FR1365515A - Dispositif amplificateur d'un signal de pression, applicable notamment à la régulation des avions en vol d'approche d'atterrissage - Google Patents
Dispositif amplificateur d'un signal de pression, applicable notamment à la régulation des avions en vol d'approche d'atterrissageInfo
- Publication number
- FR1365515A FR1365515A FR935977A FR935977A FR1365515A FR 1365515 A FR1365515 A FR 1365515A FR 935977 A FR935977 A FR 935977A FR 935977 A FR935977 A FR 935977A FR 1365515 A FR1365515 A FR 1365515A
- Authority
- FR
- France
- Prior art keywords
- airplanes
- amplifying
- regulation
- applicable
- pressure signal
- 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.)
- Expired
Links
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D1/00—Control of position, course, altitude or attitude of land, water, air or space vehicles, e.g. using automatic pilots
- G05D1/04—Control of altitude or depth
- G05D1/06—Rate of change of altitude or depth
- G05D1/0607—Rate of change of altitude or depth specially adapted for aircraft
- G05D1/0653—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing
- G05D1/0676—Rate of change of altitude or depth specially adapted for aircraft during a phase of take-off or landing specially adapted for landing
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D17/00—Regulating or controlling by varying flow
- F01D17/02—Arrangement of sensing elements
- F01D17/08—Arrangement of sensing elements responsive to condition of working-fluid, e.g. pressure
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F15—FLUID-PRESSURE ACTUATORS; HYDRAULICS OR PNEUMATICS IN GENERAL
- F15C—FLUID-CIRCUIT ELEMENTS PREDOMINANTLY USED FOR COMPUTING OR CONTROL PURPOSES
- F15C4/00—Circuit elements characterised by their special functions
-
- 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
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T137/00—Fluid handling
- Y10T137/2278—Pressure modulating relays or followers
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Physics & Mathematics (AREA)
- Mechanical Engineering (AREA)
- Theoretical Computer Science (AREA)
- Fluid Mechanics (AREA)
- Aviation & Aerospace Engineering (AREA)
- Radar, Positioning & Navigation (AREA)
- Remote Sensing (AREA)
- General Physics & Mathematics (AREA)
- Automation & Control Theory (AREA)
- Measuring Fluid Pressure (AREA)
Priority Applications (4)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR935977A FR1365515A (fr) | 1963-05-24 | 1963-05-24 | Dispositif amplificateur d'un signal de pression, applicable notamment à la régulation des avions en vol d'approche d'atterrissage |
US36950464 US3324870A (en) | 1963-05-24 | 1964-05-22 | Pressure-signal amplifying device, especially applicable to the regulation of aircraft in flight during landingapproach |
CH670064A CH437000A (fr) | 1963-05-24 | 1964-05-22 | Relais |
GB2137564A GB1065089A (en) | 1963-05-24 | 1964-05-22 | A pressure-signal amplifying device, especially applicable to the regulation of aircraft in flight during landing-approach |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR935977A FR1365515A (fr) | 1963-05-24 | 1963-05-24 | Dispositif amplificateur d'un signal de pression, applicable notamment à la régulation des avions en vol d'approche d'atterrissage |
Publications (1)
Publication Number | Publication Date |
---|---|
FR1365515A true FR1365515A (fr) | 1964-07-03 |
Family
ID=8804632
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR935977A Expired FR1365515A (fr) | 1963-05-24 | 1963-05-24 | Dispositif amplificateur d'un signal de pression, applicable notamment à la régulation des avions en vol d'approche d'atterrissage |
Country Status (4)
Country | Link |
---|---|
US (1) | US3324870A (fr) |
CH (1) | CH437000A (fr) |
FR (1) | FR1365515A (fr) |
GB (1) | GB1065089A (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3812873A (en) * | 1971-11-18 | 1974-05-28 | Johnson Service Co | Fluid signal limiting device |
US4235829A (en) * | 1979-05-07 | 1980-11-25 | Western Electric Company, Inc. | Vapor delivery system and method of maintaining a constant level of liquid therein |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2682893A (en) * | 1950-05-16 | 1954-07-06 | Solar Aircraft Co | Surge arrestor |
US2934898A (en) * | 1953-09-29 | 1960-05-03 | Curtiss Wright Corp | Jet engine thrust control system |
US2979068A (en) * | 1956-09-27 | 1961-04-11 | Taylor Instrument Co | Step-type control system and relay therefor |
US3078670A (en) * | 1958-07-16 | 1963-02-26 | Bmw Triebwerkbau Gmbh | Fuel control system responsive to ambient conditions for combustion turbine power plants |
US3075351A (en) * | 1960-04-08 | 1963-01-29 | Bendix Corp | Control for hydraulic servo-actuated apparatus |
-
1963
- 1963-05-24 FR FR935977A patent/FR1365515A/fr not_active Expired
-
1964
- 1964-05-22 CH CH670064A patent/CH437000A/fr unknown
- 1964-05-22 US US36950464 patent/US3324870A/en not_active Expired - Lifetime
- 1964-05-22 GB GB2137564A patent/GB1065089A/en not_active Expired
Also Published As
Publication number | Publication date |
---|---|
CH437000A (fr) | 1967-05-31 |
US3324870A (en) | 1967-06-13 |
GB1065089A (en) | 1967-04-12 |
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