Background of Invention
This invention relates to a gas pressure regulating valve for use in conjunction with underwater breathing apparatus.
Where the breathable gases supplied to a diver include a reclaimable gas such as helium, then exhaled gases are piped to surface apparatus for extraction of the reclaimable gas in a line at a lower pressure than the divers gas exhalation pressure. A valve usually termed a "gas reclaim" or "gas recovery" valve is used to isolate the divers breating space from the lower pressure in the gas reclaim line. One previously proposed gas reclaim valve is a single stage device having the disadvantage that the divers exhalation effort to operate the valve varies according to the pressure differential with the reclaim line. This disadvantage gives rise to discomfort in breathing; and moreover such a single stage device offers relatively little safeguard against the diver being subjected to reclaim line pressure (suction) in the event of a malfunction. Another previously proposed gas reclaim valve is a two-stage valve, but having the disadvantages of, first, being of unduly large physical dimensions and, second, having a relatively large number of moving components whose total mass is such as to demand undue breathing effort to operate the valve. Moreover, this valve is prone to malfunction in the event of ingress of foreign matter, particles, hair etc.
An object of the present invention is to provide a gas pressure regulating valve for use in conjunction with underwater breathing apparatus in which the aforesaid disadvantages are obviated or mitigated.
According to the present invention, there is provided a gas pressure regulating valve for use in conjunction with underwater breathing apparatus, comprising a first chamber disposed between a first shiftable wall member and a first fixed wall member for receiving exhaled gases, a second chamber disposed between a second shiftable wall member and a second fixed wall member, the first and second fixed wall members defining a third chamber therebetween for connection with a gas reclaim line, and a tubular duct extending from the first chamber to the second chamber through both wall members, said first shiftable wall member cooperating with an adjacent end of said tubular duct to constitute a first stage valve, and said second shiftable wall member cooperating with ports in said second fixed wall member to constitute a second stage valve.
An embodiment of the present invention will now be described, by way of example, with reference to the accompanying drawings in which:
FIG. 1 is a sectional elevation of a gas reclaim valve in accordance with the present invention; and
FIG. 2 is a plan view showing a modification of a part of the valve of FIG. 1.
In FIG. 1 a first stage chamber 10 is defined between a first shiftable wall member or diaphragm 11 and a first fixed wall member 12. The wall member 12 is formed integrally with a peripheral skirt portion 12A which fits snugly within a protective outer cup 13 and in cooperation with an annular seal 14 forming the periphery of the flexible diaphragm 11. The outer cup 13 is adapted for mounting on a divers head gear (part of which is represented at 15) by means of a clamp plate 16 and clamp screw 17. The first stage chamber 10 serves to receive divers exhaled gases directly through an inlet tube 18.
A second stage chamber 19 is formed between a second shiftable wall member in the form of a diaphragm 20 and a second fixed wall member in the form of an annular land 21 having a convex surface configuration with which the diaphragm 20 cooperates to cover a plurality of ports or openings 22 communicating with a third chamber 23 disposed between the wall member 12 and the annular land 21. The ports 22 consists of an annnular pattern of circular openings of different sizes of which the smallest are nearer the centre of the annular land 21 so that in use the gas flow rate between the chamber 19 and the chamber 23 is proportional to the degree to which the diaphragm 20 is lifted from its land. The annular land 21 fits snugly within a second outer cup member 24 and cooperates with an annular seal 25 forming the periphery of the diaphragm 20. The chamber 23 communicates with a gas reclaim line 26 by way of an exhaust tube 27 set into the cupped member 24.
The central portion of the diaphragm 11 is provided with a stiffening disc llA; and the central portion of the diaphragm 20 is provided with a circular spring seat and valve disc assembly 20A.
