OXYGEN SYSTEM FOR PARACHUTING

Abstract

An oxygen system supplies either 100% oxygen to a demand valve in a or pulses of oxygen to the mask. Switching is automatic during a parachute descent. The system includes a valve manifold that is responsive to ambient pressure such that at low pressures it is configured to deliver gas from either an oxygen cylinder or an aircraft supply line to the mask demand valve and at higher pressures it is configured to deliver gas from the cylinder to a pulse gas delivery system. The mask also includes an inhalation valve that is closed if oxygen is supplied to the demand valve. Otherwise, the inhalation valve opens to allow ambient air to be drawn in and the pulse gas delivery system delivers a pulse of oxygen in response to the onset of inhalation.

Claims

1. A supplementary oxygen system for variable-altitude use, the system comprising: a valve manifold that is connectable via a regulator to a pressure vessel containing compressed oxygen, the valve manifold having first and second outputs and an output selection valve; a pulse gas delivery system in fluid communication with the second output and that is activatable to deliver a pulse of gas of predetermined duration; wherein the output selection valve is switchable between a first position in which gas flowing through the manifold is directed to the first output and a second position in which gas flowing through the manifold is directed to the second output and to the pulse gas delivery system.

2. The mask for use with the supplementary oxygen system of claim 1 and that is configured to seal around a user's mouth and nose, the mask comprising: a demand valve that is connectable to the first output of the valve manifold; an inhalation valve; a connection manifold that is connectable with an output of the pulse gas delivery system; an exhalation valve; and a piloting line that provides fluid communication between the inhalation valve and an input to the demand valve, wherein the inhalation valve is configured such that it is closed if a gas pressure above ambient is present in the piloting line and openable to allow ambient air to be drawn into the mask otherwise and the pulse gas delivery system is configured to be responsive to a drop in pressure inside the mask to deliver a pulse of oxygen.

3. The mask in accordance with claim 2 wherein the inhalation valve is openable in response to a drop in pressure within the mask, and wherein the pressure drop required to initiate opening of the valve is a larger drop than that to which the pulse gas delivery system is responsive.

4. The mask in accordance with claim 2 wherein the connection manifold is located at a position on the mask that, when fitted to a user, is in the vicinity of the user's nose and mouth.

5. The supplementary oxygen system in accordance with claim 1 that includes the mask as set out in claim 2.

6. The supplementary oxygen system in accordance with claim 1 that also includes a switching mechanism responsive to atmospheric pressure, wherein if atmospheric pressure is below a threshold level then the output selection valve is in its first position and if the atmospheric pressure is above a threshold level then the output selection valve is in its second position.

7. The supplementary oxygen system in accordance with claim 6 wherein the output selection valve includes: a fluid passageway that is moveable with a reaction member; a biasing means arranged to urge the reaction member and fluid passageway to a configuration in which the output selection valve is in its second position and fluid flow through the fluid passageway is to the second output and pulse gas delivery system; a control chamber adjacent the reaction member and in fluid communication via a restricted passage with a gas source, in which a build up of gas pressure within the chamber serves to urge the reaction member and fluid passageway to a configuration in which the output selection valve is in its first position and fluid flow through the fluid passageway is to the first output; and wherein the switching mechanism includes: a pressure responsive element; and a switching valve coat seat; whereby the switching valve seat may be either open or closed in response to a state of the pressure responsive element such that when the valve seat is in its low-pressure configuration, gas is directed into the control chamber.

8. The supplementary oxygen system in accordance with claim 7 wherein the roles of the biasing means and the control chamber are reversed, that is, the biasing means urges the reaction member to a configuration in which the output selection valve is in its first position and fluid flow is to the first output and gas pressure within the control chamber serves to urge the reaction member to a configuration in which the output selection valve is in its second position and fluid flow is to the second output and pulse gas delivery system; and gas is directed into the chamber when the switching valve seat is in its high-pressure configuration.

9. The supplementary oxygen system in accordance with claim 7 wherein the pressure responsive element is an aneroid which expands as atmospheric pressure is reduced, and the switching valve seat is in its low-pressure configuration when closed, the aneroid being arranged such that, at or below the threshold pressure it is of a length sufficient to seal the switching valve seat.

