GB1577943A - Creation of Inventions and Patents with Artificial Intelligence

GB1577943A – Gas mixing apparatus
– Google Patents

GB1577943A – Gas mixing apparatus
– Google Patents
Gas mixing apparatus

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Publication number
GB1577943A

GB1577943A
GB2149776A
GB2149776A
GB1577943A
GB 1577943 A
GB1577943 A
GB 1577943A
GB 2149776 A
GB2149776 A
GB 2149776A
GB 2149776 A
GB2149776 A
GB 2149776A
GB 1577943 A
GB1577943 A
GB 1577943A
Authority
GB
United Kingdom
Prior art keywords
pressure
chamber
supply
normal
oxygen
Prior art date
1976-05-24
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
GB2149776A
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.)

UK Secretary of State for Defence

Original Assignee
UK Secretary of State for Defence
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.)
1976-05-24
Filing date
1976-05-24
Publication date
1980-10-29

1976-05-24
Application filed by UK Secretary of State for Defence
filed
Critical
UK Secretary of State for Defence

1976-05-24
Priority to GB2149776A
priority
Critical
patent/GB1577943A/en

1977-05-18
Priority to US05/798,253
priority
patent/US4148311A/en

1977-05-20
Priority to CA278,936A
priority
patent/CA1072415A/en

1977-05-24
Priority to DE19772723471
priority
patent/DE2723471A1/en

1977-05-24
Priority to FR7715846A
priority
patent/FR2353094A1/en

1980-10-29
Publication of GB1577943A
publication
Critical
patent/GB1577943A/en

Status
Expired
legal-status
Critical
Current

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Classifications

G—PHYSICS

G05—CONTROLLING; REGULATING

G05D—SYSTEMS FOR CONTROLLING OR REGULATING NON-ELECTRIC VARIABLES

G05D11/00—Control of flow ratio

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

Description

(54) IMPROVEMENTS IN OR RELATING TO GAS MIXING APPARATUS
(71) 1, SECRETARY OF STATE FOR
DEFENCE, LONDON, do hereby declare the invention, for which I pray that a patent may be granted to me, and the method by which it is to be performed, to be particularly described in and by the following state ment:- The present invention relates to apparatus for supplying a mixture of gases at pressure. It is particularly concerned with respiration systems for supplying oxygen and air to airborne personnel, especially airscrew.
A typical aircraft capable of flying at high altitude, eg over 30,out ft, has respiration apparatus for supplying breathing gas directly to each aircrewman. In the usual system air is drawn from the cabin, which is supplied from the environment. The pressure in the cabin is arranged to decrease with altitude at a rate such that at about 20,000 m real altitude the equivalent cabin altitude is 7,000 m. It is therefore necessary to supplement the air with oxygen to an increasing extent with altitude, because of the variation with altitude of the partial pressures of the constituent gases in air. In most such respiration svstems hitherto, oxygen stored in the aircraft is passed through a venturi, and the air is therebv drawn into the mixture.These systems are incapable of supplying less than a certain proportion of oxygen. which proportion is considerably more than that required at lower altitudes.
As a consequence not only has more oxygen than has actually been required had to be stored. but that kind of quantity has had to be stored in liquid or highlv pressurised state. and the resultant weight penalty has been aggravated by location and/or insulation problems.
The present invention provides a simple apparatus wherein the oxygen partial pressure in the supply mixture can be varied in accordance with altitude.
According to the present invention apparatus for supplying a mixture of two gases at pressure comprises a supply regulator having a first chamber with an inlet and an outlet for the first gas and a second chamber with an inlet and an outlet for the second gas, control means responsive to a higher pressure in the first chamber than in the second to permit the second gas to enter the second chamber, adjustment means sensible to environmental pressure to modify the action of the control means, a first restrictor in the first outlet and the second restrictor in second outlet, the secod restrictor bore being larger than that of the first, a junction between the first and second outlets and a common supply duct down-stream of the restrictors, and a first demand regulator permitting on demand flow of gas in the common supply.
In use of apparatus in accordance with the invention, while there is no demand for gas mixture on the demand regulator this latter prevents the passage therethrough the gases, and the pressure of the gas in the first chamber is equalised with that in the second by virtue of the junction between the two outlets. When there is a demand on the demand regulator this latter permits gas to flow therethrough. Because the difference in the restrictor sizes permits flow more readily from the second chamber than the first, a pressure difference is set up between the two which causes admission of the second gas into the second chamber and thence into the common supply. Insofar as a change is required in the proportion of the first gas in the mixture. the adjustment means can be used to alter the pressure difference between the chambers at which the second gas will be allowed to flow.
