GB1104849A - Improvements in or relating to oxygen regulators - Google Patents
Improvements in or relating to oxygen regulatorsInfo
- 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
Links
- QVGXLLKOCUKJST-UHFFFAOYSA-N atomic oxygen Chemical compound [O] QVGXLLKOCUKJST-UHFFFAOYSA-N 0.000 title abstract 10
- 229910052760 oxygen Inorganic materials 0.000 title abstract 10
- 239000001301 oxygen Substances 0.000 title abstract 10
- 230000003434 inspiratory effect Effects 0.000 abstract 3
- 230000001105 regulatory effect Effects 0.000 abstract 2
- 101100269850 Caenorhabditis elegans mask-1 gene Proteins 0.000 abstract 1
- 230000006837 decompression Effects 0.000 abstract 1
- IWEDIXLBFLAXBO-UHFFFAOYSA-N dicamba Chemical compound COC1=C(Cl)C=CC(Cl)=C1C(O)=O IWEDIXLBFLAXBO-UHFFFAOYSA-N 0.000 abstract 1
- 230000000694 effects Effects 0.000 abstract 1
- 239000000203 mixture Substances 0.000 abstract 1
- 230000029058 respiratory gaseous exchange Effects 0.000 abstract 1
Classifications
-
- G—PHYSICS
- G05—CONTROLLING; REGULATING
- G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES
- G05D16/00—Control of fluid pressure
- G05D16/20—Control of fluid pressure characterised by the use of electric means
- G05D16/2006—Control of fluid pressure characterised by the use of electric means with direct action of electric energy on controlling means
- G05D16/2013—Control 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
- G05D16/2026—Control 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
- G05D16/2046—Control 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
-
- A—HUMAN NECESSITIES
- A62—LIFE-SAVING; FIRE-FIGHTING
- A62B—DEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
- A62B7/00—Respiratory apparatus
- A62B7/14—Respiratory 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).
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)
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)
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)
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 |
-
1965
- 1965-10-18 GB GB4410065A patent/GB1104849A/en not_active Expired
-
1966
- 1966-10-14 DE DE19661559692 patent/DE1559692B1/en active Pending
Cited By (6)
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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