10. The supplementary oxygen system in accordance with claim 6 wherein the output selection valve is a solenoid valve that is connected to an output of an atmospheric pressure sensor.

11. The supplementary oxygen system in accordance with claim 1 wherein the valve manifold also includes an input selection valve that is in fluid communication with an input to the output selection valve via a link passage, the input selection valve being switchable between a first position in which gas flow from an input cylinder port that is connected to an output of the regulator is directed towards the link passage and a second position in which gas flow from a supply port is directed towards the link passage, the supply port being adapted to receive a connector from an external oxygen supply.

12. The supplementary oxygen system in accordance with claim 11 wherein the system also includes an input selection valve switching mechanism responsive to gas pressure within the supply port.

13. The supplementary oxygen system in accordance with claim 12 wherein the input selection valve includes: a fluid passageway that is moveable with a reaction member; and a biasing means arranged to urge the reaction member and fluid passageway to a configuration in which the input selection valve is in its first position in which gas flow from the input cylinder port is directed towards the link passage; and wherein the supply port and reaction member are arranged such that gas pressure arising from gas flowing into the input selection valve from the supply port urges the reaction member towards a configuration in which the input selection valve is in its second position in which gas flow from the supply port is directed towards the link passage.

14. The supplementary oxygen system in accordance with claim 13 wherein a control chamber is located adjacent the reaction member and in fluid communication via a passage with the supply port and positioned such that gas pressure within the chamber counters the effect of the biasing means on the reaction member.

15. The supplementary oxygen system in accordance with claim 14 wherein the biasing means is set such that it balances gas pressure within the chamber at a supply pressure threshold level.

16. The supplementary oxygen system in accordance with claim 11 wherein the system includes an inhibitor mechanism that is actuated by attachment of the connector to the supply port to prevent the output selection valve from being switchable to its second position.

17. The supplementary oxygen system in accordance with claim 7, wherein: the valve manifold also includes an input selection valve that is in fluid communication with an input to the output selection valve via a link passage, the input selection valve being switchable between a first position in which gas flow from an input cylinder port that is connected to an output of the regulator is directed towards the link passage and a second position in which gas flow from a supply port is directed towards the link passage, the supply port being adapted to receive a connector from an external oxygen supply; and the output selection valve reaction member has an end face that is located in the vicinity of the supply port and the reaction member is configured such that, on attachment of the connector, a peripheral surface of the connector makes contact with the end face and prevents it moving into the position required for the output selection valve to direct fluid flow to the second output.

18. The supplementary oxygen system in accordance with claim 11 for use with an oxygen aircraft supply line to which the connector is fitted, wherein the connector includes a check valve that is openable by way of connection of the connector to the supply port.

19. The supplementary oxygen system in accordance with claim 18 wherein the aircraft supply line also includes a minimum pressure shut-off valve that is arranged to cut off supply to the connector if gas pressure within the aircraft supply line falls below a threshold value and a regulator adapted to, if the shut-off valve is open, deliver gas at substantially constant pressure to the connector.

20. The supplementary oxygen system in accordance with claim 7 wherein the output selection valve reaction member is a spool piston configured to run in a bore that includes a series of spool seals between respective pairs of which are located openings leading to the first output, a link passageway and the second output and wherein the fluid passageway is formed by a narrowed region of the piston that cannot make contact with the seals.

21. The supplementary oxygen system in accordance with claim 13 wherein: the input selection valve reaction member is a spool piston configured to run in a bore that includes a series of spool seals between respective pairs of which are located openings leading to the input cylinder port and the link passageway; the supply port opens into the bore at a location outside the seals, on a side in closer proximity to the link passageway; and the fluid passageway is formed by a narrowed region of the piston that cannot make contact with the seals.

