CA1217990A - Combined pressure compensating exhalation and anti- suffocation valve - Google Patents

Combined pressure compensating exhalation and anti- suffocation valve

Info

Publication number
CA1217990A
CA1217990A CA000456072A CA456072A CA1217990A CA 1217990 A CA1217990 A CA 1217990A CA 000456072 A CA000456072 A CA 000456072A CA 456072 A CA456072 A CA 456072A CA 1217990 A CA1217990 A CA 1217990A
Authority
CA
Canada
Prior art keywords
exhaust port
diaphragm assembly
valve
port plate
exhalation
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
CA000456072A
Other languages
French (fr)
Inventor
William K. Ansite
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.)
Scott Technologies Inc
Original Assignee
Figgie International Inc
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 Figgie International Inc filed Critical Figgie International Inc
Application granted granted Critical
Publication of CA1217990A publication Critical patent/CA1217990A/en
Expired legal-status Critical Current

Links

Classifications

    • AHUMAN NECESSITIES
    • A62LIFE-SAVING; FIRE-FIGHTING
    • A62BDEVICES, APPARATUS OR METHODS FOR LIFE-SAVING
    • A62B18/00Breathing masks or helmets, e.g. affording protection against chemical agents or for use at high altitudes or incorporating a pump or compressor for reducing the inhalation effort
    • A62B18/08Component parts for gas-masks or gas-helmets, e.g. windows, straps, speech transmitters, signal-devices
    • A62B18/10Valves
    • YGENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10TTECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T137/00Fluid handling
    • Y10T137/7722Line condition change responsive valves
    • Y10T137/7837Direct response valves [i.e., check valve type]
    • Y10T137/7876With external means for opposing bias

Abstract

ABSTRACT

A combined pressure compensated exhalation and anti-suffocation valve assembly of the type which may find utility in an aviator's breathing mask. The valve assembly (14) includes a valve body (20) provided with an exhaust port (44) and a compensated pressure chamber (62) in communication with the mask cavity through an orifice tube (72). Disposed within the valve body (14) are a movable diaphragm assembly (22) and an exhaust port plate (24) supported by and movable toward and away from the diaphragm assembly. There is a lost motion connection (106, 108 or 138, 140) extending between the diaphragm assembly and the exhaust port plate, the connection being capable of permitting the exhaust port plate to move relative to the diaphragm assembly within a predetermined range of movements, the parts being so arranged and constructed that if during an inspiratory effort the diaphragm assembly attempts to move away from the exhaust port plate a distance greater then that permitted by the lost motion connection means, as would be the case if the breathing gas supply fails to deliver an adequate supply of gas to the mask cavity, the diaphragm assembly acting through the lost motion connection means will cause corresponding movement of the exhaust port plate thereby opening the mask cavity to ambient.

Description

I
The present invention relates generally to breathing apparatus of the type which may be worn by an aviator, and more particularly to a valve which may be utlllæed with a breathing mask or helmet both as an exhalation valve and an anti-suEfocation valve, which valve is pressure compensated.
Exhalation valves are well known in the prior art. One such valve is shown in US. 3,459,216. This form of valve, slightly modified, is in commercial use today. It performs very satisfactorily as an exhalation valve. However, when utilized with a breathing mask it is also necessary to provide an anti-suffocation valve in the case that the supply of breathing gas (customarily oxygen) should fail. Various types of anti-suffocation valves are well known in the art and they generally function on the same principles.
Thus, when an aviator should inhale and create a vacuum within the mask cavity, at least equal to a predetermined pressure differential, for example, approxi-mutely 6 inches of water, the valve will open and permit the aviator to breathe ambient air. The designs vary and once open the valve may stay open or it may close after the pressure differential drops below the predator-mined amount. These designs perform quite satisfactorily in normal conditions. Ilowever~ if a person wearing such a mask should enter water to a level below 6 inches, the water pressure will cause Tao valve to open (as there is now more than 6 inches of water pressure differential between the mask cavity and ambient), causing the mask cavity to flood with water. This obviously can create I severe problems, particularly lo the person entering the ¦ water is unconscious, as may be the case when a pilot has ejected from an aircraft over water. It should be ¦ observed that in most situations where an aviator enters ¦ the water the normal breathing supply is in operation and it is not necessary for the aviator to cause the anti-suffocation valve to open. However, the mere pressure of the water on the valve will cause it to open which, in I some situations could lead to drowning.
¦ The prior art has recognized the problem of convent l tonal anti-suffocation valves. Thus D U. S . 3,362,420 ¦ discloses an anti-suffocation valve which, due to a solenoid operated circuit will not open when a sensor is in salt water. While this patent presumably operates in a satisfactory manner, it should be obvious that it is a relatively expensive design and -requires a power supply for its proper operation.

