GB760111A - Improvements in or relating to mass flow control systems - Google Patents

Improvements in or relating to mass flow control systems

Info

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
Application number
GB1258153A
Inventor
John Grieve
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.)
Normalair Ltd
Original Assignee
Normalair Ltd
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 Normalair Ltd filed Critical Normalair Ltd
Priority to GB1258153A priority Critical patent/GB760111A/en
Publication of GB760111A publication Critical patent/GB760111A/en
Expired legal-status Critical Current

Links

Classifications

    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/02Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • BPERFORMING OPERATIONS; TRANSPORTING
    • B64AIRCRAFT; AVIATION; COSMONAUTICS
    • B64DEQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
    • B64D13/00Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft
    • B64D13/02Arrangements or adaptations of air-treatment apparatus for aircraft crew or passengers, or freight space, or structural parts of the aircraft the air being pressurised
    • B64D13/04Automatic 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.
GB1258153A 1953-05-06 1953-05-06 Improvements in or relating to mass flow control systems Expired GB760111A (en)

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)

* Cited by examiner, † Cited by third party
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

Cited By (4)

* Cited by examiner, † Cited by third party
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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