22. A valve manifold for directing gas flow therethrough from either one of a pair of input ports to either one of a pair of output ports, with one possible flow connection being suppressed, the manifold comprising: an input selection valve with output to a link passageway and an output selection valve with input from the link passageway, wherein the input and output selection valves include respective spool pistons with narrowed regions configured to run in respective bores that each include a series of spool seals between respective pairs of which are located openings which, in the input selection port lead to a first input port and to the link passageway and, in the output selection port, to the first output port, the link passageway and the second output port; and a sealable second input port is located in the bore of the input selection valve outside the seals proximal to the link passageway; the input spool piston is moveable by means of gas pressure at the second input port and between a first position in which the narrowed region is positioned at a central seal such that the first input port is in fluid communication with the link passageway and a second position in which the narrowed region is positioned at a seal intermediate the second input port and link passageway, thereby providing fluid communication therebetween; and the output spool piston is moveable by means of a switching mechanism that is responsive to atmospheric pressure and between a first position in which the narrowed region is positioned at a seal located intermediate the first output port and the link passageway and a second position in which the narrowed region is positioned at a seal located intermediate the link passageway and the second output port; and wherein the manifold includes an inhibitor mechanism that is actuated by attachment of an external connector to the second input port to prevent the output selection valve from being switchable to its second position.

Description

[0031] The invention will now be described, by way of example only, and with reference to the accompanying drawings, in which:

[0032] FIG. 1 shows a possible embodiment of the present invention, integrated into a complete bailout system, including the hose to deliver the oxygen from the aircraft oxygen supply.

[0033] FIG. 2A to 2C show different views of a possible embodiment of the present invention, illustrating a bailout valve manifold, with its different functions.

[0034] FIGS. 3A to 3D show a possible embodiment of an input and output mode selection manifold that selects the oxygen source and delivery mode.

[0035] FIG. 4 shows a possible embodiment of a mask according to the present invention, with its parts.

[0036] FIGS. 5A and 5B show a possible embodiment of an anti-suffocation valve according to the present invention, which is open when pressure to the demand valve is not present (as shown in FIG. 5A), allowing the user to inhale through an inhalation valve, and closed (as shown in FIG. 5B) when the pressure to the demand valve supply is present.

[0037] FIG. 6A shows a detail embodiment of a regulator and low pressure shut-off valve according to the present invention, in the open position. FIG. 6B shows the same in the closed position, when the supply pressure is below the threshold.

DESCRIPTION OF PREFERRED EMBODIMENTS

[0038] FIG. 1

[0039] With reference to FIG. 1, there is shown an overview of a complete bailout system that includes aspects of the present invention. Also shown in the overview is the hose to deliver oxygen from the aircraft oxygen supply that is detached at the bailout cylinder end before exiting the aircraft.

[0040] A cylinder (or other pressure vessel) (1) containing oxygen at high pressure (2) is connected to a bailout manifold valve (3). The detail of the manifold valve is shown in FIGS. 2 and 3 and its operation will be explained in more detail later, with reference to these figures.

[0041] The manifold valve has two outlets. The first is a supply (4) to a demand valve (6). The demand valve uses known technology to deliver 100% oxygen in response to a user's demand. The second supply (5) is to a connection (5a) on a mask (9). This outlet is used to deliver pulsed oxygen in response to a user's inhalation. A flow indicator (8) may be incorporated in the second supply line (5) to give a visual indication of pulsed flow.

[0042] The supply to the demand valve is also fed to an inhalation valve (7) via a tube (4a). The inhalation valve is closed when pressure to the demand valve (6) is present, thus ensuring that all inhalation is from the demand valve. When there is no pressure to the demand valve (6), the inhalation valve is open, allowing the user to inhale though a valve with a small opening pressure. The pressure required to open the inhalation valve is relatively small, but still set to be higher than that needed to activate a pulsed delivery system in the bailout manifold valve (3). This timing of oxygen delivery ensures that oxygen is included at the start of the inhalation gas intake. That is, the user will first inhale the pulsed oxygen and then the remainder of their inhalation breath will be formed from ambient air drawn through the inhalation valve.

