DE3835668A1 - Steuerbarer lufteinlauf fuer hochleistungsflugzeuge - Google Patents
Steuerbarer lufteinlauf fuer hochleistungsflugzeugeInfo
- Publication number
- DE3835668A1 DE3835668A1 DE19883835668 DE3835668A DE3835668A1 DE 3835668 A1 DE3835668 A1 DE 3835668A1 DE 19883835668 DE19883835668 DE 19883835668 DE 3835668 A DE3835668 A DE 3835668A DE 3835668 A1 DE3835668 A1 DE 3835668A1
- Authority
- DE
- Germany
- Prior art keywords
- signal
- air
- lip
- air inlet
- signals
- 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.)
- Granted
Links
- 238000005259 measurement Methods 0.000 claims description 5
- 238000000034 method Methods 0.000 claims description 3
- 230000001960 triggered effect Effects 0.000 claims 2
- YAFQFNOUYXZVPZ-UHFFFAOYSA-N liproxstatin-1 Chemical compound ClC1=CC=CC(CNC=2C3(CCNCC3)NC3=CC=CC=C3N=2)=C1 YAFQFNOUYXZVPZ-UHFFFAOYSA-N 0.000 description 18
- RZVHIXYEVGDQDX-UHFFFAOYSA-N 9,10-anthraquinone Chemical compound C1=CC=C2C(=O)C3=CC=CC=C3C(=O)C2=C1 RZVHIXYEVGDQDX-UHFFFAOYSA-N 0.000 description 3
- 230000008878 coupling Effects 0.000 description 1
- 238000010168 coupling process Methods 0.000 description 1
- 238000005859 coupling reaction Methods 0.000 description 1
- 230000001419 dependent effect Effects 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005086 pumping Methods 0.000 description 1
- 230000001105 regulatory effect Effects 0.000 description 1
- 230000011664 signaling Effects 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 230000001360 synchronised effect Effects 0.000 description 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- 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
- F02C7/042—Air intakes for gas-turbine plants or jet-propulsion plants having variable geometry
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0253—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
- B64D2033/026—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Physics & Mathematics (AREA)
- Geometry (AREA)
- Combined Controls Of Internal Combustion Engines (AREA)
- Toys (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19883835668 DE3835668A1 (de) | 1988-10-20 | 1988-10-20 | Steuerbarer lufteinlauf fuer hochleistungsflugzeuge |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE19883835668 DE3835668A1 (de) | 1988-10-20 | 1988-10-20 | Steuerbarer lufteinlauf fuer hochleistungsflugzeuge |
Publications (2)
Publication Number | Publication Date |
---|---|
DE3835668A1 true DE3835668A1 (de) | 1990-04-26 |
DE3835668C2 DE3835668C2 (enrdf_load_stackoverflow) | 1990-11-29 |
Family
ID=6365492
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
DE19883835668 Granted DE3835668A1 (de) | 1988-10-20 | 1988-10-20 | Steuerbarer lufteinlauf fuer hochleistungsflugzeuge |
Country Status (1)
Country | Link |
---|---|
DE (1) | DE3835668A1 (enrdf_load_stackoverflow) |
Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2833771A1 (de) * | 1978-08-02 | 1982-09-09 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verstellbarer lufteinlauf, insbesondere zweidimensionaler schraegstossdiffusor fuer gasturbinenstrahltriebwerke zum antrieb von hochleistungsflugzeugen |
-
1988
- 1988-10-20 DE DE19883835668 patent/DE3835668A1/de active Granted
Patent Citations (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2833771A1 (de) * | 1978-08-02 | 1982-09-09 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Verstellbarer lufteinlauf, insbesondere zweidimensionaler schraegstossdiffusor fuer gasturbinenstrahltriebwerke zum antrieb von hochleistungsflugzeugen |
Non-Patent Citations (3)
Title |
---|
GB-Z.: "Flight International", 12. Sept. 1974, S. 313-315 * |
GB-Z.: "Oil engine and Gas Turbine", Bd. 32, Sept. 1964, S. 36-39 * |
US-ASME-Paper 61-AV-65 * |
Also Published As
Publication number | Publication date |
---|---|
DE3835668C2 (enrdf_load_stackoverflow) | 1990-11-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP3479181B1 (de) | Verfahren und assistenzsystem zur detektion einer flugleistungsdegradierung | |
DE602005000027T2 (de) | Verfahren und Vorrichtung zum Optimiern des Spoilerausschlags eines Flugzeuges während des Fluges | |
DE1271557B (de) | Flugzeug mit mindestens einem Strahltriebwerk zur Vortriebserzeugung | |
DE3421441C2 (enrdf_load_stackoverflow) | ||
DE102010027081A1 (de) | Früherkennung eines Wirbelringstadiums | |
DE3437824C3 (de) | Unbemannter Flugkörper mit einem Fallschirmbergesystem | |
DE69709838T2 (de) | Verfahren und Vorrichtung zur Detektion von Windstössen in einem Luftfahrzeug | |
DE4421139A1 (de) | Luftfahrzeug | |
DE602004000178T2 (de) | Verfahren und Vorrichtung zur Triebwerkstreibstoffzufuhr bei einem Flugzeug im Automatikflug | |
DE3835668C2 (enrdf_load_stackoverflow) | ||
DE2255760C3 (de) | Regler, insbesondere zur Fluglagesteuerung eines mit Gasturbinentriebwerken ausgerüsteten Flugzeugs | |
DE3835667C2 (enrdf_load_stackoverflow) | ||
DE3835669C2 (enrdf_load_stackoverflow) | ||
DE4436356A1 (de) | Verfahren zur Flugweggenerierung | |
DE602004000484T2 (de) | Verfahren und Vorrichtung zur Trimmwinkelregelung eines Flugzeugs | |
DE3835663C2 (enrdf_load_stackoverflow) | ||
DE202015104591U1 (de) | Hubschrauber mit mehreren Rotoren und variabler Blattsteigung | |
DE3835664C2 (enrdf_load_stackoverflow) | ||
DE3835665C2 (enrdf_load_stackoverflow) | ||
DE4310017C2 (de) | Transportflugzeug mit stumpfem Heck | |
DE2012243B1 (de) | Flugzeug mit Deltaflügel | |
DE10022819C1 (de) | Verfahren und Vorrichtung zur Vermeidung der Kolllision eines rotierenden Rotorblattes eines Drehflüglers mit Blattwirbeln | |
DE102004045732A1 (de) | Flugzeug mit Flügeln, deren maximaler Auftrieb durch steuerbare Flügelkomponenten veränderbar ist | |
DE2630651A1 (de) | Total-energie-steuerungssystem fuer flugzeuge | |
DE3517352C2 (enrdf_load_stackoverflow) |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
OP8 | Request for examination as to paragraph 44 patent law | ||
D2 | Grant after examination | ||
8364 | No opposition during term of opposition | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: DEUTSCHE AEROSPACE AG, 8000 MUENCHEN, DE |
|
8320 | Willingness to grant licenses declared (paragraph 23) | ||
8327 | Change in the person/name/address of the patent owner |
Owner name: DAIMLER-BENZ AEROSPACE AKTIENGESELLSCHAFT, 80804 M |
|
8339 | Ceased/non-payment of the annual fee |