GB760111A - Improvements in or relating to mass flow control systems - Google Patents
Improvements in or relating to mass flow control systemsInfo
- Publication number
- GB760111A GB760111A GB1258153A GB1258153A GB760111A GB 760111 A GB760111 A GB 760111A GB 1258153 A GB1258153 A GB 1258153A GB 1258153 A GB1258153 A GB 1258153A GB 760111 A GB760111 A GB 760111A
- Authority
- GB
- United Kingdom
- Prior art keywords
- conduit
- flow
- air
- duct
- venturi
- 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
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
-
- 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
- B64D13/00—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
- B64D13/02—Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
- B64D13/04—Automatic control of pressure
Landscapes
- Health & Medical Sciences (AREA)
- General Health & Medical Sciences (AREA)
- Pulmonology (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Measuring Volume Flow (AREA)
Abstract
760,111. Automatic air-flow control systems. NORMALAIR, Ltd. May 6, 1954 [May 6, 1953], No. 12581/53. Class 38 (4). In a system for maintaining constant mass air-flow through a duct to the pressurized cabin of an aircraft in which the pressure difference in a venturi-type head measuring airflow in the duct controls electrical contacts energizing an electrically operated flow valve in the duct, the venturi is automatically throttled in response to pressure in the duct. In Fig. 1, air supplied to conduits 10 from port and starboard aircraft engines, respectively, passes through refrigerators s and non-return valves t to a common conduit 13 leading to the aircraft cabin. In each conduit 10 a venturi tube 1 measuring air-flow is arranged to maintain constant mass air-flow by electrically controlling a valve 2. In order to increase airflow automatically whenever a refrigerator s is put into operation, the increase in back pressure resulting from putting the refrigerator into operation influences a piston 3 through a conduit 14 to move a spring-loaded rod 4 into the throat of venturi tube 1. In the event of failure of one of the aircraft engines, the resulting drop of pressure in the corresponding conduit 10 allows an associated spring-loaded piston 6 to be moved so that the pressure in the other conduit 10 is effective through an associated non-return valve 9 and conduit 8 to influence pistons 16 moving rod 4 into the venturi throat so as to increase air flow from the engine still functioning. Specifications 655,328 and 656,763 are referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1258153A GB760111A (en) | 1953-05-06 | 1953-05-06 | Improvements in or relating to mass flow control systems |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1258153A GB760111A (en) | 1953-05-06 | 1953-05-06 | Improvements in or relating to mass flow control systems |
Publications (1)
Publication Number | Publication Date |
---|---|
GB760111A true GB760111A (en) | 1956-10-31 |
Family
ID=10007268
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1258153A Expired GB760111A (en) | 1953-05-06 | 1953-05-06 | Improvements in or relating to mass flow control systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB760111A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0087935A2 (en) * | 1982-02-25 | 1983-09-07 | The Garrett Corporation | Fluid flow control system |
EP0190943A2 (en) * | 1985-02-08 | 1986-08-13 | AlliedSignal Inc. | Aircraft engine bleed air flow balancing technique |
-
1953
- 1953-05-06 GB GB1258153A patent/GB760111A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0087935A2 (en) * | 1982-02-25 | 1983-09-07 | The Garrett Corporation | Fluid flow control system |
EP0087935A3 (en) * | 1982-02-25 | 1985-12-18 | The Garrett Corporation | Fluid flow control system |
EP0190943A2 (en) * | 1985-02-08 | 1986-08-13 | AlliedSignal Inc. | Aircraft engine bleed air flow balancing technique |
EP0190943A3 (en) * | 1985-02-08 | 1987-10-28 | The Garrett Corporation | Aircraft engine bleed air flow balancing technique |
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