[0043] An oxygen supply hose (10) includes a connector (11), which is used to connect to the aircraft oxygen supply, typically at 5 bar, two lengths (12, 14) of hose and a pressure shut-off valve and regulator (13). The hose (12) extends between the connector (11) and the input of the minimum pressure shut-off valve and regulator (13). This device (13) reduces the input pressure in the supply hose (14) to the working pressure of the bailout manifold valve (3), which is lower than the normal output pressure of the aircraft oxygen supply. If the pressure of the aircraft oxygen supply falls below a threshold, typically just below the level of the working pressure of the bailout manifold, the minimum pressure shut-off (13) activates and shuts.

[0044] The output of the minimum pressure shut-off valve and regulator (13) feeds through a hose (14) to a connector (15), which connects into a port in the bailout manifold valve (3). Fitting the connector (15) to the bailout manifold valve mechanically switches the output to be 100% oxygen through the demand valve and supplies the system with oxygen from the aircraft supply.

[0045] If the aircraft oxygen supply fails, but connector (15) is still connected to the bailout manifold valve (3), a valve in the bailout manifold valve switches, so that the user inhales from the bailout cylinder (1), without interruption to their breathing.

[0046] When the connector (15) is disconnected from the bailout manifold valve (3), the valve becomes responsive to ambient air pressure. A valve within the bailout manifold valve determines either 100% oxygen delivery or pulsed oxygen delivery, each delivered from the bailout cylinder. The valve switches automatically between these two states, as dictated by ambient pressure.

[0047] FIGS. 2A to 2C

[0048] These FIGS. 2A to 2C illustrate, from different angles, a bailout valve manifold in accordance with an embodiment of the present invention. The bailout valve manifold consists of three main components.

[0049] High Pressure Valve and Regulator, (201).

[0050] The high pressure valve and regulator (201) delivers low pressure (typically 4 bar) oxygen to the parts downstream. It consists of a threaded connection (202) to the cylinder (1), with an on-off valve (203) a fill connection (204), a pressure indicator (205), burst disc, (206) and a regulator (207). These elements are well known to one skilled in the art, so will not be described in detail. The on-off valve may be omitted or replaced with a valve on the low pressure side, after the regulator.

[0051] Input and Output Mode Selection Manifold (211).

[0052] This is described in more detail with reference to FIG. 3, but an overview of its function is as follows:

[0053] The manifold (211) includes an arrangement of valves and passages. The configuration of the valves determines which particular passages are brought in to form a fluid connection between one of two inputs: one from the regulator (201) via interface (208) and a second being an oxygen input (209) from the aircraft oxygen supply; and one of two outputs: a first being an input (213) of the oxygen pulse delivery system via interface (210) and the second being the outlet (4) to the demand valve.

[0054] The oxygen input (209) receives the connector (15) from the aircraft oxygen supply. The connector mechanically activates a valve (shown in FIG. 3A) within the manifold to select delivery to the demand valve outlet connection (4), and to close the output to the pulsed delivery unit (212).

[0055] The detail of the input and output mode selection manifold can be more clearly understood with reference to FIG. 3.

[0056] Oxygen Pulse Delivery Unit (212)

[0057] Examples of pulse delivery units are known in the prior art. In this embodiment, the unit (212) receives oxygen from the input and output selection manifold, as determined by various components within the manifold (211). The unit delivers a pre-determined pulse of oxygen to a user immediately in response to a drop in pressure, at the onset of the user's inhalation. Such devices are, for example, described in EP1863555, “Conserving device for breathable gas”.

[0058] FIGS. 3A to 3D

[0059] FIGS. 3A to 3D show schematic sections of an embodiment of an input and output mode selection manifold (211) that selects the oxygen source and delivery mode. The views put into one plane all the working elements to enable them to be seen together, to aid understanding.

[0060] The function of the input and output selection manifold in all operating states, is shown in the progression of FIGS. 3A through to 3D.

[0061] FIG. 3A shows the input and output selection valves in the position they are in when the aircraft oxygen supply is connected, regardless of the ambient pressure. This is as would be seen in a pressurised, or depressurised, cabin for pre-breathing on 100% oxygen from the aircraft oxygen supply.

[0062] FIG. 3B shows the input and output selection valves in the position they are in when the aircraft oxygen supply is connected, regardless of the ambient pressure, but the supply of oxygen is insufficient. This is as would be seen when the aircraft oxygen supply has failed, so the pressure at the connector (15) is zero.

