Nacelle core with insert
09752595 ยท 2017-09-05
Assignee
Inventors
- Jose S. Alonso-Miralles (Chula Vista, CA, US)
- Charles M. Biset (San Diego, CA, US)
- Christian Soria (La Mesa, CA, US)
Cpc classification
F04D29/522
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F05B2250/283
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
B64D2033/0206
PERFORMING OPERATIONS; TRANSPORTING
F05B2260/96
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
International classification
B64D29/00
PERFORMING OPERATIONS; TRANSPORTING
F04D29/32
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
F04D29/52
MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
Abstract
Aspects of the disclosure are directed to a structure comprising: a plurality of cells, a first non-permeable insert in a first cell of the plurality of cells, the first insert configured to constrict, by at least a first threshold amount, a flow of fluid in the first cell such that: acoustic power over a frequency range is attenuated by the structure by at least a second threshold amount, and a resonant frequency associated with the structure is shifted by at least a third threshold amount.
Claims
1. A structure comprising: a plurality of cells; a non-permeable first insert in a first cell of the plurality of cells, the first insert configured to constrict, by at least a first threshold amount, a flow of fluid in the first cell such that: acoustic power over a frequency range is attenuated by the structure by at least a second threshold amount, and a resonant frequency associated with the structure is shifted by at least a third threshold amount; wherein a surface of the first insert forms a hole that extends along an axis through the first insert, and a sectional geometry of the surface as viewed in a plane parallel to the axis is substantially round.
2. The structure of claim 1, wherein the first threshold amount is 90%.
3. The structure of claim 1, wherein the frequency range corresponds to 0-10 KHz.
4. The structure of claim 1, further comprising a non-permeable second insert, wherein the first insert is located at a first distance as measured from a bottom of the first cell, and wherein the second insert is located at a second distance as measured from the bottom of the first cell.
5. The structure of claim 4, wherein the first distance and the second distance are different.
6. The structure of claim 1, further comprising a non-permeable second insert, wherein the second insert is located in the first cell.
7. The structure of claim 1, further comprising a non-permeable second insert, wherein the second insert is located in a second cell of the plurality of cells.
8. The structure of claim 1, wherein each of the plurality of cells has a substantially hexagonal shape, and wherein the cells are arranged relative to one another to form a honeycomb profile.
9. The structure of claim 8, wherein outer edges of the first insert adhere to the shape of the first cell.
10. The structure of claim 1, wherein the frequency range and the second threshold amount are based on at least one of: a count of inserts within at least one of the cells, a location of the first insert within the first cell, a size of the first insert, a size of a hole defined by the first insert, a shape of the first insert, or a shape of the first cell.
11. The structure of claim 1, wherein the structure is configured to be incorporated in a nacelle of an aircraft.
12. The structure of claim 11, wherein the structure is configured to be incorporated in at least one of a translating sleeve or a blocker door.
13. The structure of claim 11, wherein at least one of the frequency range or the second threshold amount is based on a size of a fan housed within the nacelle.
14. The structure of claim 1, wherein the frequency range corresponds to 0-1 KHz.
15. The structure of claim 1, wherein the sectional geometry of the surface as viewed in the plane parallel to the axis is semi-circular.
16. A structure comprising: a plurality of cells; a non-permeable first insert in a first cell of the plurality of cells, the first insert configured to constrict, by at least a first threshold amount, a flow of fluid in the first cell such that: acoustic power over a frequency range is attenuated by the structure b at least a second threshold amount, and a resonant frequency associated with the structure is shifted by at least a third threshold amount; a non-permeable second insert in a second cell of the plurality of cells; and a non-permeable third insert in the second cell of the plurality of cells; wherein the first insert is substantially located at a center of the first cell, the second insert is substantially located at a top of the second cell, and the third insert is substantially located at a bottom of the second cell.
17. The structure of claim 16, wherein the first insert is a first distance from a bottom of the first cell, the second insert is a second distance from the bottom of the second cell, the third insert is a third distance from the bottom of the second cell, and the first distance is less than the second distance and greater than the third distance.
18. A structure, comprising: a plurality of cells comprising a first cell; and a non-permeable first insert arranged in the first cell, the first insert configured to constrict, by at least a first threshold amount, a flow of fluid in the first cell such that: acoustic power over a frequency range is attenuated by the structure by at least a second threshold amount, and a resonant frequency associated with the structure is shifted by at least a third threshold amount; wherein an aperture extends along a centerline through the first insert, the aperture is partially formed by an annular edge portion of the first insert, and the annular edge portion comprises a curved bevel.
19. The structure of claim 18, wherein the aperture is further partially formed by a second annular edge portion of the first insert, and the second annular edge portion comprises a curved bevel.
Description
BRIEF DESCRIPTION OF THE DRAWINGS
(1) The present disclosure is illustrated by way of example and not limited in the accompanying figures in which like reference numerals indicate similar elements.
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DETAILED DESCRIPTION
(11) It is noted that various connections are set forth between elements in the following description and in the drawings (the contents of which are included in this disclosure by way of reference). It is noted that these connections are general and, unless specified otherwise, may be direct or indirect and that this specification is not intended to be limiting in this respect. A coupling between two or more entities may refer to a direct connection or an indirect connection. An indirect connection may incorporate one or more intervening entities.
