DE1068999B - - Google Patents

Info

Publication number
DE1068999B
DE1068999B DENDAT1068999D DE1068999DA DE1068999B DE 1068999 B DE1068999 B DE 1068999B DE NDAT1068999 D DENDAT1068999 D DE NDAT1068999D DE 1068999D A DE1068999D A DE 1068999DA DE 1068999 B DE1068999 B DE 1068999B
Authority
DE
Germany
Prior art keywords
nacelle
flow
swiveled
engines
engine
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.)
Pending
Application number
DENDAT1068999D
Other languages
German (de)
English (en)
Publication date
Publication of DE1068999B publication Critical patent/DE1068999B/de
Pending legal-status Critical Current

Links

Classifications

    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C29/00—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft
    • B64C29/0008—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded
    • B64C29/0041—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors
    • B64C29/0075—Aircraft capable of landing or taking-off vertically, e.g. vertical take-off and landing [VTOL] aircraft having its flight directional axis horizontal when grounded the lift during taking-off being created by jet motors the motors being tiltable relative to the fuselage
    • 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
    • B64C21/06—Influencing air flow over aircraft surfaces by affecting boundary layer flow by use of slot, ducts, porous areas or the like for sucking
    • 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
    • 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)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
DENDAT1068999D Pending DE1068999B (fr)

Publications (1)

Publication Number Publication Date
DE1068999B true DE1068999B (fr) 1959-11-12

Family

ID=594223

Family Applications (1)

Application Number Title Priority Date Filing Date
DENDAT1068999D Pending DE1068999B (fr)

Country Status (1)

Country Link
DE (1) DE1068999B (fr)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE1140779B (de) * 1960-05-07 1962-12-06 M A N Turbomotoren G M B H Verstellbarer Lufteinlauf fuer Strahltriebwerke
US3099422A (en) * 1959-10-30 1963-07-30 Messerschmitt Ag Tiltable pod for jet power units on aircraft

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3099422A (en) * 1959-10-30 1963-07-30 Messerschmitt Ag Tiltable pod for jet power units on aircraft
DE1140779B (de) * 1960-05-07 1962-12-06 M A N Turbomotoren G M B H Verstellbarer Lufteinlauf fuer Strahltriebwerke

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