JP2019138977A - Resonance type sound absorption panel - Google Patents

Resonance type sound absorption panel Download PDF

Info

Publication number
JP2019138977A
JP2019138977A JP2018020323A JP2018020323A JP2019138977A JP 2019138977 A JP2019138977 A JP 2019138977A JP 2018020323 A JP2018020323 A JP 2018020323A JP 2018020323 A JP2018020323 A JP 2018020323A JP 2019138977 A JP2019138977 A JP 2019138977A
Authority
JP
Japan
Prior art keywords
hole
sound absorbing
protrusion
absorbing panel
resonance type
Prior art date
Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
Granted
Application number
JP2018020323A
Other languages
Japanese (ja)
Other versions
JP7064236B2 (en
Inventor
俊治 榎本
Shunji Enomoto
俊治 榎本
石井 達哉
Tatsuya Ishii
達哉 石井
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Japan Aerospace Exploration Agency JAXA
Original Assignee
Japan Aerospace Exploration Agency JAXA
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Japan Aerospace Exploration Agency JAXA filed Critical Japan Aerospace Exploration Agency JAXA
Priority to JP2018020323A priority Critical patent/JP7064236B2/en
Publication of JP2019138977A publication Critical patent/JP2019138977A/en
Application granted granted Critical
Publication of JP7064236B2 publication Critical patent/JP7064236B2/en
Active legal-status Critical Current
Anticipated expiration legal-status Critical

Links

Landscapes

  • Soundproofing, Sound Blocking, And Sound Damping (AREA)
  • Devices Affording Protection Of Roads Or Walls For Sound Insulation (AREA)
  • Building Environments (AREA)
  • Panels For Use In Building Construction (AREA)
  • Exhaust Silencers (AREA)

Abstract

To provide a resonance type sound absorption panel which improves sound absorption performance with a simple shape change as much as possible, does not remarkably increase weight due to the shape change and can be easily applied to an existing sound absorption panel.SOLUTION: A resonance type sound absorption panel 1 comprises: a cell structure which is constituted from partitions 12 for partitioning cells 11 and a surface plate 20 where through holes 21 are formed and a back wall 30, which are arranged on upper and lower portions of the partitioned cells 11; and protrusions protruding in a center axis direction of the through holes 21 from a wall side of at least one of a surface side end and a back side end of the through holes 21 and having protrusion length which is 20% or less of diameters of the through holes 21.SELECTED DRAWING: Figure 1

Description

本発明は、自動車、航空機、船舶用エンジンの騒音低減(騒音伝播経路での減音)や建築物、公共設備、自動車用道路、鉄道施設の騒音低減(騒音伝播経路での遮音)、車両、自動車、航空機などの車内、客室内の騒音低減(閉空間の減音)、精密機器を収納するフェアリング内部の騒音振動軽減(閉空間の減音)等に用いられる共鳴型吸音パネルに関する。   The present invention relates to noise reduction (noise reduction in noise propagation path) for automobiles, aircraft and marine engines, noise reduction in buildings, public facilities, automobile roads, railway facilities (sound insulation in noise propagation path), vehicles, The present invention relates to a resonance type sound absorbing panel used for reducing noise in a vehicle such as an automobile and an aircraft, reducing noise in a cabin (sound reduction in a closed space), and reducing noise vibration in a fairing that houses precision equipment (sound reduction in a closed space).

共鳴型吸音パネルは、一般的には、セル構造のパネルの表裏に表面板及び背後壁を貼り、セルを区画する隔壁に囲まれた各小空間に通じる貫通孔を表面板に設けてなる。   In general, a resonance type sound absorbing panel is formed by attaching a surface plate and a back wall on the front and back of a panel having a cell structure, and providing a through hole in the surface plate that leads to each small space surrounded by partition walls partitioning the cells.

共鳴型吸音パネルに関連する技術は従来からいくつか提案されてきた。   Several techniques related to the resonance type sound absorbing panel have been proposed.

特許文献1は、孔部をセル内部に伸長させた吸音構造を有しており、共鳴周波数を低周波数側にシフトすることを提案する。これは、吸音率を極大とする周波数を低周波数にシフトさせることはできるが、積極的に吸音率を増加させることには繋がらない。   Patent Document 1 has a sound absorbing structure in which a hole is extended inside a cell, and proposes to shift the resonance frequency to a lower frequency side. This can shift the frequency at which the sound absorption rate is maximized to a low frequency, but does not lead to positively increasing the sound absorption rate.