The environmental pressure sensing.
whereby the proportion of the first gas in the mixture may be varied in accordance with changes in environmental pressure, may be of water pressure in the case of oxygen/air supply apparatus used in diving equipment, or of air pressure in the case of oxygen/air supply apparatus used by airborne personnel.
According to a preferred feature of the invention the control means responsive to a higher pressure in the first chamber than in the second to permit the second gas to enter the second chamber may comprise a diaphragm separating the first chamber from the second and a valve in the second chamber inlet operable by the diaphragm.
The adjustment means may be arranged to operate on the diaphragm.
The environmental pressure sensing means may comprise an aneroid capsule.
and may be additionally adjustable.
In an important embodiment of the invention the apparatus is part of equipment for supplying respiratory gas to a person, and the first gas supply is oxygen stored at above normal atmospheric pressure and the second gas supply is air at above atmospheric pressure, perhaps supplied from the environment via a pump and a filter. The outlet from the demand regulator is connected directly to a respirator mask. such as an oro-nasal mask. so that the demand regulator is arranged to permit the passage of common supply gas on sensing the reduction of pressure in the common supply downstream thereof brought about by the user commencing inspiration.
In the case of oxygen/air apparatus an aneroid capsule is preferably arranged to increase the proportion of oxygen with altitude.
Oxygen/air apparatus according to the invention and for aircrew also has advantageously the usual emergency facilities including an emergency oxygen supply. preferably connected into the apparatus downstream of the supply regulator, an emergen cv demand regulator by-passing the normal demand regulator. and a pressure breathing facility catering for accidental loss of en vironmental pressure.
The demand regulators. both normal and emergency may be of a construction similar to that of a supply regulator. a first chamber of each being open to environmental pressure whereby a demand will open the second chamber inlet. The demand may be a suction normallv generated by inhalation.
The operation of the demand regulators may be modified bv means. perhaps including at least one aneroid. to supply emergency oxygen at pressure in the event of sudden loss of environmental pressure and to supply the normal gas mixture at a pressure slightlv above that of the environment to cater for leaks at the apparatus/user interfacc.
In the case of an airborne system . while the normal and emergency oxygen may be stored in reservoirs, the air may be derived from the engine compressors. This air supply may also be fed to the first chamber of the normal and emergency demand regulators.
Oxygen/air apparatus in accordance with the invention and for use by aircrew will now be described by way of example with reference to the schematic diagram of the apparatus accompanying the provisional specification.
As shown in the diagram the apparatus includes a supply regulator 10, and normal and emergency demand regulator 11 and 12.
The supply regulator 10 has a first gas chamber 13 with a first gas inlet 14 and a first gas outlet containing a restrictor 15, and a second gas chamber 16 with a second gas inlet 17 and a second gas outlet containing a restrictor 18. The restrictor 18 has a larger bore than the restrictor 15. A diaphragm 19 separates the two chambers and is in operative relationship with a toggle valve 20 controlling the second gas inlet 17.
An aneroid capsule 21 modifies the action of the diaphragm 19 and adjustment means 22 are provided for varying the datum position of the aneroid capsule 21.
Upstream of the first inlet 14 is a reducing valve 23 and a cock 24. and upstream of the second inlet 17 is a reducing valve 25 and a cock 26.
Downstream of the restrictors 15 and 18 the outlets are joined into a common duct 27 which. via a cock 2X, forms the inlet to the normal and emergency demand regulators 11 and 12. The regulators ii and 12 are similar in construction to the supply regulator 10. which is a conventional construction.
but the first chambers 2′) and 30 thereof are open to the cabin pressure. The gas inlets to the regulators II and 12 are controlled by toggle valves 31.32 in operative relationship with diaphragms 33. 34. The action of the diaphragms 33. 34 is modified by safety pressure aneroid capsules. 35. 36 and pressure breathing aneroid capsules 37. 38. The outlets to the regulators II and 12 pass to a mask 39.
Connected into the duct 27 is the emergency oxygen facilitv comprising an emergency reservoir 40. a cock 41. a manual control 42. an ejection trip 43. and a disconnect 44. The demand regulators and the emergency oxygen system are mounted on the aircrewman’s ejector seat. and the supply regulator 1() on the aircraft as close as possible to it to minimise the length of the ducting 27 between the supply regulator 1-0 and the emergency oxygen reservoir 4() on the one hand and the demand regulators II and 12 on the other. Normal and emergency pressure gauges 45 and 46 indicate the pressures in the duct 27 and the reservoir 40 respectively. The emergency oxygen is delivered at a pressure somewhat less than the normal oxygen.