[0063] FIG. 3C shows the input and output selection valves in the position they are in when the aircraft oxygen supply is disconnected, and the altitude is higher than the threshold for 100% oxygen.

[0064] FIG. 3D shows the input and output selection valves in the position they are in when the aircraft oxygen supply is disconnected, and the altitude is lower than the threshold for 100% oxygen.

[0065] With reference first to FIG. 3A, a housing (300), contains three main elements that make up the input and output mode selection manifold.

[0066] Aircraft Oxygen Supply Connection (15)

[0067] The Aircraft oxygen supply connection (15) is connected to a port (315) in the housing (300). A seal (316) on a connector (317) seals against the side of the port (315). The connector (317) is held in the port by a hand-wheel (318) retained by a thread (319). The connector (15) and its parts can be seen more clearly in FIG. 3C. A check valve (320) in the connection includes a poppet (322) with end (321) and seal (324) that is biased towards a closed position by a spring (323). As the connection is made, contact between the end (321) of the poppet (322) and some part of the housing (300), moves the seal (324) against the bias of the spring (323) and out of sealing contact with a bore (325).

[0068] When the aircraft oxygen supply connection is disconnected from the connection (315), as shown in FIG. 3C, the spring urges the poppet (322) to a closed position in which the seal (324) is in sealing contact with the bore (325). This means that there is no flow from the aircraft oxygen supply connection, unless it is connected to the bailout system.

[0069] Input Selection Valve (301)

[0070] The input selection valve directs oxygen to a passage (304). The oxygen enters the input selection valve (301) either from a port (303) in connection with the regulator (207) (hence from the bailout cylinder) or from a connector (15) of the aircraft oxygen supply hose (14) The passage (304) connects to the input of the output selection valve (302).

[0071] If the aircraft oxygen supply is connected and pressure is present, the aircraft oxygen supply is selected. If the aircraft oxygen supply fails, or is not connected, the passage (304) is connected via port (303) to the regulator output (207).

[0072] A pressure supply spool piston (305) runs in spool seals (306), (307), (308). The piston includes an end (309) located at the aircraft oxygen supply connection port (315) and a sliding piston head seal (350) running in a bore (351) that defines a chamber (310) in the housing (300). If aircraft oxygen supply pressure is present, it acts on the end (309) of the piston and also builds up in the chamber (310). Pressure in this chamber (310) acts on the sliding piston head seal (350), in a direction that reinforces the effect of pressure at the end (309). The bias supplied by the spring (314) counters this effect of aircraft supply pressure. The net result of the forces on the piston (305) is that it can be biased into either of two positions. The aircraft oxygen supply pressure is communicated to the chamber (310), via a passage (311). A vent to atmosphere (348) ensures that there is no trapped pressure on the spring side (314) of the supply spool piston and so is free to move.

[0073] The spring and piston sizes are arranged such that when the aircraft oxygen supply is at a normal level, pressure biases the piston to be in the position shown in FIG. 3A, so the large diameter of the spool (312) is clear of the o-ring (308), so oxygen is free to flow from the connection (15) to the passage (304).

[0074] When the aircraft oxygen supply level fails and drops to zero, or the connector (15) is disconnected, the spring biases the spool piston (305) to be in the second position seen in FIG. 3B. The large spool diameter (312) slides into sealing contact inside the seal (308), blocking off the connection between the aircraft oxygen supply and the passage (304). The small diameter (313) of the spool (305) is in line with o-ring (307), opening the path between supply (303) and the passage (304) so the passage (304) is supplied with oxygen from the bailout cylinder via the regulator (207).

[0075] Output Selection Valve (302).

[0076] The output selection valve supplies oxygen from the passage (304) to: [0077] (A) Output (4) to feed the demand valve (6 in FIG. 1) if the aircraft oxygen supply (15) is connected or if the ambient pressure is below the threshold for 100% oxygen delivery; or [0078] (B) The output (213) (also see FIG. 2A) to supply the pulse delivery unit (212 in FIG. 2B) if the aircraft oxygen supply is disconnected and the ambient pressure is above the threshold for 100% oxygen delivery.

