GB1104849A - Improvements in or relating to oxygen regulators - Google Patents

Improvements in or relating to oxygen regulators

Info

Publication number
GB1104849A
GB1104849A GB4410065A GB4410065A GB1104849A GB 1104849 A GB1104849 A GB 1104849A GB 4410065 A GB4410065 A GB 4410065A GB 4410065 A GB4410065 A GB 4410065A GB 1104849 A GB1104849 A GB 1104849A
Authority
GB
United Kingdom
Prior art keywords
oxygen
mask
pressure
transducer
altitude
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
GB4410065A
Inventor
Edgar William James Basham
Kenneth Wilfrid Tizard
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.)
Westland Group PLC
Original Assignee
Westland Aircraft 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 Westland Aircraft Ltd filed Critical Westland Aircraft Ltd
Priority to GB4410065A priority Critical patent/GB1104849A/en
Priority to DE19661559692 priority patent/DE1559692B1/en
Publication of GB1104849A publication Critical patent/GB1104849A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G05CONTROLLING; REGULATING
    • G05DSYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
    • G05D16/00Control of fluid pressure
    • G05D16/20Control of fluid pressure characterised by the use of electric means
    • G05D16/2006Control of fluid pressure characterised by the use of electric means with direct action of electric energy on controlling means
    • G05D16/2013Control of fluid pressure characterised by the use of electric means with direct action of electric energy on controlling means using throttling means as controlling means
    • G05D16/2026Control of fluid pressure characterised by the use of electric means with direct action of electric energy on controlling means using throttling means as controlling means with a plurality of throttling means
    • G05D16/2046Control of fluid pressure characterised by the use of electric means with direct action of electric energy on controlling means using throttling means as controlling means with a plurality of throttling means the plurality of throttling means being arranged for the control of a single pressure from a plurality of converging pressures
    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62BDEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B7/00Respiratory apparatus
    • A62B7/14Respiratory apparatus for high-altitude aircraft

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • Health & Medical Sciences (AREA)
  • General Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Automation & Control Theory (AREA)
  • Pulmonology (AREA)
  • General Health & Medical Sciences (AREA)
  • Business, Economics & Management (AREA)
  • Emergency Management (AREA)
  • Respiratory Apparatuses And Protective Means (AREA)

Abstract

1,104,849. Regulating apparatus for respiration. WESTLAND AIRCRAFT Ltd. 13 Oct., 1966 [18 Oct., 1965], No. 44100/65. Heading AST. [Also in Division G3] An automatic regulating apparatus for an aviator's mask 1 comprises an oxygen supply valve 2, a (conventional) sensor 3 responsive to the partial pressure of the oxygen in the mask, a pressure transducer 4 responsive to the pressure difference between the inside and outside of the mask. a combined expiratory and air-intake valve 5, and an electronic control circuit 13 - - 22 arranged to vary the ratio of air to oxygen to maintain a desired partial pressure of oxygen in the mask. The signals from sensors 3, 4 are combined to produce from member 20 positive and negative pulses of which the latter cause the valves 2, 5 to be respectively closed and open during the expiratory period and the former cause the valves 2, 5 to be opened alternately during the inspiratory period to produce the mixture of air and oxygen required to maintain the desired partial pressure, which varies with the altitude of the aircraft to produce correcting signals from the sensor 3. The valves 2, 5 are electromagnetically controlled, Figs. 3 and 4 (not shown) and are opened during the respective marks and spaces of the positive pulse train produced during the inspiratory period, the mark/space ratio being varied by the signal from sensor 3 so that the system is fully automatic up to and including 100% oxygen. An altitude reference sensor 15 provides a bias to increase the amount of oxygen to prevent mask-seal leakage when a particular altitude is reached, the effect being that the transducer 4 then operates about a new datum pressure. The expiration phase is not affected. The electronic control also prevents opening of the valve 5 under "g" loading conditions, and members 4, 15 operate together to maintain the correct mask pressure in the event of cabin decompression. Should the altitude increase above that which can be accommodated by 100% oxygen admission during the inspiratory period, the partial pressure signal from amplifier 16 adjusts a safety pressure bias 19 which acts in conjunction with the transducer 4 to increase the oxygen pressure in the mask by prolonging the opening of the valve 2. Transducer 4 produces a variable capacitance signal, Fig. 2 (not shown).
GB4410065A 1965-10-18 1965-10-18 Improvements in or relating to oxygen regulators Expired GB1104849A (en)

Priority Applications (2)

Application Number Priority Date Filing Date Title
GB4410065A GB1104849A (en) 1965-10-18 1965-10-18 Improvements in or relating to oxygen regulators
DE19661559692 DE1559692B1 (en) 1965-10-18 1966-10-14 Breathing gas supply device for high altitude breathing apparatus

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB4410065A GB1104849A (en) 1965-10-18 1965-10-18 Improvements in or relating to oxygen regulators

Publications (1)

Publication Number Publication Date
GB1104849A true GB1104849A (en) 1968-02-28

Family

ID=10431786

Family Applications (1)

Application Number Title Priority Date Filing Date
GB4410065A Expired GB1104849A (en) 1965-10-18 1965-10-18 Improvements in or relating to oxygen regulators

Country Status (2)

Country Link
DE (1) DE1559692B1 (en)
GB (1) GB1104849A (en)

Cited By (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2235136A (en) * 1989-08-18 1991-02-27 Sabre Safety Ltd Positive pressure breathing apparatus
US9022028B2 (en) 2007-07-04 2015-05-05 B/E Aerospace Systems Gmbh Oxygen supply device
WO2024023420A1 (en) * 2022-07-27 2024-02-01 Safran Aerosystems Respiratory system, in particular for an aircraft, with regulation of the proportion of oxygen
WO2024023421A1 (en) * 2022-07-27 2024-02-01 Safran Aerosystems Respiratory system, in particular for an aircraft

Families Citing this family (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE102006030668B3 (en) * 2006-07-04 2008-01-31 DRäGER AEROSPACE GMBH Cockpit oxygen mask

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
DE690930C (en) * 1934-09-09 1940-05-10 Draegerwerk Heinr U Bernh Drae Marriage breathing apparatus with lung-controlled oxygen supply
DE729638C (en) * 1939-03-23 1942-12-19 Auergesellschaft Ag Lung-controlled oxygen breathing apparatus, especially high altitude breathing apparatus
DE1104828B (en) * 1959-03-02 1961-04-13 Draegerwerk Ag Breathing apparatus with breathing air circulation

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2235136A (en) * 1989-08-18 1991-02-27 Sabre Safety Ltd Positive pressure breathing apparatus
US9022028B2 (en) 2007-07-04 2015-05-05 B/E Aerospace Systems Gmbh Oxygen supply device
WO2024023420A1 (en) * 2022-07-27 2024-02-01 Safran Aerosystems Respiratory system, in particular for an aircraft, with regulation of the proportion of oxygen
WO2024023421A1 (en) * 2022-07-27 2024-02-01 Safran Aerosystems Respiratory system, in particular for an aircraft
FR3138321A1 (en) * 2022-07-27 2024-02-02 Safran Aerosystems Respiratory system, particularly for an aircraft, with regulation of the proportion of oxygen
FR3138322A1 (en) * 2022-07-27 2024-02-02 Safran Aerosystems Respiratory system, particularly for an aircraft

Also Published As

Publication number Publication date
DE1559692B1 (en) 1971-04-22

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