과제명
NTIS 과제연계
과제기간
총연구비
- 검색어에 아래의 연산자를 사용하시면 더 정확한 검색결과를 얻을 수 있습니다.
- 검색연산자
| 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" |
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.
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.
다음과 같은 기능을 한번의 로그인으로 사용 할 수 있습니다.
NTIS 바로가기
특허 상세정보
Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
| 국가/구분 | United States(US) Patent 등록 |
|---|---|
| 국제특허분류(IPC7판) | B64C-009/16 B64C-009/00 |
| 미국특허분류(USC) | 244/216; 244/213; 244/215 |
| 출원번호 | US-0188988 (2002-07-02) |
| 등록번호 | US-7258308 (2007-08-21) |
| 발명자 / 주소 | |
| 출원인 / 주소 | |
| 대리인 / 주소 |
|
| 인용정보 | 피인용 횟수 : 13 인용 특허 : 61 |
초록
A method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface. The airfoil can include a first portion having a first leading edge, a first flow surface, and a second flow surface facing opposite from the first flow surface. The airfoil can further include a second portion having a second leading edge and a trailing edge, with at least part of the second portion being positioned aft of the first portion. The second portion is moveable relative to the first portion between a first position and a second po...
대표
청구항
We claim: 1. An airfoil assembly, comprising: a first portion having a first leading edge, a first flow surface, a second flow surface facing opposite from the first flow surface, and a hinge support; a second portion having a trailing edge body, a leading edge body, a second leading edge and a trailing edge, at least part of the second leading edge being positioned aft of the first leading edge, the second portion being movable relative to the first portion between a first position and a second position, wherein the second leading edge is separated fr...
이 특허에 인용된 특허 (61)
- Crouch Jeffrey D. ; Spalart Philippe R.. Active system for early destruction of trailing vortices. USP2000076082679.
- Lam Lawrence Y. ; Lam Michael. Aileron for fixed wing aircraft. USP2000066079672.
- Lam, Lawrence Y.; Lam, Michael. Aileron for fixed wing aircraft. USP2003046554229.
- Thornburg Francis L. (Canoga Park CA). Aileron segment control for a flaperon system. USP1979124180222.
- Fortes Rudy F. (Seattle WA). Aircraft control surface linkage. USP1990104962902.
- Maieli Joseph R. (Central Islip NY) Rosenthal Gordon (Jericho NY) Torrillo Domenick T. (Dix Hills NY). Aircraft wing. USP1977044015787.
- Fletcher John J. (Renton WA). Airfoil leading edge slat apparatus. USP1980054202519.
- Bliesner Wayne T. (Snohomish WA) Wang Timothy (Bellevue WA) Stoner Ronald C. (Bellevue WA). Apparatus and method for aircraft wing stall control. USP1991105056741.
- Pitt,Dale M.. Apparatus for increase of aircraft lift and maneuverability. USP2006047028948.
- Moelter Gunther (Ottobrunn DEX) Mueller Hermann (Munich DEX) Kunz Ruediger (Munich DEX). Apparatus for operating flap means secured to the wing of an aircraft. USP1980014181275.
- Jones, Kelly. Brake systems for aircraft wing flaps and other control surfaces. USP2004116824099.
- Squirrell Anton F. (Mellingen CHX). Cantilever spring seals for gas isolators. USP1996085542684.
- Statkus Frank D. (Woodinville WA). Continuous skin, variable camber airfoil edge actuating mechanism. USP1982094351502.
- Bachmann Lothar (Dillingham Hill Rd. ; R.F.D. #3 Auburn ME 04210) Koch William F. (R.F.D. #3 Box 483 Auburn ME 04210). Dampers with leaf spring seals. USP1989044823836.
- Sherry, Lance C.; Quarry, Steven T.. Display of altitude and path capture trajectories. USP2005036870490.
- Buus, Henning; MacFie, Thomas D.; Justad, Odd. Electric command spoiler system. USP1982124363098.
