GB2107021A - Jet engine air intakes - Google Patents

Jet engine air intakes Download PDF

Info

Publication number
GB2107021A
GB2107021A GB08226461A GB8226461A GB2107021A GB 2107021 A GB2107021 A GB 2107021A GB 08226461 A GB08226461 A GB 08226461A GB 8226461 A GB8226461 A GB 8226461A GB 2107021 A GB2107021 A GB 2107021A
Authority
GB
United Kingdom
Prior art keywords
boundary layer
inlet duct
air
flow
corner
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.)
Withdrawn
Application number
GB08226461A
Other languages
English (en)
Inventor
Dr P Armin Mackrodt
Dr Gerhard Hefer
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.)
Deutsches Zentrum fuer Luft und Raumfahrt eV
Original Assignee
Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
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 Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR filed Critical Deutsche Forschungs und Versuchsanstalt fuer Luft und Raumfahrt eV DFVLR
Publication of GB2107021A publication Critical patent/GB2107021A/en
Withdrawn legal-status Critical Current

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
    • F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Jet Pumps And Other Pumps (AREA)
  • Supercharger (AREA)
GB08226461A 1981-09-25 1982-09-16 Jet engine air intakes Withdrawn GB2107021A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE3138149A DE3138149C2 (de) 1981-09-25 1981-09-25 Verfahren und Vorrichtung zur Vergleichmäßigung der Gesamtdruckverteilung in der Verdichtereintrittsebene des Einlaufkanals von Luftsaugenden Triebwerken

Publications (1)

Publication Number Publication Date
GB2107021A true GB2107021A (en) 1983-04-20

Family

ID=6142563

Family Applications (1)

Application Number Title Priority Date Filing Date
GB08226461A Withdrawn GB2107021A (en) 1981-09-25 1982-09-16 Jet engine air intakes

Country Status (5)

Country Link
DE (1) DE3138149C2 (fr)
FR (1) FR2513703A1 (fr)
GB (1) GB2107021A (fr)
IL (1) IL66802A0 (fr)
SE (1) SE8205483L (fr)

Family Cites Families (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB223202A (fr) * 1923-10-08 1925-11-05 N. V. Instituut Voor Aero- En Hydrodynamiek
SE318194B (fr) * 1968-06-24 1969-12-01 Saab Ab

Also Published As

Publication number Publication date
SE8205483L (sv) 1983-03-26
FR2513703A1 (fr) 1983-04-01
SE8205483D0 (sv) 1982-09-24
DE3138149C2 (de) 1984-03-15
DE3138149A1 (de) 1983-04-14
IL66802A0 (en) 1982-12-31

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Legal Events

Date Code Title Description
WAP Application withdrawn, taken to be withdrawn or refused ** after publication under section 16(1)
PCNP Patent ceased through non-payment of renewal fee