特許文献2は、セル内部に中間連通孔を介して別のセルを設けたものであり、いわゆるダブルレイヤ共鳴型吸音パネルの第2層のセルを第1層のセル間に配置した格好となっているものと考えられる。そうであるなら、単位ユニットの吸音効果はダブルレイヤの吸音パネルと等価である反面、第1層のセル面積が相対的に減少する〜同一面積をダブルレイヤ吸音パネルで充填した場合に対して吸音性能が低下する、と推察される。   In Patent Document 2, another cell is provided inside the cell via an intermediate communication hole, and the second layer cell of the so-called double layer resonance type sound absorbing panel is arranged between the first layer cells. It is thought that. If so, the sound absorption effect of the unit unit is equivalent to the double layer sound absorption panel, but the cell area of the first layer is relatively reduced. It is inferred that the performance will decrease.

特許文献3は、二次元スリット状の孔部を有する吸音パネルを形成する。長方形状の吸音構造体に複雑なセル形状、孔形状をはめ込んで、共鳴周波数を調整するものとみられる。   Patent Document 3 forms a sound absorbing panel having a two-dimensional slit-shaped hole. It seems that the resonance frequency is adjusted by fitting a complicated cell shape and hole shape into the rectangular sound absorbing structure.

特開2013−8012号公報JP2013-8012A 特開2001−92468号公報JP 2001-92468 A 特開平9−3833号公報Japanese Patent Laid-Open No. 9-3833

これらの従来の技術は、吸音パネルの共鳴周波数に着目して、孔長さ、セル形状を調整するものであって、吸音量の増加という課題を積極的に示唆するものではない。   These conventional techniques adjust the hole length and cell shape by paying attention to the resonance frequency of the sound absorbing panel, and do not actively suggest the problem of increasing the sound absorption volume.

また、吸音パネルに入射する音の振幅に応じた検討がなされていない。しかし、様々な要件で吸音パネルを適用する場合には、既存の吸音パネルに対して大幅な形状変更なく吸音性能を高めることが求められる。例えば、ダクト内壁に用いる場合には、吸音パネル表面に気流が存在するために、パネル形状の大幅な変更は、ダクト内の圧力損失となって現れ、音響面以外の設計要件に影響を与える。   Moreover, examination according to the amplitude of the sound incident on the sound absorbing panel has not been made. However, when the sound absorbing panel is applied with various requirements, it is required to improve the sound absorbing performance without a significant shape change with respect to the existing sound absorbing panel. For example, when it is used for the inner wall of a duct, since there is an air flow on the surface of the sound absorbing panel, a large change in the panel shape appears as a pressure loss in the duct and affects design requirements other than the acoustic surface.

更に、例えば貫通孔を伸長する部材を付加すると、吸音パネルの重量増加にも繋がるため、軽量性を要求される航空機用エンジンなどでは不利となる。   Furthermore, for example, adding a member that extends the through hole leads to an increase in the weight of the sound absorbing panel, which is disadvantageous in an aircraft engine or the like that requires light weight.

なお、特許文献3で示唆される屈曲した孔部形状は二次元スリットではよいものの、三次元的な孔形状では実現困難か製造コストの増大が見込まれる。   Although the bent hole shape suggested in Patent Document 3 may be a two-dimensional slit, it is difficult to realize a three-dimensional hole shape or an increase in manufacturing cost is expected.

以上のような事情に鑑み、本発明の目的は、できる限り簡易な形状変更をもって、吸音性能を高め、形状変更による大幅な重量増加をすることがなく、しかも既存の吸音パネルへの適用も容易にできる共鳴型吸音パネルを提供することにある。   In view of the circumstances as described above, the object of the present invention is to improve the sound absorption performance by changing the shape as simple as possible, without significantly increasing the weight due to the shape change, and easily applied to existing sound absorption panels. An object of the present invention is to provide a resonance type sound absorbing panel that can be used.

上記目的を達成するため、本発明の一形態に係る共鳴型吸音パネルは、セルを区画する隔壁と、前記区画されたセルの上下に設けられ、少なくとも一方に貫通孔が設けられた表面板及び背後壁とから構成されるセル構造と、前記貫通孔の表面側端部及び裏面側端部の少なくとも一方の壁側より前記貫通孔の中心軸方向に突出し、前記貫通孔の直径の20%以下の突出長の突出部とを具備する。   In order to achieve the above object, a resonance type sound absorbing panel according to an embodiment of the present invention includes a partition wall that divides a cell, a surface plate that is provided above and below the partitioned cell, and at least one of which has a through-hole. A cell structure composed of a back wall and at least one wall side of the front-side end and the back-side end of the through-hole project in the direction of the central axis of the through-hole, and 20% or less of the diameter of the through-hole And a protruding portion having a protruding length.

