This invention relates to crew masks to be used in large aircraft for crew safety in the event of decompression of the cabin. More particularly, the invention relates to the inflatable harness used to secure such a mask in place for use.
A commonly used type of crew mask includes an inflatable head harness with inflatable elastic tubes that are inflated prior to placement of the harness over the head of the user and that are then deflated to grip the user's head. A valve is connected to the tubes to control inflation by the pressurized oxygen supply of a regulator on the respiratory mask.
Another similar type of oxygen supply system includes an oxygen supply with a face mask and an inflatable head harness. A plurality of chemical oxygen generators provide pressurized oxygen to a reservoir to inflate the pneumatic head harness and provide an initial breathing supply during the startup of the chemical oxygen generators.
Aircraft crew masks with inflatable harnesses are currently limited to designs that use high pressure oxygen and regulators mounted at the mask. The high pressure oxygen supply for the regulator is also used for inflating the harness. However, longstanding designs for military oxygen masks have mounted the high pressure oxygen supply and the oxygen regulator in the aircraft panel, providing lower pressure breathable oxygen to the masks, so that no high pressure oxygen gas is available at the mask to inflate a harness. Current military masks are limited to older “hard” head harnesses requiring adjustment to fit, or are supported by a flight helmet. Inflatable harness masks are preferred because they fit a range of personnel head sizes without requiring pre-adjustment or custom sized designs required of the older hard head harnesses. Thus, it would be desirable to provide an inflatable harness crew mask adapted to allow rapid inflation of the harness, to allow adaptation of the older style military mask designs to gain the benefit of automatic adjustability of modern inflatable harnesses. The current invention solves these and other problems.
Briefly, and in general terms, the present invention provides for an inflatable harness crew mask with an inflatable harness utilizing a separate pressurized gas inflation supply assembly, independent from an oxygen supply system, to supply pressurized gas to inflate the inflatable harness, allowing the inflatable harness crew mask to be connected to an oxygen supply regulator mounted in an aircraft panel and providing lower pressure breathable oxygen to the mask, and allowing the inflatable harness to be inflated, independently of oxygen supplied from the oxygen supply regulator, to fit over the head of a user without requiring pre-adjustment or custom fitting.
The present invention accordingly provides for an inflatable harness crew mask, including a mask portion including a face seal molding formed to fit around the periphery of the face of the wearer, and an inflatable harness including at least one inflatable tube connected to the face seal molding. An inflation valve is connected in fluid communication with the inflatable harness to control inflation of the harness, and a pressurized gas inflation supply assembly is configured to supply pressurized gas to the inflation valve to inflate the inflatable harness. In a presently preferred aspect, the mask portion includes a valve connector housing, and an exhalation and inhalation valve is disposed in the valve connector housing and connected in fluid communication with the mask portion. The exhalation and inhalation valve includes an inlet configured to be connected to a source of oxygen for providing breathable oxygen to the mask portion. In another presently preferred aspect, the inflation valve is also disposed in the valve connector housing.
The inflation valve of the inflatable harness crew mask includes a housing having an inlet port and an outlet port, and an inflation valve poppet slidably disposed in the inflation valve housing, with a plunger pin slidably disposed in a first end of inflation valve housing and abutting the inflation valve poppet. The plunger pin is biased to a closed position, and a gas release button is pivotally connected to the valve connector housing and disposed adjacent to the plunger pin, allowing a user to manually press the gas release button to open the inflation valve poppet, and to in turn release pressured gas through the inflation valve outlet port. In another aspect, the inflation valve includes a pressure adjusting assembly. The inflatable harness may include first and second inflatable tubes configured to fit over the head of a user, may include one or more connecting straps connected between the first and second inflatable tubes, and the one or more connecting straps may be adjustable.
In another presently preferred aspect, the pressurized gas inflation supply assembly includes a pressurized gas inflation supply cylinder having a container portion with an interior chamber for removably receiving a main body portion of a compressed gas cartridge, and a regulator portion configured to removably receive a neck portion of the compressed gas cartridge at a first end of the regulator portion. The second end of the regulator portion includes a gas outlet port connected to the outlet end of the piercing lance member, and the gas outlet port of the regulator is connected to an inflation gas supply tube. The first end of the regulator portion is removably connectable to the container portion, and includes an interior plenum configured to removably receive the neck portion of a compressed gas cartridge. In another presently preferred aspect, the compressed gas cartridge is configured to provide sufficient compressed gas for multiple inflations of the inflatable harness, and the compressed gas cartridge is a compressed carbon dioxide gas cartridge.
The gas outlet port at the second end of the regulator portion of the pressurized gas inflation supply cylinder is connected to the inflation valve by the inflation gas supply tube. The first end of the regulator portion also preferably includes a piercing lance member having a conical pierce point inlet configured to pierce a septum of the neck portion of the compressed gas cartridge, and the piercing lance member includes an interior aperture configured to allow gas flow extending therethrough from the gas cartridge to an outlet end of the piercing lance member.
