[특허]Tip turbine engine integral fan, combustor, and turbine case

[미국특허] Tip turbine engine integral fan, combustor, and turbine case 원문보기

IPC분류정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F02K-003/02
출원번호	US-0720539 (2004-12-01)
등록번호	US8033092 (2011-09-27)
국제출원번호	PCT/US2004/039973 (2004-12-01)
§371/§102 date	20070531 (20070531)
국제공개번호	WO06/059971 (2006-06-08)
발명자 / 주소	Suciu, Gabriel L. Norris, James W. Nordeen, Craig A. Merry, Brian
출원인 / 주소	United Technologies Corporation
대리인 / 주소	Carlson, Gaskey & Olds, P.C.
인용정보	피인용 횟수 : 2 인용 특허 : 71

초록 ▼

A tip turbine engine assembly includes an integral engine outer case located radially outward from a fan assembly. The integral outer case includes a rear portion and a forward portion with an arcuate portion that curves radially inwardly to form a compartment. An annular combustor is housed and mounted in the compartment. Fan inlet guide vanes are integrally formed with the arcuate portion to form the integral case portion. The rear portion, forward portion, and fan inlet guide vanes are integrally formed in a casting process.

대표청구항 ▼

The invention claimed is: 1. A tip turbine engine assembly comprising:a fan rotatable in a fan plane about an axis, said fan including a fan blade defining a core airflow passage through said fan blade;a compressor rotatable in a compressor plane spaced axially forward of said fan plane and directing compressed air to said airflow passage;a turbine extending radially outwardly from said fan;a combustor axially spaced from said fan, said combustor communicating with said airflow passage; and,an engine case radially outward from said fan and said combustor.