The first stage chamber 10 and the second stage chamber 19 are in mutual communication by way of a tubular duct 28 which extends through the wall member 12 and also through a central opening in the annular land 21. The duct 28 is formed integrally with the wall member 12. The duct 28 houses and locates a biasing compression spring 29 the function of which is explained herebelow. Within the first stage chamber 10 the end of the duct 28 adjacent the diaphragm 11 is cooperable therewith to constitute a first stage valve operable to close passage between chamber 10 and the chamber 19. The assembly 20A of the diaphragm 20 is cooperable with the adjacent (other) end of the duct 28 to constitute an auxiliary closure or valve operable to isolate the chamber 23 from the first stage chamber 10. Under normal operating conditions, as explained herebelow, the assembly 20A stands off from the adjacent end of the tube 28.
The cupped members 13 and 24 are provided with apertures so that surrounding sea water has access to the diaphragms 11 and 20 respectively.
Operation of the gas reclaim valve is as follows. A negative pressure differential of between 10 and 100 feet of sea water is applied to the reclaim line 26. External sea water pressure holds the diaphragm 20 against the annular land 21 to close off the ports 22. Under the action of the biasing spring 29, the chamber 19 is maintained at a negative pressure differential of 0.040 bar. The diaphragm 11 is held against the adjacent end of the duct 28 by external sea water pressure.
Upon the diver exhaling, the outer annular area of the diaphragm 11 is subjected to the exhalation pressure whereupon the diaphragm 11 is lifted from its seating on the adjacent end of duct 28 thereby admitting the exhaled gases to chamber 19. The exhaled gas pressure augmenting the biasing force of the spring 29 effects lifting of the diaphragm 20 which permits flow of exhaled gases into chamber 23 in a progressive manner by virtue mainly of the progressive increase in the size of the ports or openings 22 from which the diaphragm 20 is effectively peeled by the shifting of the assembly 20A. The convex configuration of the annular seat assists the progressive function. Upon cessation of the diver's exhalation, the lower pressure in the reclaim line 26 immediately effects reclosure of the second stage and reseating of the diaphragm 11 against the adjacent end of the duct 28.
In the event of a malfunction causing leakage past the diaphragm 20 towards the chamber 23, the interior of the duct 28 is ultimately closed by seating of the assembly 20A against the adjacent end of the duct 28. Thus, the assembly 20A constitutes an auxiliary closure in conjunction with the seating of diaphragm 11 to isolate the diver from the low pressure in chamber 23 and the reclaim line 26. Upon observing the notably increased exhalation pressure required to operate the reclaim valve, the diver may immediately continue his operations in open circuit mode by isolating the reclaim valve manually.
The disposition of the tubular duct 28 centrally of the vale with respect to the chambers and wall members confers of number of advantages. Since the larger outer annular area of the diaphragm is subjected initially to the divers exhalation pressure, the diaphragm 11 is relatively easily lifted from its seat against the adjacent end of the duct 28. Thereupon, the exhaled gases have direct access to the second stage chamber 19. Thus, the operating effort in terms of exhalation pressure is advantageously low. Since the ports 22 are deployed on a relatively large annular surface, the progressive action of the second stage of the valve is highly reliable. Further, the configuration of the first and second stage valves is such as to be tolerant of intruding particles and other foreign matter.
Modifications within the scope of the appended claims include re-positioning of or dispensing with the biasing spring 29 in which case resiliancy in the diaphragm 20 per se may be used to attain the requisite pressure differential in chamber 19. The assembly 20A may be dispensed with since the reclaim valve described will operate satisfactorily without the facility of the auxiliary closure. The configuration of the annular land 21 may be flat or concave instead of convex, so as to produce a different characteristic of the manner in which gas flow rate changes with lifting of the diaphragm 20. The ports 22 may take the form of slots disposed generally radially and each having an inner end portion configured to define a narrowing or tapering to a tip of negligible radius dimension. The modified port shown in FIG. 2 is given the same reference numerals for the corresponding part in FIG. 1 with the addition of suffix `A`. In FIG. 2, annular land 21A has a set of six ports 22A disposed radially and each having an inner end portion narrowing to a tip 32A of negligible (in context) radius dimension, for example 0.25 mm. The advantage of this narrowing configuration of the ports 22A is that the "break open" force required to lift the diaphragm (20) from closing engagement with the ports is minimized so that a smooth operation of the second stage of the valve is achieved.