In normal use of the system, the valves 24 and 26 are open, the valve 28 connects the duct 27 with the normal regulator 11, and pressurised oxygen enters the first chamber 13 at inlet 14 via the cock 24 and the valve 23. Pressurised air is supplied to the second inlet 17 via the cock 26 and the valve 25.
While there is no suction on the duct 27 the pressure in the chambers 13 and 16 is equalised by flow back of oxygen through the restrictor 18. The valve 20 thus remains closed and no air is allowed into the second chamber.
When there is a suction in the duct 27, by virtue of the different bores of the restrictors IS and 18 a pressure difference is set up between the chambers 13 and 16, the diaphragm 19 is depressed and the valve 20 opened to allow air through the second chamber to mix with the oxygen in the duct 27.
Suction in the duct 27 is brought about by inhalation by the wearer of the mask 39, which causes deflection of the diaphragm 33 of the normal demand regulator 11, and opening of the valve 31. The normal drop in cabin pressure with increase in aircraft altitude has two main effects. It will expand the aneroid capsule 21 in the supply regulator 10, raise the diaphragm 19 and increase the proportion of oxygen in the mixture. It will also expand the safety pressure aneroid capsules 35 and 36 to ensure that the gas supplied to the mask 39 is at a pressure slightly above cabin pressure so that there is enough leak of gas from the mask rather than into it.
The apparatus caters for various emergencies. In the event of failure or contamination of the bleed air the user may switch to 100″o normal oxygen using the cock 26. If the normal supply as a whole appears to fail the user will normally suspect a failure of the normal demand regulator 11 first, and will switch to the emergency demand regulator 12 using the cock 28. He may, to ensure immediate oxygen supply however operate this using the button 42 which is linked to both the cocks 28 and 41. By virtue of the lower pressure of the emergency oxygen supply this will not be used unless no oxygen is available from the normal supply. The wearer will know that the emergency supply is not being used bv reading the gauge 46.If there is an accidental loss of cabin pressure the demand regulators l l and 12 will switch to a pressure breathing mode by virtue of the operation of the aneroid capsules 37 and 38. In the event of ejection. the passage of the seat operates the trip 43. opening the cock 41 and switching the cock 2X to connect the duct 27 to the emergency demand regulator 12, and disconnects the socket 44 which closes the duct 27 at that point.
Typically the aircraft system has a normal oxygen supply pressure of 40 Ib/sq in and an emergency oxygen supply pressure of 20
Ib/sq in, and the air supply from the engine compressors is at about 50 Ib/sq in. In such a system the restrictors 15 and 18 have bores of 0.0935 in and 0.0960 in respectively.
Cabin pressure drops to about 7,000 m altitude when the aircraft reaches its ceiling which may be about 20,000 m The aneroid capsule 21 permits account to be taken of this in the supply to the user. The aneroid capsules 37 and 38 may be arranged to switch over when the environmental pressure drops below that at 10,000m; WHAT WE CLAIM lS:- 1.Apparatus for supplying a mixture of two gases at pressure and comprising a supply regulator having a first chamber with an inlet and an outlet for the first gas and a second chamber with an inlet and an outlet for the second gas, control means responsive to a higher pressure in the first chamber than in the chamber to permit the second gas to enter the second chamber, adjustment means responsive to environmental pressure to for modify the action of the control means, a first restrictor in the first outlet and a second restrictor in the second outlet, the second restrictor bore being larger than the first restrictor bore, a junction between the first and second outlets and a common supply duct down-stream of the restrictors, and a first demand regulator permitting on demand flow of gas in the common supply.
2. Apparatus as claimed in claim 1 and wherein the adjustment means comprises an aneroid capsule whereby the proportion of the first gas in the mixture may be varied in accordance with changes in environmental pressure.
3. Apparatus as claimed in claim 1 or claim 2 and wherein the means in the supply regulator responsive to a higher pressure in the first chamber than in the second chamber to permit the second gas to enter the second chamber comprises a diaphragm separating the first chamber from the second chamber and a valve in the second chamber inlet operable by the diaphragm.
4. Apparatus as claimed in any one of the claims 1 to 3 and having an emergency demand regulator by-passing the first demand regulator.
5. Apparatus as claimed in any one of the preceding claims and wherein the. either or each demand regulator comprises a first chamber open to environmental pressure, a second chamber having an inlet and an outlet connected in the common supply duct, and control means responsive to a higher pressure in the first chamber than the second chamber to permit gas in the common supply to enter the second chamber.
**WARNING** end of DESC field may overlap start of CLMS **.