이 특허에 인용된 특허 (71) 인용/피인용 타임라인 분석

Dodd, Alec G., Aerofoil blade containment.
상세보기
Dunbar Donald K. (Sharonville OH) Delaney Bobby R. (Loveland OH), Aircraft bypass turbofan engine thrust reverser.
상세보기
Seda, Jorge F., Aircraft engine with inter-turbine engine frame.
상세보기
Seda, Jorge F.; Dunbar, Lawrence W.; Gliebe, Philip R.; Szucs, Peter N.; Brauer, John C.; Johnson, James E.; Moniz, Thomas; Steinmetz, Gregory T., Aircraft engine with inter-turbine engine frame supported counter rotating low pressure turbine rotors.
상세보기
Sokhey Jack (Jagdish) Singh ; Crook Andrew James ; Snyder Philip Harold ; Vittal Baily R., Aircraft thrust vectoring system.
상세보기
Albert J. Partington, Blade group with pinned root.
상세보기
David Andrew Goshorn ; David William Crall, Blisk.
상세보기
Lifka Hans (Kochel DEX), Combination propulsion system for a flying craft.
상세보기
Mirville Francois J. (Melun FRX), Combined air-hydrogen turbo-rocket power plant.
상세보기
Howald Werner E. (5970 Crabtree La. Cincinnati OH 45243), Combustion apparatus including an air-fuel premixing chamber.
상세보기
Varney, Brian A., Combustion chamber.
상세보기
Hayes Jeffrey M. (Phoenix AZ), Counterflow single rotor turbojet and method.
상세보기
Liston Laurence D. N. ; Schoepf Joseph L. ; Royalty Charles Michael, Detachable integral aircraft tailcone and power assembly.
상세보기
Adamson Arthur P. (Cincinnati OH), Differential geared engine.
상세보기
Scott Alexander (Bristol EN) Peck Peter Eric (Bristol EN), Differentially geared reversible fan for ducted fan gas turbine engines.
상세보기
Hermann Klingels DE, Driving mechanism with counter-rotating rotors.
상세보기
Stryker Howard Y. (Glastonbury CT) Steel Thomas (Derby GB2), Ducted fan gas turbine power plant mounting.
상세보기
Gallant George A. (Burlington VT), Eddy current sensor.
상세보기
Billington Webster G. (1003 Wilshire Blvd. ; #203 Santa Monica CA 90401), Engine exhaust control system and method.
상세보기
Moore M. Samuel (Northridge CA) Paluka Charles F. (Northridge CA), Engine load sharing control system.
상세보기
Boris Paul A. (Ellington CT) Marx Jon A. (Manchester CT), Engine mount.
상세보기
Karstensen Karl W. (Peoria IL), Expansion control ring for a turbine shroud assembly.
상세보기
Eldredge David A. (Port St. Lucie FL) Ress ; Jr. Robert A. (Carmel IN), Fan blade attachment for gas turbine engine.
상세보기
Uwe Aschermann DE; Uwe Blass DE, Fan with axial blades.
상세보기
Riikonen Esko A., Fluidic pinch valve system.
상세보기
Weinstein Barry (Georgetown MA) Steyer William (Ipswich MA), Foreign particle separator system.
상세보기
Kwan, William C. T.; Pidcock, Anthony, Gas turbine engine combustion apparatus.
상세보기
Wilcox David E. (Mesa AZ), Gas turbine engine module assembly.
상세보기
Newton Arnold C. (Derby GB2), Gas turbine engine nacelle assembly.
상세보기
Sherman Alden O. (85 Weston Rd. Weston CT 06883), Gas turbine vanes and methods for making same.
상세보기
Flamang,Peter; Smook,Warren, Gear unit lubrication.
상세보기
Adamson Arthur P. (Cincinnati OH) Butler Lawrence (Cincinnati OH) Wall Robert A. (Wyoming OH), Geared counterrotating turbine/fan propulsion system.
상세보기
McKibbin Albert H. (Cromwell CT) Burno Jon D. (South Windsor CT), Geared drive system for a bladed propulsor.
상세보기
Law,Chi, Geartrain coupling for a turbofan engine.
상세보기
Mulcaire, Thomas G; Holdsworth, Michael T; Evans, Richard, Guide vane assembly.
상세보기
Nastuk John A. (Danvers MA) Williams Charles L. (Albuquerque NM), High pressure gas generator rotor tie rod system for gas turbine engine.
상세보기
Gilchrist Alan R. (Fairfield OH) Sullivan Thomas J. (Fairfield OH) Walker Roger C. (Middletown OH), Hybrid spinner nose configuration in a gas turbine engine having a bypass duct.
상세보기
Catlow Ronald (Derby GB2), Hydraulic seal and method of assembly.
상세보기
Carter David B. (Manchester CT) Weisse Michael A. (Tolland CT), Increased impact resistance in hollow airfoils.
상세보기
Ciokajlo John J. (Cincinnati OH) Ritchie Henry B. (Ft. Pierce FL), Jet engine turbine support.
상세보기
