), Apparatus for measuring ice distribution profiles.
상세보기
Osbond Paul C. (Northampton GB3) Whatmore Roger W. (Milton Keynes GB2) Auton John P. (Cambridge GB2), Atmospheric sensor.
상세보기
Adee James M. (San Diego CA), Buried element deicer.
상세보기
Joachim Paul DE, Cold transportation method.
상세보기
Parente Charles A., Combined acoustic and anti-ice engine inlet liner.
상세보기
Hilton R. John (Auburn WA), Composite honeycomb core structures and single stage hot bonding method of producing such structures.
상세보기
Parkman David, Condensation and frost control system.
상세보기
Rutherford Robert B., De-ice and anti-ice system and method for aircraft surfaces.
상세보기
Rutherford Robert B., De-ice and anti-ice system and method for aircraft surfaces.
상세보기
Phillips ; II Ronald W. (Mogadore OH), Deicer control system.
상세보기
Catchpole Brian George (Burwood AU), Detection of surface ice accretion.
상세보기
Stormbom Lars (Vantaa FIX), Detector and method for observation of the presence of a liquid and/or of a change of phase in same.
상세보기
Cattaneo Christian J. (Lissy FRX) Derouet Patrick R. J. (Soignolles en Brie FRX) Laroche Michel C. F. (Le Mee sur Seine FRX), Device for detecting and preventing the formation of ice on contoured surfaces.
상세보기
Giamati Michael J. ; Siesel Jeffrey J., Drainmast with integral electronic temperature control.
상세보기
Cole Derek (Bangor GB5), Duct for hot air.
상세보기
Cole Derek (Bangor GB5) Arnold Michael J. (Bangor GB5), Duct for hot air.
상세보기
Nikkanen John P. (West Hartford CT) Bubello Robert (Meridan CT) Maier Grant P. (Glastonbury CT), Efficient anti-ice exhaust method.
상세보기
Nikkanen John P. (West Hartford CT) Bubello Robert (Meridan CT) Maier Grant P. (Glastonbury CT), Efficient anti-ice exhaust vent.
상세보기
Kim John Jungwoo, Fiber optic ice detector.
상세보기
French Arnold E. ; Miller Phillip M., Freeze/overflow detector with deactivating mechanism.
상세보기
Rose Philip M. (Chula Vista CA) Yu Jia (San Diego CA), Honeycomb noise attenuation structure.
상세보기
Leuchten William E. (Mountain Lake NJ) Kretow Robert P. (Howell NJ), Honeycomb reinforcing sheet for the reinforcement of panels and method of reinforcing panels.
상세보기
Harper-Tervet Jan (Palmdale CA) Simenz Rod F. (Sherman Oaks CA) George James C. (Los Angeles CA), Honeycomb sandwich structure having dissimilar metal face sheets.
상세보기
Bourland ; Jr. Gordon (Arlington TX) Price Howard M. (Burleson TX), Honeycomb structure.
상세보기
Levit, Mikhail R., Honeycomb structure.
상세보기
Biersach James R. (511 Kimberlee Drive N. Baxter MN 56401), Honeycomb structure and method of making same.
상세보기
Vivekanandan Jothiram, Ice detection using radiometers.
상세보기
Cronin Dennis J. ; Jackson Darren G. ; Owens David G., Ice detector configuration for improved ice detection at near freezing conditions.
상세보기
Kleven Lowell A. (Eden Prairie MN), Ice detector probe.
상세보기
Stallabrass James R. (Ottawa CA) Ringer T. Rayman (Ottawa CA) Bailey Donald L. (Ottawa CA) Hearty Patrick F. (Hull CA), Icing detector.
상세보기
Padawer Jacques (170 Villard Ave. Hastings-on-Hudson NY 10706) Goldberg Robert M. (120 Orleans La. Jericho NY 11753), Icing detector for aircraft surfaces.
상세보기
Gupta Alankar (Renton WA) Waters Kenneth L. (Federal Way WA), Integrated thermal anti-icing and environmental control system.
상세보기
Dana A. Kromer ; John A. Severson, Integrated total temperature probe system.
상세보기
Cole James B. (Mercer Island WA), Leading edge slat/anti-icing system and method for airfoil.
상세보기
Geraldi Joseph J. (Dryden NY) Hickman Gail A. (Dryden NY) Khatkhate Ateen A. (Ithaca NY) Pruzan Dan A. (Ithaca NY), Measuring ice distribution profiles on a surface with attached capacitance electrodes.
상세보기
Call David B. (Boulder CO) Nolan James A. (Evergreen CO) Lassman Steven J. (Boulder CO), Meteorological data encoder for measuring atmospheric conditions.
상세보기
Breer, Marlin D.; Olsen, Ronald F.; Kunze, Jr., Robert K.; Riedel, Brian L., Method and apparatus for aircraft inlet ice protection.
상세보기
Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel, Method and apparatus for aircraft inlet ice protection.
상세보기
Marlin D. Breer ; Ronald F. Olsen ; Robert K. Kunze, Jr. ; Brian L. Riedel, Method and apparatus for aircraft inlet ice protection.
상세보기
Andy Lynn Derryberry ; David Michael Jackson ; Jon Donald Tromblee ; Jurgen Pannock, Method and apparatus for de-icing dehumidifier.
상세보기
Friddell, Stephen D.; Prichard, Alan K., Method and apparatus for liquid containment, such as for aircraft fuel vessels.
상세보기
MacKenzie Innes K.,CAX, Method and apparatus for measuring ice thickness on substrates using backscattering of gamma rays.
상세보기
Peter Albert Lauwers BE, Method and device for cool-drying.
상세보기
Benjamin Edward Andrews, Method for cleaning ductwork.
상세보기
Thornton-Trump Walter E. (108 Bellvue Drive Beaver Lake ; Plattsmouth NB 68048), Method for deicing aircraft.
상세보기
Hans Kristian Holmen NO, Method of and apparatus for detection of ice accretion.
상세보기
Parente Charles A. (Oyster Bay NY), Method of making an acoustic attenuating liner.
상세보기
Blair Winford (La Mesa CA), Method of manufacture of honeycomb noise attenuation structure for high temperature applications.
상세보기
Stormbom Lars (Vantaa FIX) Lyyra Matti (Vantaa FIX), Method of measuring dewpoint or gas concentration and apparatus for prediction of icing.
상세보기
Lee, Dae Sung; Lee, Kyung Il; Hwang, Hak In, Microwave power sensor and method for manufacturing the same.
상세보기
Newman Michael D. ; McCormick Stephen, Modular apparatus for cooling and freezing of food product on a moving substrate.
상세보기
Schindler Guenter M. (Palos Verdes CA), Multi-layered acoustic liner.
상세보기
Birbragher Fernando (Miami FL), Nacelle anti-icing system.
상세보기
Wilson, Robert Samuel, Noise attenuation panel.
상세보기
Wilson, Robert Samuel, Noise attenuation panel.
상세보기
Birbragher Fernando (Miami FL), Noise reduction nacelle.
상세보기
Mark Anderson ; Larry Meiners ; Joe Burns, Probe and integrated ice detection and air data system.
상세보기
LeBlond Henri (Versailles FRX) Choisnet Joel (La Frette S/Seine FRX) Dodel Gregoire (Neuilly Sur Seine FRX), Procedure and devices to determine the severity of icing conditions for an aircraft.
상세보기
Mears John S. ; Bulow Ronald A. ; Joyce David L. ; Kast Kevin H., Sensor ice shield.
상세보기
Hilton R. John (Auburn WA), Single stage hot bonding method for producing composite honeycomb core structures.
상세보기
Blohowiak Kay Y. ; Osborne Joseph H. ; Krienke Kenneth A., Sol coating of metals.
상세보기
Blohowiak Kay Y. ; Osborne Joseph H. ; Krienke Kenneth A., Sol for bonding expoxies to aluminum or titanium alloys.
상세보기
Blohowiak Kay Y. ; Osborne Joseph H. ; Krienke Kenneth A., Sol for coating metals.
상세보기
Blohowiak Kay Y. ; Osborne Joseph H. ; Krienke Kenneth A., Sol-gel coated metal.
상세보기
Snyder Stephen J. (West Hills CA), Sound attenuating laminate for jet aircraft engines.
상세보기
Taylor Maurice Ian (Allestree EN), Sound attenuating structure.
상세보기
Clark Walter L. (Scottsdale AZ) Sutton Trevor G. (Tempe AZ), Static pressure probe and method.
상세보기
Jessup Jerry R. ; Perez ; Sr. Richard, Structural bonding with encapsulated foaming adhesive.
상세보기
Blohowiak Kay Y. ; Osborne Joseph H. ; Krienke Kenneth A., Surface pretreatment for sol coating of metals.
상세보기
Blohowiak Kay Y. ; Osborne Joseph H. ; Krienke Kenneth A., Surface pretreatment of metals to activate the surface for sol-gel coating.
상세보기
Rosenthal Herman A. (San Diego CA), Swirl anti-ice system.
상세보기
Rosenthal Herman Allen, Swirl anti-ice system.
상세보기
Arnold Michael J. (Bangor GB5) Cole Derek (Bangor GB5), Thermal anti-icing of aircraft structures.
상세보기
McLaren Douglas (Seattle WA) Orr William W. (Mercer Island WA), Thermal anti-icing system for aircraft.
상세보기
Hagen Floyd W. (Eden Prairie MN), Three pressure pseudo -D 상세보기

