DE60310138D1 - Flugzeug mit nach vorne öffnenden und abgesenkten störklappen zur giersteuerung - Google Patents

Flugzeug mit nach vorne öffnenden und abgesenkten störklappen zur giersteuerung

Info

Publication number
DE60310138D1
DE60310138D1 DE60310138T DE60310138T DE60310138D1 DE 60310138 D1 DE60310138 D1 DE 60310138D1 DE 60310138 T DE60310138 T DE 60310138T DE 60310138 T DE60310138 T DE 60310138T DE 60310138 D1 DE60310138 D1 DE 60310138D1
Authority
DE
Germany
Prior art keywords
forward opening
mudguages
gyro
lowered
management
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Expired - Lifetime
Application number
DE60310138T
Other languages
English (en)
Other versions
DE60310138T2 (de
Inventor
Dennis Clark
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Northrop Grumman Corp
Original Assignee
Northrop Grumman Corp
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Northrop Grumman Corp filed Critical Northrop Grumman Corp
Publication of DE60310138D1 publication Critical patent/DE60310138D1/de
Application granted granted Critical
Publication of DE60310138T2 publication Critical patent/DE60310138T2/de
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C1/0009—Aerodynamic aspects
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/08—Stabilising surfaces mounted on, or supported by, wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/32—Air braking surfaces
    • B64C9/323—Air braking surfaces associated with wings
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/34—Adjustable control surfaces or members, e.g. rudders collapsing or retracting against or within other surfaces or other members
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D7/00—Arrangements of military equipment, e.g. armaments, armament accessories, or military shielding, in aircraft; Adaptations of armament mountings for aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
    • B64C2001/0045—Fuselages characterised by special shapes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/10—All-wing aircraft
    • B64C2039/105—All-wing aircraft of blended wing body type
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/10—Drag reduction
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/30—Wing lift efficiency
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/40—Weight reduction
DE60310138T 2003-01-29 2003-12-16 Flugzeug mit nach vorne öffnenden und abgesenkten störklappen zur giersteuerung Expired - Lifetime DE60310138T2 (de)

Applications Claiming Priority (3)

Application Number Priority Date Filing Date Title
US353660 2003-01-29
US10/353,660 US6892982B2 (en) 2003-01-29 2003-01-29 Aircraft with forward opening inlay spoilers for yaw control
PCT/US2003/039927 WO2004108526A1 (en) 2003-01-29 2003-12-16 Aircraft with forward opening inlay spoilers for yaw control

Publications (2)

Publication Number Publication Date
DE60310138D1 true DE60310138D1 (de) 2007-01-11
DE60310138T2 DE60310138T2 (de) 2007-10-11

Family

ID=32736231

Family Applications (1)

Application Number Title Priority Date Filing Date
DE60310138T Expired - Lifetime DE60310138T2 (de) 2003-01-29 2003-12-16 Flugzeug mit nach vorne öffnenden und abgesenkten störklappen zur giersteuerung

Country Status (11)

Country Link
US (2) US6892982B2 (de)
EP (1) EP1587734B1 (de)
JP (1) JP2006514591A (de)
KR (1) KR20050095907A (de)
AT (1) ATE346791T1 (de)
AU (1) AU2003304182A1 (de)
BR (1) BR0318083A (de)
CA (1) CA2514825A1 (de)
DE (1) DE60310138T2 (de)
IL (1) IL169894A0 (de)
WO (1) WO2004108526A1 (de)

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GR20130100618A (el) * 2013-10-25 2015-05-18 Ιωαννης Γεωργιου Μικρος Βελτιωση διεδρων αεροσκαφους στελθ για ταχυτητα
CN104691743A (zh) * 2015-03-17 2015-06-10 中国空气动力研究与发展中心高速空气动力研究所 一种飞翼布局航向控制的嵌入式操纵面
RU2622908C1 (ru) * 2016-07-07 2017-06-21 Федеральное государственное автономное образовательное учреждение высшего образования "Сибирский федеральный университет" (СФУ) Радиолокационный способ обнаружения летательных аппаратов
CN109625240A (zh) * 2018-11-23 2019-04-16 中国航空工业集团公司沈阳飞机设计研究所 减弱飞翼布局飞机俯仰角力矩非线性度的装置及系统
CN115092380A (zh) * 2022-08-22 2022-09-23 中国空气动力研究与发展中心空天技术研究所 一种适用于扁平融合体布局飞行器的三通道解耦控制面

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Also Published As

Publication number Publication date
BR0318083A (pt) 2005-12-06
EP1587734B1 (de) 2006-11-29
IL169894A0 (en) 2007-07-04
WO2004108526A1 (en) 2004-12-16
US7448578B2 (en) 2008-11-11
ATE346791T1 (de) 2006-12-15
AU2003304182A1 (en) 2005-01-04
CA2514825A1 (en) 2004-12-16
EP1587734A1 (de) 2005-10-26
KR20050095907A (ko) 2005-10-04
DE60310138T2 (de) 2007-10-11
US20060102802A1 (en) 2006-05-18
US20040144893A1 (en) 2004-07-29
US6892982B2 (en) 2005-05-17
JP2006514591A (ja) 2006-05-11

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Legal Events

Date Code Title Description
8381 Inventor (new situation)

Inventor name: CLARK, WALTER, FULLERTON, CA 92835, US

8364 No opposition during term of opposition