- Spitzer ; Robert E. ; May ; III ; Fred W.. Engine out control system for STOL aircraft. USP1978084106730.
- Kim Sharp GB. Fairing arrangement for an aircraft. USP2002096450457.
- Johnson,Brian D. Fairing arrangements for aircraft. USP2006057051982.
- Munoz Saiz Manuel,ESXITX 28017. Flight controls with automatic balance. USP2000086109567.
- Chenoweth Charles C. (Renton WA) Takats Imre J. (Bellevue WA). Fly-by-wire lateral control system. USP1984094472780.
- Prow, Clayton A.; Sakurai, Seiya; Wells, Stephen L.. Gapped trailing-edge control surface for an airfoil. USP2003086601801.
- Nash Dudley O. (Cincinnati OH). High excursion seal with flexible membrane to prevent gas leakage through hinge. USP1986034575099.
- Norbert A. Weisend, Jr.. Inflatable airfoil device. USP2002096443394.
- Gratzer Louis B. (Seattle WA). Laminar flow control airfoil. USP1986034575030.
- Schuster, John H.. Leading edge flap and boundary layer control system. USP1985104544117.
- Gruensfelder Cynthia Ann ; Brase ; Jr. Lawrence O.. Leading edge for an aircraft. USP2001046213433.
- Bliesner Wayne T. (Snohomish WA). Leading edge slat/wing combination. USP1996085544847.
- Middleton Wilbur D. (Bellevue WA) Paulson John A. (Bellevue WA). Leading edge vortex flap for wings. USP1981104293110.
- Lewis George E. (Renton WA). Maneuver load alleviation system. USP1989014796192.
- Williams George H. (Bristol GBX). Mechanism for supporting and extending a high lift device for aircraft wings. USP1989064838503.
- Trikha, Arun K.. Method and apparatus for controlling aircraft devices with multiple actuators. USP2004066755375.
- Earl K. Ferrel ; Richard P. Klingele ; Wolfram Hansis ; William B. Betters. Method and apparatus for detecting skew and asymmetry of an airplane flap. USP2002056382566.
- Abbott Terence S. (Williamsburg VA) Person ; Jr. Lee H. (Yorktown VA). Method and system for monitoring and displaying engine performance parameters. USP1991095050081.
- Breitbach Elmar J.,DEX ; Bein Thilo,DEX. Profile edge of an aerodynamic profile. USP2000066076776.
- Capbern Patrick (Cornebarrieu FRX) Charieras Jrme (Toulouse FRX) Chaumel Pascal (Plaisance du Touch FRX). Rigid kruger nose for the leading edge of an aircraft wing. USP1995125474265.
- Wataru Yada JP; Hiroshi Yamanouchi JP; Minoru Uchida JP; Katsutoshi Tada JP. Rotor blade operating device in airplane and flaperon operating device in airplane. USP2002106464175.
- Einarsson Stefan (Lindome SEX). Sealing means for a door lacking a threshold. USP1985074528775.
- Dizdarevic Faruk. Slot forming segments and slot changing spoilers. USP2001126328265.
- Bellego Roger (Blagnac FRX) Foch Etienne (Toulouse FRX). System for controlling the high-lift flaps of an aircraft. USP1988124789119.
- Huynh,Neal V.. Systems, apparatuses, and methods for moving aircraft control surfaces. USP2006067059563.
- Sakurai Seiya (Seattle WA). Three-position variable camber Krueger leading edge flap. USP1992105158252.
- Dean Roy D. (Seattle WA). Three-position variable camber flap. USP1981044262868.
- Rudolph Peter K. C. (Seattle WA) Hudson Verne L. (Bellevue WA). Trailing edge flap assembly. USP1984094471927.
- Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976113994451.
- Cole James B. (Mercer Island WA). Variable camber airfoil. USP1976033941334.
- Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1984104475702.