Objects and Summary of the Invention if It is therefore an object of the present invention l! to provide an improved anti-suffocation valve which is relatively simple, inexpensive and reliable in operation.

More specifically. it is an obiec~ of the present invention to provide an anti-suffocatlon valve which is designed in such manner t ha it will not open when ambient exceeds internal pressure except when caused to open by the wearer of the breathing apparatus through the initiation of an inspiratory effort. More specifically, it is an object of the present invention to combine an anti-suffocation valve with a pressure compensated exhalation valve.
In accordance with the objects of this invention the invention is accomplished by incorporating into the known pressure compensated exhalation valve of the type shown in U. S. 3,459,216 additional structure which will cause the exhaust port valve to open when an inspiratory effort exceeds a predetermined pressure differential. I
The foregoing, as well as other objects and advantage of this invention, will be more fully understood from the consideration of the following detailed description taken in conjunction with the accompanying drawings in which preferred forms of this invention are illustrated.

Brief Description of the Drawings Fig. 1 is a cross-sectional view of one form of a combined pressure compensated exhalation and anti-suffocation valve.
Fig. 2 is a sectional view taken generally along the line 2-2 in Fig. 1.
Fig, 3 is a cross section of a modified form of a combined pressure compensated exhalation and anti-suffocation valve.

1~1'795~0 Fig. 4 is an enlarged detail of a portion of the valve shown in Fig. 3.
Fig. 5 is a scl)em.l~ie i.llustrat;oll of a breathing Newsweek which may illcorporclte Lowe valve of this invention.

Detailed Description ....
Referring first to Fix. 5 a mast is indicated generally at 10 and is provided with an inlet tube 12 connected to a supply of breathing gay which is typically oxygen. Mounted adjacent the supply tube 12 is an exhalation valve indicated generally at 14, the exhalation valve being in communication with the mask cavity through an orifice tube 16 which may be connected with the breathing supply tube 12. Jo the orifice tube may be connected with the breathing tube 12 it should be noted that the pressure within the breathing tube 12 will be essentially the same as that within the mask cavity.
One form of thy valve 14 is more fully illustrated in Fig. 1 to which reference Jill now be made. The combined pressure compensated exhalation and anti suffoca-lion valve includes a valve body indicated generally at 20, a movable diaphragm assembly indicated generally at l 22, an exhaust port plate 24, lost motion ¦ connection means, one form of which is indicated generally at 26 in Fig. 1 and, similarly, resilient means, one form of which is indicated generally at 28 in Fig. 1.
As is conventional in the prior art, the valve body is formed of two sections, one section 30 of the valve lZ~7990 V