[0079] FIG. 3A shows one embodiment of output selection valve that is configured to state (A). An output selection spool piston (326) runs in a bore in the housing (300) and is arranged to be moveable between two positions. In a first position, as shown in FIG. 3A, the large spool diameter (327) is in sealing contact with o-rings (328), (329), and (331), and the small spool diameter (332) is in line with the o-ring (330), allowing gas to flow from passage 304 to the outlet (4) to feed the demand valve for 100% oxygen.

[0080] In FIGS. 3A and 3B, the piston is held in this position by a face (333) of the piston (326) being pushed by a face (334) of the hand wheel (318) of the connector (15). This prevents the piston being moved by a spring (352), which is arranged to apply a bias towards the piston position in which gas output (213) is to the pulsed delivery system (212). Whatever the ambient pressure, therefore, the gas supply is to the demand valve feed (4).

[0081] When the connector 15 is removed and the ambient pressure is lower than the threshold for 100% oxygen, and so supply to the demand valve needs to be maintained, it is necessary that the piston is kept in this position, even though the hand-wheel (318) is not there to push it.

[0082] This alternative mechanism to maintain position (A) is achieved by a pressure building up in the chamber (335), which acts on a seal (349) on the head (347) of the piston, sliding in a bore (337). When pressure at the output pressure of the regulator (207) is present in chamber (335), the piston (347) is held in the position shown in FIGS. 3A to 3C.

[0083] Position (B) is achieved as follows: When pressure is not present in the chamber (335), the spring (352) moves the piston to the second position, as shown in FIG. 3D. In this state, the position of the small diameter (332) of the spool is in line with o-ring (329), allowing a connection from the passage (304) to the feed (213) to the pulse delivery unit (212) (not shown).

[0084] A vent to atmosphere (346) ensures that there is no trapped pressure on the spring side (347) of the output selection spool piston (326) and so the spool piston is free to move.

[0085] The pressure in chamber (335) is controlled as follows:

[0086] Gas from a connection from the regulator (207, not shown) communicates with a port (336). The pressure acts to push gas through a bleed restrictor (353) into a passage (338). The restrictor is set to give a low flow, arranged to be small in the context of the cylinder and expected duration e.g. in the region 10 ml/min.

[0087] Passage (338) communicates with a seat (339), which can be sealed or open according to the position of a seal (340) under the action of an aneroid (342).

[0088] In FIG. 3A, the ambient pressure is above the threshold set for 100% oxygen. The higher pressure means that the aneroid (342) is compressed, with the result that the seal (340) is out of contact with the seat (339). The bleed flow from the restrictor (353) into the passage (338) is therefore free to flow from the seat (330) and out of a vent (341) to ambient. The seat is arranged to be as small as possible, to minimise seat pressure force on the aneroid, but large compared the bleed restrictor (353). There is therefore no pressure build-up in the passage (338) or the chamber (335), so the spool piston (357) is free to be moved by the spring (334) if the connector (15) is disconnected, or by the connector hand wheel face (334) acting against the spring when the connector is connected.

[0089] The situation shown in FIG. 3C arises when the parachutist is at high altitude, where the pressure is below the threshold and 100% oxygen is required. The aneroid (342) is expanded, and the seal (340) sealably held against the seat (339). Flow from the bleed restrictor (353) cannot escape, and so the pressure in the passage (338) and chamber (335) builds up until it is equal to the supply pressure. This pressure, acting on the area of the seal (349), pushes the piston against the spring (352) to the position shown in FIG. 3C, so the user is breathing 100% oxygen.

[0090] As the parachutist falls and the pressure around him increases, the aneroid (342) compresses in response to the ambient pressure increase. As the pressure increases above the threshold for 100% oxygen, the seal (340) moves away from the seat (339), and breaks the seal. The pressure in the chamber (335) and the passage (338) escapes, and exits through the vent (339), and the spring (334) urges the piston to position (A), as seen in FIG. 3D.

