DE2821913A1 - System zur beeinflussung der grenzschicht an flugzeugen - Google Patents

System zur beeinflussung der grenzschicht an flugzeugen

Info

Publication number
DE2821913A1
DE2821913A1 DE19782821913 DE2821913A DE2821913A1 DE 2821913 A1 DE2821913 A1 DE 2821913A1 DE 19782821913 DE19782821913 DE 19782821913 DE 2821913 A DE2821913 A DE 2821913A DE 2821913 A1 DE2821913 A1 DE 2821913A1
Authority
DE
Germany
Prior art keywords
boundary layer
aircraft
air
wing
outboard
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.)
Granted
Application number
DE19782821913
Other languages
German (de)
English (en)
Other versions
DE2821913C2 (enrdf_load_stackoverflow
Inventor
Everts Walfred Swanson
Marvin Dale Wehrman
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.)
Boeing Co
Original Assignee
Boeing Co
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 Boeing Co filed Critical Boeing Co
Priority to DE19782821913 priority Critical patent/DE2821913A1/de
Publication of DE2821913A1 publication Critical patent/DE2821913A1/de
Application granted granted Critical
Publication of DE2821913C2 publication Critical patent/DE2821913C2/de
Granted legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C21/00—Influencing air flow over aircraft surfaces by affecting boundary layer flow
    • B64C21/02—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like
    • B64C21/04—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for blowing
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/04—Boundary layer controls by actively generating fluid flow
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C2230/00—Boundary layer controls
    • B64C2230/06—Boundary layer controls by explicitly adjusting fluid flow, e.g. by using valves, variable aperture or slot areas, variable pump action or variable fluid pressure
    • 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

Landscapes

  • Engineering & Computer Science (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • Aerodynamic Tests, Hydrodynamic Tests, Wind Tunnels, And Water Tanks (AREA)
DE19782821913 1978-05-17 1978-05-17 System zur beeinflussung der grenzschicht an flugzeugen Granted DE2821913A1 (de)

Priority Applications (1)

Application Number Priority Date Filing Date Title
DE19782821913 DE2821913A1 (de) 1978-05-17 1978-05-17 System zur beeinflussung der grenzschicht an flugzeugen

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19782821913 DE2821913A1 (de) 1978-05-17 1978-05-17 System zur beeinflussung der grenzschicht an flugzeugen

Publications (2)

Publication Number Publication Date
DE2821913A1 true DE2821913A1 (de) 1979-11-22
DE2821913C2 DE2821913C2 (enrdf_load_stackoverflow) 1988-04-21

Family

ID=6039746

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19782821913 Granted DE2821913A1 (de) 1978-05-17 1978-05-17 System zur beeinflussung der grenzschicht an flugzeugen

Country Status (1)

Country Link
DE (1) DE2821913A1 (enrdf_load_stackoverflow)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19747308A1 (de) * 1997-10-27 1999-07-15 Seemann Christina Vorrichtung zur Steigerung des dynamischen Auftriebs bei Flugzeugen und anderen Transportsystemen
US20240076033A1 (en) * 2022-09-02 2024-03-07 Raytheon Technologies Corporation Aerial vehicle fluid control system integrated with gas turbine engine

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
RU2165585C1 (ru) * 1999-09-20 2001-04-20 Государственное унитарное предприятие "Конструкторское бюро приборостроения" Способ управления полетом управляемого летательного аппарата и управляемый летательный аппарат

Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3889903A (en) * 1973-03-09 1975-06-17 Boeing Co Airfoil leading edge structure with boundary layer control

Patent Citations (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3889903A (en) * 1973-03-09 1975-06-17 Boeing Co Airfoil leading edge structure with boundary layer control

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE19747308A1 (de) * 1997-10-27 1999-07-15 Seemann Christina Vorrichtung zur Steigerung des dynamischen Auftriebs bei Flugzeugen und anderen Transportsystemen
US20240076033A1 (en) * 2022-09-02 2024-03-07 Raytheon Technologies Corporation Aerial vehicle fluid control system integrated with gas turbine engine
US12208884B2 (en) * 2022-09-02 2025-01-28 Rtx Corporation Aerial vehicle fluid control system integrated with gas turbine engine

Also Published As

Publication number Publication date
DE2821913C2 (enrdf_load_stackoverflow) 1988-04-21

Similar Documents

Publication Publication Date Title
DE3121653C2 (enrdf_load_stackoverflow)
DE3811614C1 (enrdf_load_stackoverflow)
DE2359518C3 (de) Hubdüseneinrichtung für ein Flugzeug
DE3346809A1 (de) Axialsymmetrische schubduese mit veraenderbarer querschnittsflaeche
DE4008956A1 (de) Einlaufsystem fuer ueber- oder hyperschallflugzeuge
DE1228107B (de) Strahltriebwerk-Schubduese
EP0454696B1 (de) Schubdüse
DE2743371A1 (de) Kombiniertes heissgas-servosteuersystem fuer ruder und rueckstoss bei flugkoerpern
EP3366907B1 (de) Konvergent-divergente schubdüse für ein turbofan-triebwerk eines überschallflugzeugs und verfahren zur einstellung der düsenhalsfläche in einer schubdüse eines turbofan-triebwerks
DE2037407A1 (de) Ruckschlag und Schuburrikehrvorrichtung rurFVmäUanak
DE3106644A1 (de) "einlassverkleidung fuer einen zweidimensionalen gasturbinentriebwerkseinlass"
EP0942792A2 (de) Vorrichtung zur abkühlung von strangpressprofilen
DE1202648B (de) Trimmeinrichtung fuer ein Gaskissenfahrzeug
DE2821913A1 (de) System zur beeinflussung der grenzschicht an flugzeugen
DE3934268C2 (enrdf_load_stackoverflow)
DE2105077A1 (de) Vorrichtung zum gleichmäßigen Verteilen von Luft innerhalb von an Luftverteilkanäle einer Klimaanlage angeschlossenen Räumen
DE1069952C2 (de) Vorrichtung zur Schubregelung von Heißstrahltriebwerken
WO2022194770A1 (de) Profilkühlvorrichtung und kühlstrang für eine profilkühlvorrichtung
DE60200153T2 (de) Lufteinlasskanal und Flugkörper, insbesondere Rakete, mit einem solchen Lufteinlasskanal
GB1600454A (en) Boundary layer control system for aircraft
DE3803412C1 (en) Multilayer extrusion apparatus
DE1506580A1 (de) Steuerbarer Luftausblasespalt an Flugzeugtragflaechen
DE2913350A1 (de) Strahltriebwerk fuer lenkflugkoerper
DE4223413C2 (de) Einlaufsystem für Über- und Hyperschallflugzeuge
DE2856033A1 (de) Einrichtung zur steuerung und stabilisierung von fluggeraeten

Legal Events

Date Code Title Description
8110 Request for examination paragraph 44
D2 Grant after examination
8364 No opposition during term of opposition
8339 Ceased/non-payment of the annual fee