body being adapted to be connected to the mask in an airtigtlt relationship, end another section 32 being secured to the first section 30. To this end, an annular member 34 it prevailed, the member ill haven fluorite positioning posts cxtend$ng towards the first section 30 away from one side 38 of the annular member, an there being second ¦ positioning post 40 extending away from the other side 42 of the annular member, the posts 36 and 40 being adapted to be received within suitable apertures in the first and second sections 30, 32 and being secured thereto by staking or the live. the section 30 of the valve body is cast otherwise secured about an exhaust port 44 which is provided with a hardened knife edge 46, The exhaust port 44 is in communication with a passageway which onus part of the mask cavity, The other section 32 of the valve body has a generally cup-shaped configuration, the rim So having a radially outer peripheral surface 52 which is adapted Jo contact the other wide 42 of the annular member 34.
Spiced radially inwardly from thy Ursa it an annular recess 54 which 18 adapted to Rockwell a bead edge 56 of an el~stomeric member 58 which form a portion of thy diaphragm assembly 22. By can be seen from Fig. 1 the bead edge 56 is securely trapped within the annular recess 54 between the member 34 and the rip So. A dosed cylindrical portion 60 is disposed radially inwardly of the rim 50 and forms a c~mpen~iating pressure chamber 62.
Supported by the end wall 64 of the closed cylindrical portion 60 are a plurality of sprint supports 66 which are guy spaced equal radial di~t.lnces from the center of the end wall 64. Each of the sprint supports 66 its provide with a shouldered portion 67 which receives one end of a valve ¦ spring 68. The cylindrical wall of the closed cylindrical ¦ S portion 60 is provided with an aperture 70 which receives one end of an orifice tube or pressure compensating tube 16, the other end of which is interconnected with the mask cavity, either directly or through a breathing supply tube.
The movable diaphragm assembly 22 includes, in addition to the elastomeric member 58, an exhaust port plate support member 74 and a protective plate 76, an ¦ annular portion of the clas~omeric member 58 being sandwiched between the protective plate 76 and a portion 15 of the exhaust port plate support member 74. One end of the spring 68 bears against toe protective plate 76 as I¦ can be seen from Fig. 1. The exhaust port plate support member has a first cylindrical sleeve portion 78 which extends towards the exhaust port 44, and second cylindrical portion 80 which extends towards the end wall 1 64, the second cylindrical portion being closed by an ¦ end wall I provided with a central aperture 84. The I cylindrical portion 80 includes a safety relief indicated ¦ generally at 86, which relief means will be described in greater detail below, The exhaust port plate I is a disk-lLke member having a surface 88 which is adapted to be contacted by the knife edge 46 ox the valve seat 44 when the valve 24 is closing the exhaust port. The exhaust port valve is I

. -6-lZ17990 also provided with a cylindrical sleeve portion 90 which is telescopically received within the cylindrical sleeve portion 78, the cooperating sleeves 78 and 90 permitting telescoping movement of they'll exhaust port plate 24 relative to the diaphragm assembly 22. spring 92 extends between the exhaust port plate 24 and the exhaust port plate support member 74 and normally biases the exhaust port plate away from the diaphragm assembly.
The safety relief means 86 includes a poppet valve 94 having one end of which normally closes the orifice 84 in the end wall 82. The poppet 94 is provided with a stem portion 96 which passes through a suitable aperture 98 in an aperture and threaded member 100. spring 102 extends between the threaded member 100 and an enlarged portion 104 of the poppet Al The structure so far described is to a large extent disclosed in U. S. 3,459,21~ and will operate in the same manner as the pressure compensated exhalation valve having, ¦