[0091] In FIG. 3C, the connector (15) is shown in its configuration when disconnected from the manifold. The spring (323) urges the poppet (322) into a sealing position, where the seal (324) seals the bore (334). This prevents the escape of gas from the supply hose (10 in FIG. 1).

[0092] The aneroid (342) can be adjusted by the thread (343) of an adjusting screw (344), which is advantageously connected to the aneroid. The screw can be set such that the aneroid opens at a given pressure by holding it at the threshold pressure, monitoring the pressure in chamber (335), and adjusting the thread using a screwdriver in the slot (345). The setting can be checked by changing the pressure around the parts, and noting the pressure around the aneroid at which the pressure in chamber (335) collapses. The thread (343) can be locked by use of a suitable sealant.

[0093] FIG. 4

[0094] This figure shows an embodiment of a mask assembly according to an aspect of the present invention, with its parts. Most are known so will not be described in detail, and, where necessary, additional detail is shown in subsequent figures.

[0095] A face-seal (401) made of a resilient material such as rubber is shaped to seal against the face of a user. A hard shell or exoskeleton (402) may be used on the outside of the rubber with a number of fastening features (403), which are used to attach a harness or similar to hold the mask to the face.

[0096] The mask and harness may be available in a number of sizes to seal to the faces of a variety of users.

[0097] The supply (4) to the demand valve (6) supplies oxygen according to the input and output selection manifold (211). The demand valve may be any of a number of types, able to provide oxygen to the user to meet their demand, for example that described in EP14168160.1 “Medical breathing apparatus”. It may be advantageous for the demand valve to provide a slightly positive pressure—i.e. slightly above atmospheric pressure so that if there are any leaks, they are out, and not in. Achieving positive pressure with a demand valve is known.

[0098] A connector (406) at the feed to the demand valve allows the same pressure that is feeding the demand valve to be fed via a tube (4a) to a combined inhalation and anti-suffocation valve (7) which is shown in more detail in FIGS. 5A and 5B. When pressure is present, the valve (7) is closed, so any gas inhaled by the user comes from the demand valve. When pressure is not present, the valve is open, allowing inhalation through an inhalation valve that opens in response to a pressure difference across it. When the demand valve is not pressurised, supplementary oxygen is delivered from the pulsed delivery unit (212), and the pressure to trigger an oxygen pulse is generated by the opening pressure of the inhalation valve.

[0099] A tube (5) to the connection manifold (5a) joins the mask to the pulse delivery unit (212), such that the pressure in the mask at the onset of inhalation is communicated to the pulse delivery unit and flow from the pulse delivery unit is delivered into the mask. The connection manifold inside the mask directs the oxygen to the region of the mouth and nose of the user, so that as much of the pulse of oxygen as possible is inhaled with the initial inhalation. A conformable tube, i.e. one that is able to be bent to a shape, which is then maintained, may be provided inside the mask, connected to the inside of the connection manifold (5a) to help achieve this for difference face shapes and sizes.

[0100] An exhalation valve (404) allows exhalation. If the demand valve delivers negative pressure (i.e. when breathing from the demand valve, there is never a pressure higher than ambient inside the mask during inhalation), the exhalation valve would have to have an opening threshold above the range of positive pressure encountered, so that the demand valve did not leak gas out of the exhalation valve. This is known, and normally achieved by a sprung valve, or a resilient flap valve, arranged to be deflected at the point it is closed. Typically a housing around the exhalation valve directs the exhaled gas downwards through a “snood”, (405), which also helps to prevent icing of the exhalation valve in cold conditions, by shielding it from ambient air and protecting the heat transferred from the exhaled air. The direction downwards also helps to prevent misting of any goggles or visor the user may be wearing.

[0101] FIGS. 5A and 5B

[0102] FIG. 5B shows a possible embodiment of a combined inhalation and anti-suffocation valve according to the present invention that is closed when pressure to the demand valve (6) is present in the tube (4a).

[0103] A housing (501), which is on the atmosphere side of the mask (9), receives the pressure connection (4a) communicating pressure to a piston (502) with a seal (503) operating in a bore (504) that urges the piston against a closing spring (505) to a closed position, where a resilient sealing member (506), mounted on the outside of the piston (507), is held closed against a seat (508) of a second housing (509).

