IT1025770B - Sistema di regolazione dell entrata dell aria per fropulsori di aerei - Google Patents

Sistema di regolazione dell entrata dell aria per fropulsori di aerei

Info

Publication number
IT1025770B
IT1025770B IT2953174A IT2953174A IT1025770B IT 1025770 B IT1025770 B IT 1025770B IT 2953174 A IT2953174 A IT 2953174A IT 2953174 A IT2953174 A IT 2953174A IT 1025770 B IT1025770 B IT 1025770B
Authority
IT
Italy
Prior art keywords
pulsers
aircraft
air inlet
adjustment system
inlet adjustment
Prior art date
Application number
IT2953174A
Other languages
English (en)
Italian (it)
Original Assignee
Messerschmitt Boelkow Blohm
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 Messerschmitt Boelkow Blohm filed Critical Messerschmitt Boelkow Blohm
Application granted granted Critical
Publication of IT1025770B publication Critical patent/IT1025770B/it

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
    • F02C7/057—Control or regulation
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F05—INDEXING SCHEMES RELATING TO ENGINES OR PUMPS IN VARIOUS SUBCLASSES OF CLASSES F01-F04
    • F05D—INDEXING SCHEME FOR ASPECTS RELATING TO NON-POSITIVE-DISPLACEMENT MACHINES OR ENGINES, GAS-TURBINES OR JET-PROPULSION PLANTS
    • F05D2200/00—Mathematical features
    • F05D2200/10—Basic functions
    • F05D2200/11—Sum

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Feedback Control In General (AREA)
  • Control Of Turbines (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
IT2953174A 1973-11-27 1974-11-18 Sistema di regolazione dell entrata dell aria per fropulsori di aerei IT1025770B (it)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
DE19732358926 DE2358926C3 (de) 1973-11-27 1973-11-27 Regelung von verstellbaren Überschallufteinläufen, insbesondere zweidimensionalen SchrägstoBdiffusoren für Gasturbinenstrahltriebwerke zum Antrieb von Hochleistungsflugzeugen

Publications (1)

Publication Number Publication Date
IT1025770B true IT1025770B (it) 1978-08-30

Family

ID=5899148

Family Applications (1)

Application Number Title Priority Date Filing Date
IT2953174A IT1025770B (it) 1973-11-27 1974-11-18 Sistema di regolazione dell entrata dell aria per fropulsori di aerei

Country Status (5)

Country Link
DE (1) DE2358926C3 (de)
FR (1) FR2252489B1 (de)
GB (1) GB1480366A (de)
IN (1) IN144247B (de)
IT (1) IT1025770B (de)

Families Citing this family (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE2833771C2 (de) * 1978-08-02 1985-12-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verstellbarer Lufteinlauf, insbesondere zweidimensionaler Schrägstoßdiffusor für Gasturbinenstrahltriebwerke zum Antrieb von Hochleistungsflugzeugen
US4523603A (en) * 1978-08-02 1985-06-18 Peikert Juergen Air intake control for an adjustable air inlet, particularly two-dimensional oblique shock diffuser for gas turbine jet engines for the propulsion of high performance aircraft
DE2846972C1 (de) * 1978-10-28 1986-07-17 Messerschmitt-Bölkow-Blohm GmbH, 8012 Ottobrunn Verstellbarer Lufteinlauf,insbesondere zweidimensionaler Schraegstossdiffusor fuer Gasturbinenstrahltriebwerke zum Antrieb von Flugzeugen
US6272838B1 (en) * 1999-02-25 2001-08-14 Alliedsignal, Inc. Method and apparatus for controlling the inlet duct leading to an auxiliary power unit
EP3412563B1 (de) 2017-06-08 2022-11-23 Airbus Defence and Space GmbH Variabler und anpassbarer umlenkungsloser höckereinlass
CN111216905B (zh) * 2020-01-09 2023-04-18 中国航空工业集团公司沈阳飞机设计研究所 一种采用非线性控制律控制斜板起调角度的方法

Also Published As

Publication number Publication date
DE2358926C3 (de) 1979-08-02
IN144247B (de) 1978-04-15
DE2358926A1 (de) 1975-05-28
DE2358926B2 (de) 1978-12-07
GB1480366A (en) 1977-07-20
FR2252489B1 (de) 1978-09-22
FR2252489A1 (de) 1975-06-20

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