The present disclosure relates to aircraft evacuation assemblies, and more specifically to a self-righting life raft.
In the event of an emergency water landing, aircraft typically have one or more life rafts that can be deployed to hold evacuated passengers. Conventional non-reversible rafts may be either deployed in a specific orientation to prevent inflation in an inverted position or may be able to be manually righted after an inverted deployment. While certain conventional life rafts are reversible, meaning they can be deployed and utilized to support evacuated passengers on either side of the life raft, these reversible life rafts often utilize orientation sensing technology and/or they have redundant features, which may add to the complexity and cost of the life raft.
According to various embodiments, the present disclosure provides a life raft that includes a base and an inflatable canopy. The base has a first side and a second side and the inflatable canopy is coupled to the first side of the base and configured to inflate and extend across the first side of the base to form a first chamber defined between the first side of the base and the inflatable canopy, according to various embodiments. The inflatable canopy is configured to inflate in response to deploying the life raft, in accordance with various embodiments.
In various embodiments, the base includes an inflatable border tube defining a first inflatable volume. The inflatable canopy may define a second inflatable volume and the first inflatable volume may be in fluidic communication with the second inflatable volume. In various embodiments, a user access opening is defined between the inflatable border tube and the inflatable canopy. A charge cylinder may be coupled to the inflatable border tube, and the charge cylinder may be positioned offset from the user access opening.
In various embodiments, the inflatable canopy is coupled along and extends from at least 50% of a circumference of the base. In various embodiments, the base has a diameter and the inflatable canopy spans a height in an inflated state, with the height measured between the first side of the base and the inflatable canopy. The height may be substantially equal to the diameter, or the height may be greater than the diameter. In various embodiments, the internal volume of the inflatable canopy in an inflated state is about 10,000 cubic inches. In various embodiments, the inflatable canopy has a dimpled dome shape.
Also disclosed herein, according to various embodiments, is a method of using a life raft. The method may include initializing inflation of the life raft and deploying the life raft in water to self-right life raft. In various embodiments, the life raft self-rights in response to inflation of an inflatable canopy coupled to a first side of a base of the life raft.
The forgoing features and elements may be combined in various combinations without exclusivity, unless expressly indicated herein otherwise. These features and elements as well as the operation of the disclosed embodiments will become more apparent in light of the following description and accompanying drawings.
The subject matter of the present disclosure is particularly pointed out and distinctly claimed in the concluding portion of the specification. A more complete understanding of the present disclosure, however, may best be obtained by referring to the detailed description and claims when considered in connection with the drawing figures, wherein like numerals denote like elements.
The detailed description of exemplary embodiments herein makes reference to the accompanying drawings, which show exemplary embodiments by way of illustration. While these exemplary embodiments are described in sufficient detail to enable those skilled in the art to practice the disclosures, it should be understood that other embodiments may be realized and that logical changes and adaptations in design and construction may be made in accordance with this disclosure and the teachings herein. Thus, the detailed description herein is presented for purposes of illustration only and not of limitation. Throughout the present disclosure, like reference numbers denote like elements. Accordingly, elements with like element numbering may be shown in the figures but may not be necessarily be repeated herein for the sake of clarity.
In the event of an emergency water landing, aircraft typically have one or more life rafts that can be deployed to hold evacuated passengers. In various embodiments, and with reference to
In various embodiments, and with reference to
In various embodiments, the first side 111 of the base 110 of the life raft 100 is a top surface of the life raft 100 upon which passengers are supported in response to the life raft 100 being deployed in water. That is, the base 110 of the life raft 100 may be inflatable, and the base 110 may include one or more inflatable border tubes 114A, 114B. The first and second inflatable border tubes 114A, 114B may provide buoyancy to the life raft 100 and may be mounted one above the other. The first and second inflatable border tubes 114A, 114B may provide a degree of buoyancy redundancy in that each border tube may be independently capable of supporting the weight of the life raft 100 when filled to capacity with passengers. The first inflatable border tube 114A may circumscribe the first side 111 of the base 110 and the second inflatable border tube 114B may circumscribe the second side 112 of the base 110. The base 110 of the life raft 100 may include one or more ladders, handles, etc., that facilitate passengers embarking. The second side 112 of the base 110 of the life raft 100 may be a bottom surface of the life raft 100 that faces the water.
In various embodiments, and with reference to
In various embodiments, and with continued reference to
In various embodiments, and with reference to
In various embodiments, various features of the life raft 100 may contribute to the self-righting ability of the life raft 100. For example, the inflatable canopy 120 may be coupled along and may extend from at least 50% of a circumference of the base 110. That is, from the perspective a passenger sifting in the center of the life raft 100, at least 180 degrees of the passenger's view is obstructed by the inflatable canopy 120. In various embodiments, the inflatable canopy 120 is coupled along and extends from at least 70% of the circumference of the base 110. This extent of coverage of the inflatable canopy 120 over the base 110 helps to enable the self-righting performance of the life raft 100, according to various embodiments.