[0104] A gap in the second housing (509) seals to the mask.

[0105] FIG. 5A shows the mask in the open position, when the pressure to the demand valve supply is not present. The spring (505) urges the piston (502) away from the seat (508) creating an opening (510) though which the user may inhale.

[0106] An inhalation valve (511), consisting of a disc (512) of resilient material, fixed in the middle with a fastener (513), and arranged to be deformed against an inhalation valve seat (514) in the closed position, such that the pressure in the mask has to be a little lower or negative compared to the ambient pressure. The level of the negative pressure for opening the inhalation valve (511) is arranged to be at a level such that the pulse delivery unit (212 in FIG. 2B) triggers before the inhalation valve opens.

[0107] This allows the user to inhale the remainder of their inhalation from ambient atmosphere, thus providing a pulsed oxygen supplement.

[0108] FIGS. 6A and 6B

[0109] FIG. 6A shows a detail embodiment of a regulator and low pressure shut-off valve that may be used with the present invention, in the open position, when pressure from the aircraft oxygen supply is present at the correct level, typically 5 to 6 bar.

[0110] An inlet (601) in a housing (600) receives pressure from the hose (12 in FIG. 1) from the aircraft oxygen supply. A passage (602) transmits the gas to the inlet (609) of a regulator (610). A closing piston (603) with a seal (604) sealably sliding in a bore (605) in the housing (600). A closing spring (606) retained by a cover (607) is arranged to bias the piston to a closed position, where a seal (608) seal to the regulator inlet (609). Pressure in the passage (602) acts on the seal diameter of the piston, to urge the closing piston against the closing spring to an open position.

[0111] The regulator is a standard piston regulator which is well known, arranged to deliver a substantially constant pressure, typically 4 bar, which is about 1 bar, lower than that normally supplied by the aircraft oxygen supply.

[0112] When the pressure from the aircraft oxygen supply is in its normal range, the piston is held in an open position, and the regulator delivers normal 4 bar pressure to the hose (14 in FIG. 1).

[0113] FIG. 6B shows the same in the closed position, when the supply pressure is below the threshold for normal demand valve and pulse delivery operation.

[0114] As the supply pressure from the aircraft oxygen supply falls, the pressure becomes insufficient to hold the piston (603) open against the closing spring (606), and the closing piston moves to a closed position, in which the seal (608) closes the inlet to the regulator (609).

[0115] The aim of this arrangement is to ensure that as soon as the aircraft oxygen supply pressure drops below a level suitable for operation, the supply to the cylinder valve manifold is cut off. At this point the pistons in the valve manifold as described in FIGS. 3A to 3C, switch over completely immediately with no intermediate state.

[0116] It will be apparent to one skilled in the art that this embodiment of the invention provides an integration of 100% oxygen delivery via a demand valve and a pulsed oxygen delivery system in which a predetermined pulse of oxygen is delivered at the start of the inhalation cycle to supplement the oxygen in the ambient air. This alone leads to a remarkable improvement in the efficiency of oxygen delivery during a parachuting trip. In an alternative embodiment, the pulsed delivery system can be adapted to deliver a pulse of variable volume. The volume of oxygen in the pulse can be reduced as the parachutist descends, the pressure increases and the amount of oxygen drawn from the environment increases. This refinement represents, with increased conservation of oxygen, a still further improvement over the prior art.

SUMMARY

[0117] It will be clear to one skilled in the art that the present invention provides a means to provide supplementary oxygen to a parachutist in a way that uses the oxygen more efficiently than prior art, allowing for a smaller cylinder or longer duration or a combination of both.

[0118] It will also be clear that all the parts of the system lend themselves to be designed to give very clear “digital” function, in which there are no functions that rely on very precise characteristics.

[0119] The present invention provides a system that may be fully automatic in its operation, so that the user has merely to turn on the cylinder valve (203) and connect and disconnect the aircraft oxygen supply. All other changes happen automatically, so the user can concentrate on their other tasks, increasing safety and effectiveness.