Self-closing valve
11009140 ยท 2021-05-18
Assignee
Inventors
Cpc classification
B64D2201/00
PERFORMING OPERATIONS; TRANSPORTING
F16K31/165
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F16K21/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
F16K21/16
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Embodiments of the present disclosure relate generally to valves that provide controlled inflation. The valves are designed to allow inflation of one or more inflatable devices and to stop inflation once a desired inflation level has been reached. This can allow the valve to be used with a single inflation source in order to inflate a plurality of inflatable devices. In a specific example, this disclosure provides systems and methods for inflating an ejector bag for door-mounted or fuselage-mounted inflatable evacuation slides or slide/rafts used for evacuating passenger vessels, such as aircraft. Other examples relate to sustaining the inflation of individual tubes that communicate with one another in evacuation slides, evacuation slide/rafts, life rafts and/or other inflatable devices.
Claims
1. A method for inflating an ejector bag used to propel an evacuation slide or slide/raft from an aircraft-mounted enclosure, the method comprising: providing an inflator, wherein in use, the inflator inflates both the ejector bag and the evacuation slide or slide/raft; the ejector bag equipped with a self-closing valve comprising: an inlet configured to fluidly communicate with the inflator via a first tubing, a valve closing feature comprising a first end and a second end, a poppet connected to the first end of the valve closing feature, the second end of the valve closing feature configured to be secured to a surface of the ejector bag, wherein upon activation of the inflator, inflation air is delivered to the ejector bag, causing the ejector bag to inflate, which forces the evacuation slide or slide/raft out of the aircraft-mounted enclosure.
2. The method of claim 1, wherein the valve closing feature is positioned internal to the ejector bag and wherein the second end of the valve closing feature is secured to an internal surface of the ejector bag.
3. The method of claim 1, wherein the valve closing feature is positioned external to the ejector bag and wherein the second end of the valve closing feature is secured to an external surface of the ejector bag.
4. The method of claim 1, wherein the valve closing feature comprises a cable, a cord, a line, a rope, a lanyard, a fabric strip, or a webbing.
5. The method of claim 1, wherein the valve closing feature comprises a feature that can be provided in a non-tensioned configuration and that can be tensioned into a tensioned configuration.
6. The method of claim 1, used for sequential inflation of the ejector bag and then the evacuation slide or slide/raft.
7. The method of claim 1, used for concurrent inflation of the ejector bag and the evacuation slide or slide/raft.
8. The method of claim 1, wherein upon inflation of the ejector bag, the valve closing feature is extended to its fullest amount and pulls away from the valve, causing the valve to shut itself off due to expansion of the ejector bag.
9. An inflation system method for inflating an ejector bag used to propel an evacuation slide or slide/raft from an aircraft-mounted enclosure, the method comprising: providing an ejector bag equipped with a self-closing valve comprising: an inlet configured to fluidly communicate with an inflator via a first tubing, a valve closing feature comprising a first end and a second end, a poppet connected to the first end of the valve closing feature, the second end of the valve closing feature configured to be secured to a surface of the ejector bag, providing an evacuation slide or slide/raft comprising a second tubing, wherein the ejector bag and the evacuation slide or slide/raft share the inflator, wherein the ejector bag is in fluid communication with the inflator via the first tubing and wherein the evacuation slide or slide/raft is in fluid communication with the inflator via the second tubing, wherein upon activation of the inflator, inflation air is delivered to the ejector bag, causing the ejector bag to inflate, which forces the evacuation slide or slide/raft out of the aircraft-mounted enclosure.
10. The method of claim 1, wherein the self-closing valve comprises a dry disconnect coupling.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
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DETAILED DESCRIPTION
(16) Embodiments of the present disclosure provide a self-closing valve that may be used in various inflation situations. The valve may also be referred to as self-regulating. In certain examples, the valve may find particular use in connection with inflation of ejector bags. In other examples, the valve may be used in connection with other inflatables, such as life rafts, which are required to have multiple chambers for redundancy and/or for use with ramps designed to be used with inflatable life rafts. For example, if the life raft ramp (or an alternate life raft chamber) is punctured in use, it is desirable to prevent the entire life raft itself from deflating. In other examples, the valve may be used in connection with canopies of life rafts that are intended to be self-erecting, such as canopy support tubes or inflatable arch tubes. Similar to the life raft ramps, puncture of the canopy should not cause the remainder of the life raft to deflate. Some of these systems have used one-way valves that allow air to be delivered for inflation, but that do not allow air to escape the inflatable tube or device through the valve once inflated. The self-closing valve described herein allows airflow into separate chambers. In a specific example, the self-closing valve allows airflow to be delivered from a single inflation source.
