Patent Grant
10046851
The present disclosure relates to landing gear systems and, more specifically, to a noise abating device for use with an articulating landing gear.
Aircraft noise generated during approach is a growing concern at airports. Noise restrictions have a significant influence on the availability of flight times and allowed aircraft types. Due to significant advances in engine technology, airframe noise is becoming relatively more significant as a source of noise. Typical articulating or trailing arm type landing gear systems incorporate a forward main post and a trailing arm attached via a joint. A shock strut may extend between these two members so that the trailing arm may articulate upward or downward. Typically, the joint is a forked clevis at the lower end of the main post, mating to the trailing arm. During deployment, prior to landing and/or after takeoff, air rushes through an open space within the forked clevis, causing noise and harsh tones at frequencies audible to the human ear. Thus, there remains a need for landing gear noise abatement systems.
A noise abatement system may comprise a retention member and a covering member.
In various embodiments, a retention member may comprise a post adapted to interface with the landing gear by friction fitting or a fastening apparatus adapted to interface with the landing gear by fasteners.
In various embodiments, a covering member may comprise a void covering portion which extends substantially across a void in the landing gear, and optionally, a landing gear covering portion which extends beyond one or more of the edges of the void.
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 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 and their best mode. While these exemplary embodiments are described in sufficient detail to enable those skilled in the art to practice the inventions, it should be understood that other embodiments may be realized and that logical, chemical and mechanical changes may be made without departing from the spirit and scope of the disclosure. Thus, the detailed description herein is presented for purposes of illustration only and not of limitation. For example, 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. Also, 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. As used herein, phrases such as “make contact with,” “coupled to,” “touch,” “interface with” and “engage” may be used interchangeably.
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In various embodiments, covering member 302 may extend substantially over void 108 in the landing gear and/or may occupy a cross-sectional area bounded in the X-axis by the forked clevis at the lower end of the main post 102 and in the Y-axis by the main post 102 and the trailing arm 104. However, covering member 302 may be positioned in any configuration adapted to ameliorate aerodynamic noise by diverting air flow from the void 108. In various embodiments, covering member 302 extends in a plane substantially normal to the direction of air flow. In various embodiments, a covering member comprises a void covering portion which extends substantially over a void in the landing gear or may occupy a cross-sectional area bounded in the X-axis by the forked clevis at the lower end of the main post 102 and in the Y-axis by the main post 102 and the trailing arm 104. In various exemplary embodiments of noise abatement systems, a covering member includes a void covering portion and other covering portions, which extend beyond one or more of the edges of the void, for example, forward main post covering portions, trailing arm covering portions, side flange covering portions, and fastening side flange covering portions as illustrated with respect to the various exemplary embodiments of noise abatement systems of
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Furthermore, fastening slide flange portions 1004 may also serve as a retention member and may have a fastening apparatus 1008 by which noise abatement system 1000 may be held, maintained, or otherwise coupled or retained in mechanical communication with forward main post 102. In various embodiments, fastening side flange covering portions 1004 are bent, for example, to follow a profile of the forward main post 102, wherein a 90 degree bend causes fastening apparatus 1008 of at least one fastening side flange covering portion 1004 to be positioned generally against a face of forward main post 102 substantially normal to a plane of void covering portion 1002.
A noise abatement system 300 may comprise two fastening side flange covering portions 1004. Alternatively, a noise abatement system 300 may comprise one fastening side flange covering portion 1004, or three fastening side flange covering portions 1004, or four fastening side flange covering portions 1004 or any number or configuration of fastening side flange covering portions 1004 adapted to hold, maintain, or otherwise couple or retain system 300 in mechanical communication with forward main post 102.
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Now, having described various components of various exemplary noise abatement systems, a noise abatement system may be manufactured from various materials. In one exemplary embodiment, a noise abatement system may comprise plastic. Alternatively, a noise abatement system may comprise metal, such as titanium, aluminum or stainless steel, though it may alternatively comprise numerous other materials configured to provide support, such as, for example, composite, ceramic, a para-aramid fiber material such as a para-aramid fiber composite material, for example, a KEVLAR® brand material available from E. I. du Pont de Nemours and Company, ultra high molecular weight polyethylene such as an ultra-high molecular weight polyethylene composite material, for example, a DYNEEMA® brand material available from Royal DSM, an aramid fiber material such as an aramid fiber composite material, alloy, glass, binder, epoxy, polyester, acrylic, or any material or combination of materials having a desired strength, stiffness, or flexibility sufficient to maintain resiliency during use. In various embodiments, various portions of noise abatement systems as disclosed herein are made of different materials or combinations of materials, and/or may comprise coatings. For example, a retention member may be coated with a frictional material and covering member may be coated with an aerodynamic material. In various embodiments, the retention member is manufactured separately from the covering member.
In various embodiments, noise abatement systems may comprise multiple materials, or any material configuration suitable to enhance or reinforce the resiliency and/or support of the system when subjected to wear in an aircraft operating environment or to satisfy other desired electromagnetic, chemical, physical, or biological properties. Furthermore, noise abatement systems may comprise materials with grain structures or with no grain structures. Noise abatement systems may comprise materials with similar grain structures, or with differing grain structures or grain direction or with similar grain structures or grain direction or any grain structure or direction suitable for achieving desired properties in the system; for example, resiliency under aerodynamic loads and temperature changes.
In various embodiments, while the noise abatement systems described herein have been described in the context of aircraft applications; however, one will appreciate in light of the present disclosure, that the system described herein may be used in connection with various other vehicles, for example, cars, trucks, busses, trains, boats, and submersible vehicles, or any other vehicle or device, having a void through which gas or fluid may flow, creating, for instance, noise or drag.
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 inventions. The scope of the inventions 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.” Moreover, where a phrase similar to “at least one of A, B, or 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.
Systems, methods and apparatus are provided herein. In the detailed description herein, references to “various embodiments”, “one embodiment”, “an embodiment”, “an example embodiment”, 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 herein is to be construed under the provisions of 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.
This application is a divisional of U.S. Ser. No. 14/048,914, filed Oct. 8, 2013, now U.S. Pat. No. 9,796,467, entitled “LANDING GEAR NOISE ABATEMENT DEVICES,” which is hereby incorporated by reference in its entirety.
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| Number | Date | Country | |
|---|---|---|---|
| Parent | 14048914 | Oct 2013 | US |
| Child | 15706033 | US |