- Cole James B. (Mercer Island WA). Variable camber leading edge assembly for an airfoil. USP1987114706913.
- Wang Timothy (Bellevue WA). Variable camber leading edge flap. USP1980024189120.
- Zapel Edwin J. (Box 433 Maple Valley WA 98038). Variable camber leading edge for airfoil. USP1979104171787.
- McKinney Maurice E. (Bellevue WA) Rudolph Peter K. C. (Seattle WA). Variable camber leading edge mechanism with Krueger flap. USP1984014427168.
- McKinney Maurice E. (Bellevue WA). Variable camber trailing edge for airfoil. USP1982014312486.
- Zapel ; Edwin J.. Variable camber trailing edge for airfoil. USP1978124131253.
- Dean Roy Delmar (Seattle WA) Weiland Richard Herschel (Seattle WA). Variable pivot trailing edge flap. USP1976103985319.
- Vassberg, John Charles; Gregg, III, Robert D.. Variable trailing edge geometry and spanload control. USP2005016843452.
- Harper Philip M. (Bellevue WA) Johnson Kirby W. (Brier WA). Variable twist leading edge flap. USP1980024189121.
- Cole, James B.. Variable-camber airfoil. USP1985114553722.
- Cole James B. (Mercer Island WA). Wind edge movable airfoil having variable camber. USP1987034650140.
- Brown Robert B. (Kent WA). Wing leading edge slat. USP1982114360176.
- Rogers John T. (Bellevue WA) Manning Kenneth J. R. (Bellevue WA). Wing load alleviation system using tabbed allerons. USP1984104479620.
- Victor Paul F. (Redmond WA). Wing trailing edge air dam. USP1987124712752.
이 특허를 인용한 특허 피인용횟수: 13
- Sakurai,Seiya; Finnila,James E.; Stephenson,Martin F.. Aerospace vehicle flow body systems and associated methods. USP2009037500641.
- Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2013108567726.
- Lacy, Douglas S.; Kordel, Jan A.; Dovey, John V.; Balzer, Michael A.; Sakurai, Seiya; Huynh, Neal V.. Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods. USP2011108038103.
- Lacy, Douglas S.; Beyer, Kevin W.; Brown, Stephen T.; Dees, Paul W.; Huynh, Neal V.; Kordel, Jan A.; Prow, Clayton A.; Sakurai, Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2010067744040.
- Lacy,Douglas S.; Beyer,Kevin W.; Brown,Stephen T.; Dees,Paul W.; Huynh,Neal V.; Kordel,Jan A.; Prow,Clayton A.; Sakurai,Seiya. Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods. USP2009017475854.
- Droney, Christopher K.; Rawdon, Blaine K.. Aircraft wing assemblies. USP2017019550559.
- Saliveros, Efstratios; Friedel, Hendrik. Flap system for an aircraft, method for adjusting the lift of an aircraft and aircraft comprising a main wing and at least one flap system. USP2017119815547.
- Beyer, Kevin W.; Sakurai, Seiya; Stephenson, Martin F.. Hinged panel operation systems and methods. USP2015069061753.
- Beyer, Kevin W.; Sakurai, Seiya. Link mechanisms, including Stephenson II link mechanisms for multi-position flaps and associated systems and methods. USP2012078226048.
- Manley, David J.; Grip, Robert E.. Shape-changing control surface. USP2013028382045.
- Huynh, Neal V.; Bleeg, Robert J.; Pepper, Ralph Scott; Standley, John A.; Bocksch, Brian L.. Systems and methods for controlling aircraft flaps and spoilers. USP2011027891611.
- Good, Mark S.; Vijgen, Paul M.; Gitnes, Seth E.; Thomas, Glynn Michael. Systems and methods for providing differential motion to wing high lift device. USP2010067726610.
- Kordel, Jan A.; Sakurai, Seiya; Balzer, Michael A.; Dovey, John V.. Trailing edge device catchers and associated systems and methods. USP2010087766282.