In another aspect, the regulator portion preferably includes a regulator valve adjacent to the outlet end of the piercing lance member. The regulator valve includes a regulator valve chamber, and a ball member disposed in the regulator valve chamber. The second end of the regulator valve may also include a gas pressure adjusting assembly configured to regulate the pressure of the gas released from the compressed gas cartridge to a desired lower harness inflation tube pressure. A pressure charge indicator assembly may also be mounted in fluid communication with the regulator valve chamber.
Other features and advantages of the present invention will become more apparent from the following detailed description of the preferred embodiments in conjunction with the accompanying drawings, which illustrate, by way of example, the operation of the invention.
While crew masks with an inflatable head harness are useful in placing a harness of a mask over the head of the user, pressurized oxygen that is commonly used to inflate such an inflatable harness is not available in some aircraft, such as military aircraft, so that a method and system for inflating an inflatable harness of a crew mask is needed that can be used in such aircraft in which a source of pressurized oxygen is not available for inflation of a crew mask head harness.
Referring to the drawings, which are provided by way of illustration and not by way of limitation, the invention is embodied in an inflatable harness crew mask 10, having a mask portion 11 typically including a clear flexible lens 12 mounted in an elastomeric face seal molding 14 formed to fit around the periphery of the face of the wearer, as is illustrated in
Referring to
As is shown in
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The regulator includes a ball valve 76 adjacent to the outlet end of the piercing lance member, including a ball member 80 disposed in the ball valve chamber 82, with a ball valve closing compression spring 84 disposed between the ball member and the outlet end of the piercing lance member and configured to bias the ball member against a ring seal 86 disposed between the ball member and the valve seat 88, to thereby bias the ball valve to be closed, at the upper end of the ball valve chamber. The regulator also includes a gas pressure adjusting assembly 90 mounted in the regulator for regulating the pressure of the gas released from the gas cartridge to a desired lower harness inflation tube pressure. The gas pressure adjusting assembly includes a pressure adjusting screw 92 threadably mounted in the second end 94 of the regulator. A main compression spring 96 is disposed between the pressure adjusting screw and a compression plate member 98, and a pin 100 is disposed between the ball member and the compression plate member to transfer pressure from the pressure adjusting screw through its associated compression spring to bias the ball member open against the valve closing pressure of the ball valve closing compression spring, for controlling gas released from the gas cartridge to a desired lower harness inflation tube pressure, such as approximately 70 psig, for example. The compression of the main spring determines the regulated pressure.
A pressure charge indicator assembly 102 is preferably mounted in an aperture 104 at the side of the regulator and connected with the ball valve chamber, including an indicator poppet or button 106 that pops out when a new cylinder is engaged and stays out until the pressure falls below a threshold pressure, such as approximately 100 psig for example. This indication is used to alert the user that there is a sufficient gas pressure charge in the gas cartridge of the cylinder for at least one more inflation of the inflatable harness left in the cylinder if the poppet is out or up.
The inflation gas supply tube is connected to a gas outlet port 108 of the regulator that is connected in fluid communication with the interior ball valve chamber for supplying pressurized gas to the inflatable harness. As is illustrated in
Referring to
A gas connector tubing 128 is connected to the inflation valve outlet port to conduct the pressurized gas to an outlet fitting connector 130 which is in turn connected to the inflatable tubes of the inflatable harness. A pressure adjusting screw 132 is threadably mounted in the second end 134 of the inflation valve housing. A main compression spring 136 is disposed between the pressure adjusting screw and the base of the inflation valve poppet to bias the inflation valve poppet closed.
Prototype Testing:
A functional unit of the invention was mocked up using a commercially available carbon dioxide, 16-gram inflator for bicycle tires. The unit was connected to the harness supply valve of an existing inflatable harness full-face crew mask. The results shown in the table below were observed after testing three cartridges at an ambient temperature of 70° F. for 10 to 12 inflations average.
From the foregoing, it thus can be seen that the invention uses a compressed gas cylinder mounted on the crew mask and connected to the inflatable harness for supplying pressurized gas to the inflatable harness independent of breathable oxygen supplied to the crew mask. Specifically, the invention uses a small compressed gas cylinder and regulator which are mounted on an aircraft crew member's oxygen mask, thus causing the mask harness to inflate and be donned quickly over one's head. The cylinder provides enough gas for multiple inflations of the harness and allows older military masks which interface to panel mounted regulators to be reconfigured to have the newer preferred inflatable harness. The invention provides economically added and simply constructed means of adapting modern inflatable harness technology to older crew masks, thus avoiding the cost and logistic complexity, particularly for military aircraft, of replacing a large investment in masks and equipment.
It will be apparent from the foregoing that while particular forms of the invention have been illustrated and described, various modifications can be made without departing from the spirit and scope of the invention. Accordingly, it is not intended that the invention be limited, except as by the appended claims.
This application is based upon provisional Application No. 60/899,434, filed February 2007.
Number | Date | Country | |
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60899434 | Feb 2007 | US |