IPC	Description
A	생활필수품
A62	인명구조; 소방(사다리 E06C)
A62B	인명구조용의 기구, 장치 또는 방법(특히 의료용에 사용되는 밸브 A61M 39/00; 특히 물에서 쓰이는 인명구조 장치 또는 방법 B63C 9/00; 잠수장비 B63C 11/00; 특히 항공기에 쓰는 것, 예. 낙하산, 투출좌석 B64D; 특히 광산에서 쓰이는 구조장치 E21F 11/00)
A62B-1/08	.. 윈치 또는 풀리에 제동기구가 있는 것

내보내기 구분	파일저장 인쇄 메일전송
구성항목	기본정보 상세정보 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

연합인증

Method and apparatus for liquid containment, such as for aircraft fuel vessels 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

이 특허에 인용된 특허 (98)

이 특허를 인용한 특허 (5)

관련 콘텐츠

특허 원문 보기

IPC 상위 출원인

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

선택된 텍스트

연합인증

Method and apparatus for liquid containment, such as for aircraft fuel vessels 원문보기

초록 ▼

대표청구항 ▼

연구과제 타임라인

전체(0) 논문(0) 특허(0) 보고서(0)

전체(0) 논문(0) 특허(0) 보고서(0)

이 특허에 인용된 특허 (98)

이 특허를 인용한 특허 (5)

관련 콘텐츠

특허 원문 보기

IPC 상위 출원인

AI-Helper ※ AI-Helper는 오픈소스 모델을 사용합니다.

선택된 텍스트