Claims (21)

**WARNING** start of CLMS field may overlap end of DESC **.
normal oxygen.
In normal use of the system, the valves 24 and 26 are open, the valve 28 connects the duct 27 with the normal regulator 11, and pressurised oxygen enters the first chamber 13 at inlet 14 via the cock 24 and the valve 23. Pressurised air is supplied to the second inlet 17 via the cock 26 and the valve 25.
While there is no suction on the duct 27 the pressure in the chambers 13 and 16 is equalised by flow back of oxygen through the restrictor 18. The valve 20 thus remains closed and no air is allowed into the second chamber.
When there is a suction in the duct 27, by virtue of the different bores of the restrictors IS and 18 a pressure difference is set up between the chambers 13 and 16, the diaphragm 19 is depressed and the valve 20 opened to allow air through the second chamber to mix with the oxygen in the duct 27.
Suction in the duct 27 is brought about by inhalation by the wearer of the mask 39, which causes deflection of the diaphragm 33 of the normal demand regulator 11, and opening of the valve 31. The normal drop in cabin pressure with increase in aircraft altitude has two main effects. It will expand the aneroid capsule 21 in the supply regulator 10, raise the diaphragm 19 and increase the proportion of oxygen in the mixture. It will also expand the safety pressure aneroid capsules 35 and 36 to ensure that the gas supplied to the mask 39 is at a pressure slightly above cabin pressure so that there is enough leak of gas from the mask rather than into it.
The apparatus caters for various emergencies. In the event of failure or contamination of the bleed air the user may switch to 100″o normal oxygen using the cock 26. If the normal supply as a whole appears to fail the user will normally suspect a failure of the normal demand regulator 11 first, and will switch to the emergency demand regulator 12 using the cock 28. He may, to ensure immediate oxygen supply however operate this using the button 42 which is linked to both the cocks 28 and 41. By virtue of the lower pressure of the emergency oxygen supply this will not be used unless no oxygen is available from the normal supply. The wearer will know that the emergency supply is not being used bv reading the gauge 46.If there is an accidental loss of cabin pressure the demand regulators l l and 12 will switch to a pressure breathing mode by virtue of the operation of the aneroid capsules 37 and 38. In the event of ejection. the passage of the seat operates the trip 43. opening the cock 41 and switching the cock 2X to connect the duct 27 to the emergency demand regulator 12, and disconnects the socket 44 which closes the duct 27 at that point.
Typically the aircraft system has a normal oxygen supply pressure of 40 Ib/sq in and an emergency oxygen supply pressure of 20
Ib/sq in, and the air supply from the engine compressors is at about 50 Ib/sq in. In such a system the restrictors 15 and 18 have bores of 0.0935 in and 0.0960 in respectively.
Cabin pressure drops to about 7,000 m altitude when the aircraft reaches its ceiling which may be about 20,000 m The aneroid capsule 21 permits account to be taken of this in the supply to the user. The aneroid capsules 37 and 38 may be arranged to switch over when the environmental pressure drops below that at 10,000m; WHAT WE CLAIM lS:- 1.Apparatus for supplying a mixture of two gases at pressure and comprising a supply regulator having a first chamber with an inlet and an outlet for the first gas and a second chamber with an inlet and an outlet for the second gas, control means responsive to a higher pressure in the first chamber than in the chamber to permit the second gas to enter the second chamber, adjustment means responsive to environmental pressure to for modify the action of the control means, a first restrictor in the first outlet and a second restrictor in the second outlet, the second restrictor bore being larger than the first restrictor bore, a junction between the first and second outlets and a common supply duct down-stream of the restrictors, and a first demand regulator permitting on demand flow of gas in the common supply.

