FR2252489A1 - - Google Patents

Info

Publication number
FR2252489A1
FR2252489A1 FR7438741A FR7438741A FR2252489A1 FR 2252489 A1 FR2252489 A1 FR 2252489A1 FR 7438741 A FR7438741 A FR 7438741A FR 7438741 A FR7438741 A FR 7438741A FR 2252489 A1 FR2252489 A1 FR 2252489A1
Authority
FR
France
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
FR7438741A
Other languages
French (fr)
Other versions
FR2252489B1 (de
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.)
Airbus Defence and Space GmbH
Original Assignee
Messerschmitt Bolkow Blohm AG
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 Bolkow Blohm AG filed Critical Messerschmitt Bolkow Blohm AG
Publication of FR2252489A1 publication Critical patent/FR2252489A1/fr
Application granted granted Critical
Publication of FR2252489B1 publication Critical patent/FR2252489B1/fr
Expired 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
    • 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)
FR7438741A 1973-11-27 1974-11-26 Expired FR2252489B1 (de)

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 (2)

Publication Number Publication Date
FR2252489A1 true FR2252489A1 (de) 1975-06-20
FR2252489B1 FR2252489B1 (de) 1978-09-22

Family

ID=5899148

Family Applications (1)

Application Number Title Priority Date Filing Date
FR7438741A Expired FR2252489B1 (de) 1973-11-27 1974-11-26

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)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2511339A1 (fr) * 1978-08-02 1983-02-18 Messerschmitt Boelkow Blohm Entree d'air reglable, notamment diffuseur bidimensionnel a choc oblique pour turboreacteurs d'entrainement d'aeronefs a haute puissance

Families Citing this family (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
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

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2511339A1 (fr) * 1978-08-02 1983-02-18 Messerschmitt Boelkow Blohm Entree d'air reglable, notamment diffuseur bidimensionnel a choc oblique pour turboreacteurs d'entrainement d'aeronefs a haute puissance

Also Published As

Publication number Publication date
DE2358926A1 (de) 1975-05-28
IN144247B (de) 1978-04-15
IT1025770B (it) 1978-08-30
GB1480366A (en) 1977-07-20
DE2358926B2 (de) 1978-12-07
DE2358926C3 (de) 1979-08-02
FR2252489B1 (de) 1978-09-22

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Legal Events

Date Code Title Description
ST Notification of lapse