(17) Accordingly, although the below description relates to use of the self-closing valve for inflation of an ejector bag and a second inflatable structure, it should be understood that the disclosed self-closing valve may be used in connection with any first inflation structure and any second inflation structure. In use, once the first inflation structure has been inflated to a geometry that causes activation of the valve closing feature, the inlet to the first inflation structure is blocked which causes routing of inflation gas to the second inflation structure. Thus, although the below description describes use of the self-closing valve in connection with inflation of an ejector bag, it should be understood that the above and other uses are possible and considered within the scope of this disclosure.
(18) One advantage of the self-closing valves described herein is that they may use a single inflation source for inflating both inflation structures. As a specific example, the self-closing valves disclosed herein may be used to inflate an ejector bag (used for propelling an evacuation slide or slide/raft from a fuselage-mounted enclosure) using the same high pressure reservoir (inflation system) that inflates the unit (evacuation slide or slide/raft). In other words, the valves do not require a separate inflator system. This eliminates the need for an additional firing mechanism, reservoir, valve assembly or chemical gas generator that is typically used for inflating ejector bags.
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(20) Referring now to the self-closing valve 12 in more detail,
(21) In use, compressed air is injected into valve inlet 26. Once the ejector bag 14 (or other inflatable device that is to be inflated via use of the self-closing valve 12) has been inflated to the desired status, the valve closing feature 24 is extended to its fullest amount. This is illustrated by
(22) In
(23) During inflation, expansion of the inflatable chamber will self-tension the poppet closing cable feature 24. When sufficient tension is applied, the poppet 30 is pulled into the closed position, preventing additional gas from entering into the inflatable chamber. In
(24) In a specific embodiment, the self-closing valve 12 may have a banjo fitting and a poppet with a poppet closing cable. The banjo fitting may be used to allow the valve to swivel or turn with respect to the inflatable structure. Such fittings are well-known and not described further herein.
(25) In another embodiment, the self-closing valve 12 may be used as a dry disconnect coupling 40. Examples are illustrated by
(26) In one example, the dry disconnect coupling 40 is self-regulating in that it allows air to pass through to, but not be released from, the ejector bag 14. The dry disconnect coupling 40 will be connected to the main inflation system 16 through flexible or rigid tubing 18. (This may be the same configuration as shown by
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(28) In an alternate embodiment, the disclosed valve provides a means for sustaining the inflation of individual tubes communicated to each other in evacuation slides, evacuation slide/rafts, life rafts or other inflatable devices using the self-closing valve or dry disconnect valve described herein. Inflatable devices that are made of at least two individual tubes that are communicated to each other can benefit from being inflated from the same inflation source. Federal Aviation Administration (FAA) regulations require that if one tube is compromised (can no longer hold air) the other tube must be able to remain inflated. Accordingly, if each tube is provided with its own self-closing valve or dry disconnect valve, concern that all tubes would deflate if one were to be compromised is significantly lessened. For instance, if each tube were to have a valve (12 or 40) connected to the main inflation system, then the tubes would be filled individually and would not be dependent on each other.
(29) In another specific example, the disclosed valve could prevent buoyancy tubes from deflating on a life raft should a ramp or canopy support tube be punctured. The same could be said of the ramp and the canopy support tube should the buoyancy tubes be punctured; and/or the canopy support tube should the ramp or buoyancy tubes be punctured. The general goal is to provide each inflatable portion of a structure with its own self-closing valve in order to maintain integrity of the remainder of the structure upon damage to one of the inflatable portions.
(30) In another example, use of a self-closing valve could prevent an evacuation slide or slide/raft from deflating if the ramp to the slide is punctured.
(31) An additional embodiment includes a feature implemented on the valve to make it self-locking. This feature would retain the valve in the closed position if it is used on an evacuation slide, evacuation slide/raft, life raft or other inflatable device that has multiple inflated tubes.
(32) In an alternate embodiment, the valve closing feature may incorporate a spring or other automatic push back feature. If provided, the spring could be used to help push the poppet back into an open position. This could be useful in the event of vibration of the aircraft or vehicle during use. Additionally or alternatively, it is possible to provide a detent feature that could maintain the poppet in an open position, such that the poppet is biased in the open position. Alternate embodiments include frangible poppets or poppets that function via one or more magnetic features.
(33) In addition to the ejector bag and multiple tube inflation embodiments disclosed (life rafts, life raft ramps, canopies, canopy support tubes), it may also be possible to use the disclosed self-closing valve for sequencing the inflation of various inflatable components, such as tubes or chambers of a single inflatable component or multiple separate inflatable structures. As illustrated by
(34) In an alternate example illustrated by
(35) In a further example, more than two separate inflatable structures 54 may be inflated using the systems described herein. As illustrated by
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(38) Changes and modifications, additions and deletions may be made to the structures and methods recited above and shown in the drawings without departing from the scope or spirit of the disclosure or the following claims.