2. Apparatus as claimed in claim 1 and wherein the adjustment means comprises an aneroid capsule whereby the proportion of the first gas in the mixture may be varied in accordance with changes in environmental pressure.

3. Apparatus as claimed in claim 1 or claim 2 and wherein the means in the supply regulator responsive to a higher pressure in the first chamber than in the second chamber to permit the second gas to enter the second chamber comprises a diaphragm separating the first chamber from the second chamber and a valve in the second chamber inlet operable by the diaphragm.

4. Apparatus as claimed in any one of the claims 1 to 3 and having an emergency demand regulator by-passing the first demand regulator.

5. Apparatus as claimed in any one of the preceding claims and wherein the. either or each demand regulator comprises a first chamber open to environmental pressure, a second chamber having an inlet and an outlet connected in the common supply duct, and control means responsive to a higher pressure in the first chamber than the second chamber to permit gas in the common supply to enter the second chamber.

6. Apparatus as claimed in claim 5 and
wherein the, either or each demand regulator control means includes a diaphragm dividing the first chamber from the second and a valve operated thereby and operable on the second chamber inlet.

7. Apparatus as claimed in claim 6 and wherein the valve is a toggle valve.

8. Apparatus as claimed in any one of the preceding claims and having a normal environmental pressure adjuster operable to modify the operation of the or each demand regulator in accordance with normal variation of environmental pressure.

9. Apparatus as claimed in any one of claims 5 to 7 and having a normal environmental pressure adjuster operable upon the demand regulator control means in accordance with normal variation of environmental pressure.

10. Apparatus as claimed in claim 8 or claim 9 and wherein the normal environmental pressure adjuster comprises an aneroid capsule.

11. Apparatus as claimed in claim 4 and having a demand regulator by-pass cock operable to divert the common supply to the emergency demand regulator.

12. Apparatus as claimed in any one of the preceding claims and adapted to form part of equipment for supplying respiratory gas to a person. the first chamber inlet being adapted for connection to a supply of oxygen at a pressure above normal atmospheric pressure, the second chamber inlet being adapted for connection to a supply of air at a pressure above normal atmospheric pressure, the common supply downstream of the or each demand regulator being adapted for connection to a respirator. and the or each demand regulator being arranged to permit the passage of gas in the common supply duct on sensing a reduction in pressure downstream thereof brought about by a user commencing inhalation.

13. Apparatus as claimed in claim 12 and forming part of aircrew breathing equipment and wherein the second chamber inlet is adapted for connection to filtered air supplied from an aircraft engine compressor.

14. Apparatus as claimed in claim 12 or claim 13 and having a pressure breathing facility operable to sense an emergency change of environmental pressure and accordingly to ass respiratory gas to a user.

15. Apparatus as claimed in claim 14.
and wherein the pressure breathing facility is operable to override the or each demand regulator.

16. Apparatus as claimed in claim 15.
and wherein the pressure breathing facility includes an aneroid capsule.

17. Apparatus as claimed in any one of claims 12 to 16 and having an emergency oxygen supply connected thereinto downstream of the supply regulator.

18. Apparatus as claimed in claim 7 and having an emergency oxygen supply connected thereinto downstream of the supply regulator and upstream of the demand regulator by-pass cock.

19. Apparatus as claimed in claim 17-or claim 18 and wherein the emergency oxygen is arranged to be supplied at a lower pressure than the normal oxygen supply,

20. Apparatus as claimed in any one of claims 17 to 19 and having an emergency oxygen supply cock adapted for operation by an ejector seat mechanism.