a relief port in the compensating pressure chamber as described in said patent. In normal operation the pressure within the pressure compensating chamber 62 is equal to or, during an exhalation effort of the wearer of the mask, less than the pressure within the mask. Thus, except when the wearer of the mask exhales, the valve I 25 plate 24 will be in contact with the knife edge 46.
However, when the wearer of the mask exhales the valve plate 24 will move away from the knife edge 46 causing the I spring 92 and, to some degree, the spring 6B to be come pressed, the exhaled gas passing between the knife edge 1;Z179~0 46 and the surface 88. The safety relief 86 it provided for overpricer condition. Should such a condition exist within eke mask cavity, the poppet I will move against spring pressure 10~ rutting thy overpricer S condition, which would also exist in the compensating pressure chamber 62, to discharge to ambient. When this happen, the play 24 and ~ial~hragm assembly 22 will then move towards the ells wall 64 thereby quickly dumping the overpricer within the mask cavity between knife edge 46 anal s-lrEacc 88. For more complete detail ox the operation of the foregoing structure reference should be made to U. S. 3!459,216.
In accordance with the principles of this invention lost motion connection jeans 26 extend ~etwecn exhaust port plate 24 and the movable diaphragm assembly at 22.
In this connection in the embodiment illustrated In Fig. 1, the lost motion connection means includes elongated slots 106 in the cylindrical Levi proton 90 an pins 108 which past through sulcable apertures 110 on the cylinder-eel sleeve portion 78. In order to facilitate assembly ¦ the pins 108 are part of a C-sll~ped resilient element 112, the end of which are normally biased toward etch other.
It should be obvious that the diaphrllgm assembly 22 has a first range of movement with respect to the exhaust port 44 which will no cause corresponding movement of the exhaust port plate 24. However, of thy diaphragm assembly 22 should move away from the exhaust port plate 24 a sufficient amount the pins 108 will enact the ends lZ~7990 of the slots 106 and cause subsequent movement of the exhaust port plate. This can occur when the supply of I breathing gas to the mask cavity fails. In this situation, if the wearer of the mask should inhale, he will cause the pressure within the compensating chamber 62 to fall below ambient (as the sensing tube permits the flow of gas from within the chamber 62 to the mask cavity.) this will in turn cause the diaphragm assembly to move away from the valve seat. If there is sufficient movement of the diaphragm assembly, caused by a sufficient inspiratory effort, the pins 108 will engage the ends of the slots 106 and cause subsequent movement of the exhaust port plate 24 thereby moving the surface 88 away from the edge 46 permitting ambient gas to flow past the knife edge I into the passageway 48 through port 44. To control the force required to initiate such operation, resilient means 28 are provided. In the embodiment illustrated in Fig. 1 the resilient means includes a spring 114 which extends between the inner surface of the end wall 64 and an annular spring retainer 116 provided with upstanding portions 118, the upper surface of which engages the protective plate 76. There are spaces between the portions 118 which receive dowels 120 which limit the upward movement of the spring retainer 11~. Because of this construction the diaphragm assembly 22 can move away from the spring retainer 116, 118 during normal operation, but will engage the spring retainer during an inspiratory effort great enough to provide the necessary pressure differential in the chamber 62 to overcome spring 114.