Klees Garry W. (Mercer Island WA), Jet engine with noise suppressing mixing and exhaust sections.
상세보기
Joslin, Frederick R., Leak resistant vane cluster.
상세보기
Mark Joseph Mielke ; John Jared Decker, Method and apparatus for reducing rotor assembly circumferential rim stress.
상세보기
Ruckle Duane L. (Mesa AZ) Millan ; Jr. Ponciano P. (Mesa AZ), Method for heat treating cast titanium articles to improve their mechanical properties.
상세보기
Maurizio Avidano IT; Virgilio Crestani IT, Motor-driven fan, particularly for a motor vehicle heat exchanger.
상세보기
Rodgers Leonard J.,GB2 ; Newton Arnold C.,GB2 ; Berry James P.,GB2 ; Farrar Peter G. G.,GB2 ; Udall Kenneth F.,GB2, Mounting for coupling a turbofan gas turbine engine to an aircraft structure.
상세보기
Nightingale Douglas J. (Bellview WA), Mounting for gas turbine powerplant.
상세보기
Partington Albert J. (Winter Springs FL), Mounting of integral platform turbine blades with skewed side entry roots.
상세보기
Chapman John F. (Solihull GB2 4), Multi-layer acoustic linings.
상세보기
Polenick Michael J. ; Scott Michael W., Multiple gas turbine engines to normalize maintenance intervals.
상세보기
Partington ; Albert J., Multiple side entry root for multiple blade group.
상세보기
Rudolf Stegherr DE, Planetary gear.
상세보기
Bart Jacques R. (Evry FRX), Pod for a turbofan aero engine of the forward contrafan type having a very high bypass ratio.
상세보기
Stephens Paul S. (Sharonville OH) Szpunar Stephen J. (West Chester OH), Positioning system and impact indicator for gas turbine engine fan blades.
상세보기
Marshall Richard L. (Manchester CT) Cashman Kenneth A. (Scarborough ME), Premix combustor assembly.
상세보기
Geidel Helmut (Karlsfeld DEX) Rohra Alois (Mnchen DEX), Propfan turbine engine.
상세보기
Hadaway Edward S. (Derby GB2) Wedlake Norman J. (Bristol GB2), Reduction gear assembly and a gas turbine engine.
상세보기
Waitz Ian A. ; Brookfield John M. ; Sell Julian ; Hayden Belva J. ; Ingard K. Uno, Reduction of turbomachinery noise.
상세보기
Toborg Steven M. (Lynn MA), Reinforced compressor rotor coupling.
상세보기
Ciokajlo John J. (Henderson NV) Hauser Ambrose A. (Wyoming OH) Davison Samuel H. (Milford OH), Rotatable turbine frame.
상세보기
Davids Joseph (Maitland FL) Silvestri ; Jr. George J. (Winter Park FL), Segmental vane apparatus and method.
상세보기
Kirtley, Kevin; Graziosi, Paolo, Self-aspirating high-area-ratio inter-turbine duct assembly for use in a gas turbine engine.
상세보기
Girault Jean-Philippe N. (Tourny FRX), Single flow turbopump with integrated boosting.
상세보기
David A. Platts, Single rotor turbine engine.
상세보기
Sheridan William G., Star gear system with lubrication circuit and lubrication method therefor.
상세보기
Soligny Marcel R. (Chevilly-Larue FRX), System for attaching two rotating parts made of materials having different expansion coefficients.
상세보기
Ross Steven A. ; Albers Robert J. ; Brill Edward P. ; Kemp Andrew D. ; Plemmons Larry W., Turbine nozzle assembly.
상세보기
Rd Klaus (Grbenzell DEX) Rohra Alois (Mnchen DEX), Turbo engine.
상세보기
Perry Derick A. (Derby GB2), Turbofan gas turbine engine.
상세보기
Boudigues Serge (Sceaux FRX), Turbojet with contrarotating wheels.
상세보기
Rudolph Peter K. C. (Seattle WA) Ostrom Grazyna B. (Auburn WA), Turboprop propulsion apparatus.
상세보기

이 특허를 인용한 특허 (2) 인용/피인용 타임라인 분석

Murdock, James R.; McKaveney, Christopher S.; Elliott, Jason, Fan blade attachment of gas turbine engine.
상세보기
Kupratis, Daniel B., Hybrid turbofan engine.
상세보기

활용도 분석정보

상세보기

다운로드

내보내기

활용도 Top5 특허

해당 특허가 속한 카테고리에서 활용도가 높은 상위 5개 콘텐츠를 보여줍니다.
더보기 버튼을 클릭하시면 더 많은 관련자료를 살펴볼 수 있습니다.

내보내기 메뉴

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

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

AI-Helper ※ AI-Helper는 을 사용합니다.

AI-Helper

안녕하세요, AI-Helper입니다. 좌측 "선택된 텍스트"에서 텍스트를 선택하여 요약, 번역, 용어설명을 실행하세요.
※ AI-Helper는 부적절한 답변을 할 수 있습니다.

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

연합인증

[미국특허] Tip turbine engine integral fan, combustor, and turbine case 원문보기