(12) In accordance with various aspects of the disclosure, apparatuses, systems and methods are described for providing a shift in the frequency profile (in an amount greater than a threshold) of one or more cells that are used as part of an acoustic structure of a nacelle of an aircraft. In some embodiments, this shift may be obtained by a constriction insert in the fluid path of the cells and without changing (e.g., increasing) the depth of the cells. In this manner, flexibility may be provided in terms of an acoustic bond panel design procedure to target specific requirements while still adhering to overall nacelle packaging requirements. An insert may be non-permeable.
(13) Referring to
(14) Referring to
(15) As shown in
(16) Referring to
(17) There may be a constriction insert 312 located within the span/thickness T of the cells 306 (in
(18) The outer edges of an insert 312 in proximity to the walls of a cell 306 may be similar in shape to the outer edges 224 of the insert 212 described above in connection with
(19) Referring to
(20) The inserts 212, 312, and 812 are illustrative. One skilled in the art will appreciate based on a review of this disclosure that other shapes/form-factors for an insert that creates an effective constriction channel for the fluid path may be used.
(21) Referring to
(22) Referring to
(23) Referring to
(24) Referring to
(25) Referring to
(26) In
(27) In
(28) The embodiment of
(29) In
(30) The embodiment of
(31) In
(32) While the examples described above in connection with
(33) In accordance with aspects of this disclosure, an insert may be used to constrict a flow/movement of fluid (ex., air) with a cell. In some embodiments, the insert may provide for a threshold amount of constriction. For example, in some embodiments, the insert may provide for at least 90% constriction.
(34) The use of a constriction insert may be analogized to a lumped-element model. For example,
(35) Continuing with the analogy, the effective modal mass near a velocity maximum is a function of the acceleration of the fluid in that vicinity. The addition of a constriction insert in this sector increases the local velocity due to the restricted flow area and consequently will behave as a system with increased inertia (mass). Although the flow restriction might seem like a reduction in the mass (reduced air volume), the acceleration effects of the change in cross sectional area produce the effective mass to increase. As an illustration focusing the 1.sup.st cavity resonance condition 1002, the addition of a constriction insert close to the top of the cell effectively adds an incremental mass m.sub.2 relative to a baseline mass m.sub.1. The frequency of oscillation w.sub.n associated with a spring s having a spring constant k and loaded with the masses m.sub.1 and m.sub.2 may be expressed as:
w.sub.n=square root[k/(m.sub.1+m.sub.2)]
(36) In the above expression, given that the summation of the masses m.sub.1 and m.sub.2 appears in the denominator of the argument of the square root operation or function, the incremental mass m.sub.2 represented by the addition of the constriction insert to the cell has a tendency to reduce the frequency w.sub.n. Stated somewhat differently, the addition of a constriction insert provides for opportunities to modify acoustic behavior/output at a lower end of a frequency range, without necessarily increasing the acoustic panel thickness. Although the illustration above is focused on the 1.sup.st cavity resonance condition 1002, one skilled in the art would draw similar conclusions for the conditions 1024 and 1048 provided the constriction is placed at other locations in the cell, e.g. near a velocity maximum for the corresponding condition 1024 or 1048.
(37) The insert may be used to modify/tailor a tonal acoustic profile of a structure/core to adhere to one or more specifications/requirements. For example, the constriction provided by the insert may be adjusted/selected to provide for such a profile. In turn, the constriction that is obtained may he based on one or more parameters. Such parameters may include, for example:
(38) (1) a count of inserts within a cell,
(39) (2) a location of an insert within a cell (e.g., a distance of the insert relative to a reference location [e.g., top or bottom] of the cell),
(40) (3) a size of an insert (e.g., in terms of the thickness t of the insert [potentially relative to a thickness T of a cell] or a size [e.g., radius or diameter] of a (center) hole defined by the insert [potentially relative to a dimension of a cell]),
(41) (4) a shape/profile/geometry of an insert and/or a cell,
(42) In some embodiments, an insert may be manufactured with a cell as a common, monolithic piece. In some embodiments, the insert may be manufactured separately from the cell and then joined to the cell using one or more techniques (e.g., bonding, application of an adhesive, brazing, welding, etc.). An insert may be made of the same material as a cell. An insert may be made of one or more materials that are not used in the manufacture of a cell.
(43) Technical effects and benefits of this disclosure include an ability to tailor/customize an acoustic/tonal profile associated with a core/structure by incorporating one or more inserts within one or more cells. In some embodiments, attenuation (in an amount greater than a threshold) of acoustic power (e.g., noise) at low frequencies (e.g., over a frequency range of 0-10 KHz, a subset of frequencies over the range 0-10 KHz, frequencies that are less than 1 KHz, or as potentially based on a size of a fan housed within a nacelle) may be obtained without incurring the penalty/expense of having to increase core thickness/depth. Aspects of the disclosure may be used to select or shift the resonant behavior/frequency of one or more cells (e.g., a hexcore cell) or a structure associated with the cell(s).
(44) Aspects of the disclosure have been described in terms of illustrative embodiments thereof. Numerous other embodiments, modifications, and variations within the scope and spirit of the appended claims will occur to persons of ordinary skill in the art from a review of this disclosure. For example, one of ordinary skill in the art will appreciate that the steps described in conjunction with the illustrative figures may he performed in other than the recited order, and that one or more steps illustrated may be optional in accordance with aspects of the disclosure. One or more features described in connection with a first embodiment may be combined with one or more features of one or more additional embodiments.