DE2821913C2 - - Google Patents

Info

Publication number
DE2821913C2
DE2821913C2 DE2821913A DE2821913A DE2821913C2 DE 2821913 C2 DE2821913 C2 DE 2821913C2 DE 2821913 A DE2821913 A DE 2821913A DE 2821913 A DE2821913 A DE 2821913A DE 2821913 C2 DE2821913 C2 DE 2821913C2
Authority
DE
Germany
Prior art keywords
wing
nozzle
pipe
pipe system
nozzle chambers
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
Application number
DE2821913A
Other languages
German (de)
English (en)
Other versions
DE2821913A1 (de
Inventor
Marvin Dale Seattle Wash. Us Wehrman
Everts Walfred Edmonds Wash. Us Swanson
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 DE2821913A1 (de) 1979-11-22
DE2821913C2 true 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 (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

Families Citing this family (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
US12208884B2 (en) * 2022-09-02 2025-01-28 Rtx Corporation Aerial vehicle fluid control system integrated with gas turbine engine

Family Cites Families (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 (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

Also Published As

Publication number Publication date
DE2821913A1 (de) 1979-11-22

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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