1~17990 In the structure illustrated in Figs. 1 and 2 a pin and slot are utilized for forming the lost motion connection means, and a coil or helical spring is utilized for forming the resilient moans. Ivory, other forms of construction could be utilized and Figs. 3 and 4 illustrate such alternate forms. A the parts are essentially the same in these two figures, only the portions which differ materially will be described.
Referring now in detail to Fig. 3, it can be seen lo that the two portions 30 and 32 of the valve body 20 are held relative to each other by a screw fastener 130 and spacers 132. Mooted within the compensating pressure chamber 62 is an annular elas~omeric foam member 134 having a contoured surface 135 which is adapted to be engaged by the diaphragm assembly to give a tailored spring rate. In addition, the cylindrical sleeve portions 78 and 90 are provided with overhanging lips 138 and 140 to provide the suitable lost motion connection.
It should be obvious that while the structure just described differs in details it will perform functionally in an equivalent manner to that described above in connection with Fig. 1.
While various embodiments of this invention have been described above in conjunction with the varying figures, it should be obvious to those having ordinary skill on the art that other modifications can be made. Therefore, it is to be understood that this invention is not limited to the particular details shown and described above, but that, in fact, widely differing means may be employed in the practice of the broacher aspects of this invention.

Claims (10)

THE EMBODIMENTS OF THE INVENTION IN WHICH AN EXCLUSIVE PROPERTY OR
PRIVILEGE IS CLAIMED ARE DEFINED AS FOLLOWS:
1. A combined pressure compensating exhalation and anti-suffocation valve for a breathing mask for the type having a mask cavity adjacent the wearers nose and/or mouth, said mask cavity normally being supplied with breathing gas from a pressurized supply; said valve including a valve body provided with an exhaust port and a compensating pressure chamber having an orifice in one wall thereof, said orifice being connected to the mask cavity;
a movable diaphragm assembly, the inner surface of which forms one wall of said pressure chamber, and the outer surface of the diaphragm assembly being exposed to ambient pressures, said diaphragm assembly normally being biased outwardly from said pressure chamber toward said exhaust port;
and an exhaust port plate supported by and movable toward and away from said diaphragm assembly, said exhaust port plate normally being resiliently biased away from said diaphragm assembly toward said exhaust port to cover said exhaust port during inhalation, and said exhaust port plate normally moving away from exhaust port toward said diaphragm assembly during exhalation to uncover said exhaust port;
said combined pressure compensated exhalation and anti-suffo-cation valve further being characterized by the provision of;
lost motion connection means extending between the diaphragm assembly and the exhaust port plate and capable of permitting the exhaust port plate to move relative to the diaphragm assembly within a predetermined range of movements, the parts being so arranged and constructed that if during an inspiratory effort the diaphragm assembly attempts to move away from the exhaust port plate a distance greater than that permitted by the lost motion connection means, as would be the case if the breathing gas supply fails to deliver an adequate supply of gas to the mask cavity, the diaphragm assembly acting through the lost motion connection means will cause corresponding move-ment of the exhaust port plate thereby opening the mask cavity to ambient.
2. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 1 further characterized by the provision of resilient means mounted within said compensated pressure chamber and engage-able by the inner surface of said movable diaphragm assembly just prior to the exhaust port plate uncovering the exhaust port during an inhalation effort.
3. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 2 wherein said resilient means includes a coil spring.
4. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 3 wherein said resilient means further includes an annular member, said coil spring bearing against a first surface of said annular member and biasing it towards said diaphragm assembly, and further characterized by the provision of dowels carried by said valve body in which engage a second surface of the annular member, said dowels limiting the movement of the annular member towards said exhaust port so that during normal operation the diaphragm assembly does not contact the annular member.
5. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 2 wherein said resilient means includes an elastomeric foam member.
6. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 5 wherein said resilient foam member is contoured to provide a tailored spring rate.
7. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 1 further characterized by the provision of safety relief means for exhausting fluid through said exhaust port without regard to fluctuations in the ambient pressure, said safety relief means being openable by fluid pressure when said breathing fluid supply system becomes overpricer compensated.
8. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 1 wherein said movable diaphragm assembly includes a cylindrical sleeve supported by the outer surface of said diaphragm assembly and extending away towards said exhaust port, and said exhaust port plate includes a cylindrical sleeve concentric with the cylindrical sleeve on the diaphragm assembly and extending towards said diaphragm assembly, the parts being sized with respect to each other so that they guide one another, and said lost motion connection means includes overhanging lips on said cylindrical sleeves whereby when the diaphragm assembly moves away from the exhaust port a sufficient amount the overhanging lip on the sleeve supported by said diaphragm assembly engages the overhanging lip on the sleeve supported by the exhaust port plate to cause corresponding movement of said exhaust port plate.
9. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 1 wherein said movable diaphragm assembly includes a cylindrical sleeve supported by the outer surface of said diaphragm assembly and extending away towards said exhaust port, and said exhaust port plate includes a cylindrical sleeve concentric with the cylindrical sleeve on the diaphragm assembly and extending towards said diaphragm, the parts being sized with respect to each other so that they guide one another, said lost motion connection means including elongated slots in one of said cylindrical sleeves, and pins mounted on the other of said cylindrical sleeves and projecting into said slots whereby, when the diaphragm moves away from the exhaust port a sufficient amount the pins on the other cylindrical sleeve engages the end of the slot on the one cylindrical sleeve to cause corresponding movement of said exhaust port plate.
10. The combined pressure compensated exhalation and anti-suffocation valve as set forth in claim 9 wherein said pins are interconnected to each other by a C-shaped spring-like element, said C-shaped spring-like element normally biasing the pins towards each other.
CA000456072A 1983-07-14 1984-06-07 Combined pressure compensating exhalation and anti- suffocation valve Expired CA1217990A (en)

Applications Claiming Priority (2)

Application Number Priority Date Filing Date Title
US513,699 1983-07-14
US06/513,699 US4606340A (en) 1983-07-14 1983-07-14 Combined pressure compensating exhalation and anti-suffocation valve

Publications (1)

Publication Number Publication Date
CA1217990A true CA1217990A (en) 1987-02-17

Family

ID=24044331

Family Applications (1)

Application Number Title Priority Date Filing Date
CA000456072A Expired CA1217990A (en) 1983-07-14 1984-06-07 Combined pressure compensating exhalation and anti- suffocation valve

Country Status (7)

Country Link
US (1) US4606340A (en)
JP (1) JPS6036067A (en)
CA (1) CA1217990A (en)
DE (1) DE3424822A1 (en)
FR (1) FR2548911A1 (en)
GB (1) GB2143137B (en)
SE (1) SE8403712L (en)