In various embodiments, and with renewed reference to
The base 110 of the life raft 100, according to various embodiments, may have a diameter 118 of about 50 inches (127 centimeters), with the internal volume of the inflatable canopy being about 10,000 cubic inches (160 liters). As used in this context only, the term “about” refers to plus or minus 5% of the stated value. In various embodiments, the internal volume of the inflatable canopy 120 is between about 50% and about 100% of the internal volume of the base 110.
In various embodiments, the position of the charge cylinder 140 is offset from the location of the user access opening 122. For example, the charge cylinder 140 may be offset about 90 degrees from the user access opening 122. In various embodiments, the charge cylinder 140 is positioned opposite the user access opening 122. In various embodiments, and with reference to
In various embodiments, and with reference to
Benefits, other advantages, and solutions to problems have been described herein with regard to specific embodiments. Furthermore, the connecting lines shown in the various figures contained herein are intended to represent exemplary functional relationships and/or physical couplings between the various elements. It should be noted that many alternative or additional functional relationships or physical connections may be present in a practical system. However, the benefits, advantages, solutions to problems, and any elements that may cause any benefit, advantage, or solution to occur or become more pronounced are not to be construed as critical, required, or essential features or elements of the disclosure.
The scope of the disclosure is accordingly to be limited by nothing other than the appended claims, in which reference to an element in the singular is not intended to mean “one and only one” unless explicitly so stated, but rather “one or more.” It is to be understood that unless specifically stated otherwise, references to “a,” “an,” and/or “the” may include one or more than one and that reference to an item in the singular may also include the item in the plural. All ranges and ratio limits disclosed herein may be combined.
Moreover, where a phrase similar to “at least one of A, B, and C” is used in the claims, it is intended that the phrase be interpreted to mean that A alone may be present in an embodiment, B alone may be present in an embodiment, C alone may be present in an embodiment, or that any combination of the elements A, B and C may be present in a single embodiment; for example, A and B, A and C, B and C, or A and B and C. Different cross-hatching is used throughout the figures to denote different parts but not necessarily to denote the same or different materials.
The steps recited in any of the method or process descriptions may be executed in any order and are not necessarily limited to the order presented. Furthermore, any reference to singular includes plural embodiments, and any reference to more than one component or step may include a singular embodiment or step. Elements and steps in the figures are illustrated for simplicity and clarity and have not necessarily been rendered according to any particular sequence. For example, steps that may be performed concurrently or in different order are illustrated in the figures to help to improve understanding of embodiments of the present disclosure.
Any reference to attached, fixed, connected or the like may include permanent, removable, temporary, partial, full and/or any other possible attachment option. Additionally, any reference to without contact (or similar phrases) may also include reduced contact or minimal contact. Surface shading lines may be used throughout the figures to denote different parts or areas but not necessarily to denote the same or different materials. In some cases, reference coordinates may be specific to each figure.
Systems, methods and apparatus are provided herein. In the detailed description herein, references to “one embodiment”, “an embodiment”, “various embodiments”, etc., indicate that the embodiment described may include a particular feature, structure, or characteristic, but every embodiment may not necessarily include the particular feature, structure, or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment. Further, when a particular feature, structure, or characteristic is described in connection with an embodiment, it is submitted that it is within the knowledge of one skilled in the art to affect such feature, structure, or characteristic in connection with other embodiments whether or not explicitly described. After reading the description, it will be apparent to one skilled in the relevant art(s) how to implement the disclosure in alternative embodiments.
Furthermore, no element, component, or method step in the present disclosure is intended to be dedicated to the public regardless of whether the element, component, or method step is explicitly recited in the claims. No claim element is intended to invoke 35 U.S.C. 112(f) unless the element is expressly recited using the phrase “means for.” As used herein, the terms “comprises”, “comprising”, or any other variation thereof, are intended to cover a non-exclusive inclusion, such that a process, method, article, or apparatus that comprises a list of elements does not include only those elements but may include other elements not expressly listed or inherent to such process, method, article, or apparatus.
Number | Name | Date | Kind |
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3883913 | Givens | May 1975 | A |
4998900 | Wright | Mar 1991 | A |
5579609 | Sallee | Dec 1996 | A |
5733158 | Higginbotham | Mar 1998 | A |
5800225 | Shoaff, III | Sep 1998 | A |
Number | Date | Country |
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673417 | Jun 1954 | GB |
2005017291 | Feb 2005 | WO |
Number | Date | Country | |
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20190248456 A1 | Aug 2019 | US |