21. Apparatus substantially as hereinbefore described with reference to the drawing accompanying the provisional specification.

GB2149776A
1975-05-06
1976-05-24
Gas mixing apparatus

Expired

GB1577943A
(en)

Priority Applications (5)

Application Number
Priority Date
Filing Date
Title

GB2149776A

GB1577943A
(en)

1976-05-24
1976-05-24
Gas mixing apparatus

US05/798,253

US4148311A
(en)

1975-05-06
1977-05-18
Gas mixing apparatus

CA278,936A

CA1072415A
(en)

1976-05-24
1977-05-20
Gas mixing apparatus

DE19772723471

DE2723471A1
(en)

1976-05-24
1977-05-24

GAS MIXING DEVICE

FR7715846A

FR2353094A1
(en)

1976-05-24
1977-05-24

PERFECTED RESPIRATORY SYSTEM

Applications Claiming Priority (1)

Application Number
Priority Date
Filing Date
Title

GB2149776A

GB1577943A
(en)

1976-05-24
1976-05-24
Gas mixing apparatus

Publications (1)

Publication Number
Publication Date

GB1577943A
true

GB1577943A
(en)

1980-10-29

Family
ID=10163943
Family Applications (1)

Application Number
Title
Priority Date
Filing Date

GB2149776A
Expired

GB1577943A
(en)

1975-05-06
1976-05-24
Gas mixing apparatus

Country Status (4)

Country
Link

CA
(1)

CA1072415A
(en)

DE
(1)

DE2723471A1
(en)

FR
(1)

FR2353094A1
(en)

GB
(1)

GB1577943A
(en)

Cited By (2)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP1275416A1
(en)

2001-07-10
2003-01-15
Intertechnique
Respiratory apparatus with flow limiter

DE10217500A1
(en)

2002-04-19
2003-11-13
Draeger Aerospace Gmbh

Gas distribution system in an airplane

Families Citing this family (2)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

FR2469183A1
(en)

1979-11-15
1981-05-22
Intertechnique Sa
Regulator for breathing apparatus – has demand valve for oxygen supply with forced action valve to control inhalation and exhalation

FR3073057B1
(en)

2017-10-30
2021-10-08
Air Liquide

REGULATORY DEVICE, APPARATUS AND METHOD FOR GENERATING BREATHABLE GAS

Family Cites Families (3)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

FR861349A
(en)

1939-01-17
1941-02-06

Multiple inhaler for high altitude flight

GB907390A
(en)

1960-03-15
1962-10-03
Firewel Company Inc
Differential gas supplying apparatus

GB944931A
(en)

1960-06-11
1963-12-18
Normalair Ltd
Improvements in or relating to breathing apparatus

1976

1976-05-24
GB
GB2149776A
patent/GB1577943A/en
not_active
Expired

1977

1977-05-20
CA
CA278,936A
patent/CA1072415A/en
not_active
Expired

1977-05-24
FR
FR7715846A
patent/FR2353094A1/en
not_active
Withdrawn

1977-05-24
DE
DE19772723471
patent/DE2723471A1/en
not_active
Withdrawn

Cited By (6)

* Cited by examiner, † Cited by third party

Publication number
Priority date
Publication date
Assignee
Title

EP1275416A1
(en)

2001-07-10
2003-01-15
Intertechnique
Respiratory apparatus with flow limiter

FR2827179A1
(en)

2001-07-10
2003-01-17
Intertechnique Sa

BREATHING APPARATUS WITH FLOW LIMITER

US6796306B2
(en)

2001-07-10
2004-09-28
Intertechnique
Respiratory apparatus with flow limiter

DE10217500A1
(en)

2002-04-19
2003-11-13
Draeger Aerospace Gmbh

Gas distribution system in an airplane

US6935593B2
(en)

2002-04-19
2005-08-30
DRäGER AEROSPACE GMBH
Gas distribution system in an airplane

DE10217500B4
(en)

2002-04-19
2007-05-31
DRäGER AEROSPACE GMBH

Gas distribution system in an airplane

Also Published As

Publication number
Publication date

CA1072415A
(en)

1980-02-26

DE2723471A1
(en)

1977-12-15

FR2353094A1
(en)

1977-12-23

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