Families Citing this family (47)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH0310627Y2 (en) * 1985-10-03 1991-03-15
US4850346A (en) * 1986-10-20 1989-07-25 Wgm Safety Corp. Respirator
US4774942A (en) * 1987-08-28 1988-10-04 Litton Systems, Inc. Balanced exhalation valve for use in a closed loop breathing system
US4944293A (en) * 1989-06-23 1990-07-31 The United States Of America As Represented By The Secretary Of The Navy Timed oxygen breathing apparatus trainer
GB9007020D0 (en) * 1990-03-29 1990-05-30 Fxk Patents Ltd Emergency breathing equipment
US5280784A (en) * 1990-09-19 1994-01-25 Paul Ritzau Pari-Werk Gmbh Device in particular and inhalating device for treating the lung and the respiratory tracts
US5159924A (en) * 1990-10-03 1992-11-03 Cegielski Michael J Method and apparatus for selectively mixing gases
US5014694A (en) * 1990-10-15 1991-05-14 Bird Products Corporation Ambient pressure air/oxygen blender
SE469604B (en) * 1992-06-16 1993-08-02 Atlas Copco Tools Ab SPEED CONTROL FOR A PNEUMATIC POWER TOOL
WO1994006514A1 (en) * 1992-09-11 1994-03-31 Life Support Products, Inc. Demand valve with reduced manual flow control
US5477850A (en) * 1992-10-06 1995-12-26 Rockwell International Corp. Integrated buoyancy suit crew protection system with +/-GZ protection
JPH07553A (en) * 1993-06-01 1995-01-06 Litton Syst Inc Regulator for built-in type breathing device
US5487273A (en) * 1993-09-13 1996-01-30 Alliedsignal Inc. Turbocharger having pneumatic actuator with pilot valve
US5467766A (en) * 1993-10-13 1995-11-21 Gentex Corporation Valve for a pressure breathing system which accomplishes the Valsalva maneuver
GB9419144D0 (en) * 1994-09-22 1994-11-09 Sabre Safety Ltd Breathing apparatus
ATE235280T1 (en) * 1994-10-14 2003-04-15 Bird Products Corp PORTABLE, MECHANICAL AND DRIVEN COMPRESSOR VENTILATOR
US5651436A (en) * 1995-04-20 1997-07-29 Midwest Brake Bond Company Brake and clutch control system
US5845637A (en) * 1997-01-09 1998-12-08 Tech-One, Inc. Surface breathing device
AUPP855099A0 (en) * 1999-02-09 1999-03-04 Resmed Limited Gas delivery connection assembly
US6796308B2 (en) * 1998-12-09 2004-09-28 Resmed Limited Mask cushion and frame assembly
US6155258A (en) * 1999-02-25 2000-12-05 Voege; John S. Oxygen delivery system
US6135967A (en) 1999-04-26 2000-10-24 Fiorenza; Anthony Joseph Respiratory ventilator with automatic flow calibration
US6240919B1 (en) 1999-06-07 2001-06-05 Macdonald John J. Method for providing respiratory airway support pressure
FR2805751B1 (en) * 2000-03-02 2002-05-24 Ulmer Aeronautique SAFETY SYSTEM FOR A SEALED BREATHING DEVICE AND A BREATHING DEVICE COMPRISING SUCH A SYSTEM
DE20017940U1 (en) 2000-10-19 2000-12-28 Map Gmbh Breathing mask for supplying a breathing gas to a mask user and a derivation device for deriving breathing gas
DE60225895T2 (en) 2001-09-07 2009-04-09 ResMed Ltd., Bella Vista mask assembly
DE10201682A1 (en) 2002-01-17 2003-07-31 Map Medizin Technologie Gmbh The breathing mask arrangement
ATE473774T1 (en) 2001-10-22 2010-07-15 Map Medizin Technologie Gmbh MEDICAL MASK
DE10151984C5 (en) 2001-10-22 2008-07-17 Map Medizin-Technologie Gmbh Application device for a breathing mask arrangement
EP1545673B1 (en) 2002-09-06 2013-12-18 ResMed Limited Forehead pad for respiratory mask
GB0320761D0 (en) * 2003-09-05 2003-10-08 Smiths Group Plc Resuscitators
NZ587820A (en) 2004-06-16 2012-03-30 Resmed Ltd Cushion with a gusset for a respiratory mask assembly
JP4864976B2 (en) * 2005-10-11 2012-02-01 ビーイー・インテレクチュアル・プロパティー・インコーポレイテッド Improvement of respirator and adjuster for airplane
US20080156383A1 (en) * 2006-11-28 2008-07-03 Caterpillar Inc. Fluid-transfer system
WO2008097610A1 (en) * 2007-02-07 2008-08-14 Avox Systems, Inc. Bi-directional valve
US8464715B2 (en) * 2008-04-16 2013-06-18 Stephen Donald Flynn, SR. Multipurpose therapeutic face mask
EP2361656B1 (en) * 2010-02-26 2016-06-08 Dräger Safety AG & Co. KGaA Respirator mask
GB2497350B (en) * 2011-12-09 2017-10-18 Intersurgical Ag Valve for respiratory masks
US9993604B2 (en) 2012-04-27 2018-06-12 Covidien Lp Methods and systems for an optimized proportional assist ventilation
US10362967B2 (en) 2012-07-09 2019-07-30 Covidien Lp Systems and methods for missed breath detection and indication
US9027552B2 (en) 2012-07-31 2015-05-12 Covidien Lp Ventilator-initiated prompt or setting regarding detection of asynchrony during ventilation
US9950129B2 (en) 2014-10-27 2018-04-24 Covidien Lp Ventilation triggering using change-point detection
CN105598686B (en) * 2016-01-08 2018-03-20 苏州隆士丹自动化技术有限公司 A kind of kludge of mouth mask breather valve
GB201609168D0 (en) 2016-05-25 2016-07-06 3M Innovative Properties Co Exhaust valve shroud for a personal protection respiratory device
CN114904112A (en) * 2016-10-05 2022-08-16 费雪派克医疗保健有限公司 Patient interface
JP6833285B2 (en) * 2017-04-18 2021-02-24 株式会社重松製作所 Positive pressure exhaust valve for respiratory protective equipment
US11324954B2 (en) 2019-06-28 2022-05-10 Covidien Lp Achieving smooth breathing by modified bilateral phrenic nerve pacing

Family Cites Families (15)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2359008A (en) * 1941-02-07 1944-09-26 Air Reduction Exhaling valve
US2473518A (en) * 1946-12-16 1949-06-21 Howard F Garrard Pressure breathing mask for aviation
US2629375A (en) * 1950-10-20 1953-02-24 Bendix Aviat Corp Exhalation valve
US2828740A (en) * 1956-12-07 1958-04-01 Sierra Eng Co Emergency exhalation valve
US3050054A (en) * 1957-08-01 1962-08-21 Robertshaw Fulton Controls Co Breathing apparatus
US3444857A (en) * 1962-03-19 1969-05-20 Edouard Paul Victor Raoul Gode Compensated action nonreturn exhalation valve,more particularly for respiratory mask
US3256898A (en) * 1962-07-17 1966-06-21 British Executive And General Compensated expiratory valves
US3189027A (en) * 1962-11-29 1965-06-15 Jr Roscoe G Bartlett Anti-suffocant apparatus for oxygen supply systems
FR1389614A (en) * 1964-01-09 1965-02-19 Beagle Auster Aircraft Ltd Compensated exhalation valves, particularly for oxygen masks for aircraft pilots
US3342200A (en) * 1965-03-12 1967-09-19 Sierra Eng Co Oxygen mask exhalation check valve
US3362420A (en) * 1965-08-11 1968-01-09 Navy Usa Anti-suffocation valve
US3366108A (en) * 1965-09-20 1968-01-30 Navy Usa Pressure regulating valve for rebreathing apparatus
US3459216A (en) * 1967-06-01 1969-08-05 Sierra Eng Co Pressure compensated exhalation valve
FR2076779A5 (en) * 1970-01-28 1971-10-15 Delverdier Maurice
US3688794A (en) * 1970-08-10 1972-09-05 Bird F M Exhalation valve for respirator

Also Published As

Publication number Publication date
GB2143137B (en) 1986-10-22
DE3424822A1 (en) 1985-01-24
JPS6036067A (en) 1985-02-25
GB8417685D0 (en) 1984-08-15
FR2548911A1 (en) 1985-01-18
SE8403712L (en) 1985-01-15
SE8403712D0 (en) 1984-07-13
GB2143137A (en) 1985-02-06
US4606340A (en) 1986-08-19

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