本発明では、上記構成の突出部を設けることで、吸音性能を高めことができる。また、単に突出部を設けるだけの構成なので、簡易な形状変更でよく、形状変更による大幅な重量増加をすることがなく、しかも既存の吸音パネルへの適用も容易にできる。   In the present invention, the sound absorbing performance can be enhanced by providing the protruding portion having the above-described configuration. Further, since the structure is simply provided with the protruding portion, it is possible to change the shape easily, without significantly increasing the weight due to the shape change, and to easily apply to the existing sound absorbing panel.

本発明に係る突出部は下記のとおり様々形態で実現できる。   The protrusion part based on this invention is realizable with various forms as follows.

本発明の一形態に係る共鳴型吸音パネルは、前記突出部が、前記壁側より前記貫通孔の中心軸方向に円環状に突出してもよい。   In the resonance type sound absorbing panel according to an aspect of the present invention, the protruding portion may protrude in an annular shape from the wall side toward the central axis of the through hole.

本発明は、突出部が貫通孔の軸周りに一様ではなく、周期的あるいは非周期的に存在するものであってもよい。すなわち、本発明の一形態に係る共鳴型吸音パネルは、前記突出部を、前記貫通孔の径方向に沿って間隔をもって配置され、前記壁側より前記貫通孔の中心軸方向に突出する複数の突出部材から構成してもよい。   In the present invention, the protrusions may not be uniform around the axis of the through hole, but may exist periodically or aperiodically. That is, in the resonance type sound absorbing panel according to an aspect of the present invention, the protruding portions are arranged at intervals along the radial direction of the through hole, and are protruded from the wall side toward the central axis of the through hole. You may comprise from a protrusion member.

本発明は、突出部が先端に向かって(貫通孔の中心軸に向かって)薄くなっているか、先端が鋭角となっていても、或いは先端に向かって貫通孔の外側(空気層側)又は貫通孔の内側に反っている形状でもよい。すなわち、本発明の一形態に係る共鳴型吸音パネルは、前記突出部が、前記壁側より前記貫通孔の中心軸方向になるに従い薄くてもよい。本発明の一形態に係る共鳴型吸音パネルは、前記突出部が、前記貫通孔の軸方向のいずれか一方の方向に反りを有してもよい。   In the present invention, the protrusion is thin toward the tip (toward the central axis of the through hole), the tip has an acute angle, or the outside of the through hole (air layer side) or toward the tip. The shape may be warped inside the through hole. That is, in the resonance type sound absorbing panel according to an aspect of the present invention, the protruding portion may be thinner as it goes from the wall side toward the central axis of the through hole. In the resonance type sound absorbing panel according to an aspect of the present invention, the protruding portion may have a warp in any one of the axial directions of the through hole.

本発明は、突出部の外周と貫通孔の内面とが、多角形で接合するもの、或いは滑らかに接合するものであってもよい。すなわち、本発明の一形態に係る共鳴型吸音パネルは、前記突出部が、前記貫通孔内側の面が多角形状又はR形状であってもよい。   In the present invention, the outer periphery of the protruding portion and the inner surface of the through hole may be joined in a polygonal shape or smoothly joined. That is, in the resonance type sound absorbing panel according to an aspect of the present invention, the protruding portion may have a polygonal shape or an R shape on the inner surface of the through hole.

本発明の一形態に係る共鳴型吸音パネルは、前記突出部を有する円環部材を有し、前記表面板又は背後壁の前記貫通孔の周囲に座刳りを設け、前記座刳りに前記円環部材を嵌め込んでもよい。   A resonance type sound absorbing panel according to an aspect of the present invention includes an annular member having the protruding portion, and a countersink is provided around the through hole in the surface plate or the back wall, and the ring is formed on the countersink. A member may be fitted.

本発明の一形態に係る共鳴型吸音パネルは、前記突出部を有する円筒部材を有し、前記貫通孔に前記円筒部材を嵌め込んでもよい。   The resonance type sound absorbing panel according to an aspect of the present invention may include a cylindrical member having the protruding portion, and the cylindrical member may be fitted into the through hole.

本発明の一形態に係る共鳴型吸音パネルは、前記貫通孔より穴径の小さい孔が空けられた薄いシート状の部材を有し、前記貫通孔内に前記小さい孔が位置するように、前記表面板又は背後壁の表面に前記シート状の部材を張り付けて、前記貫通孔内に前記シート状の部材が張り出すようにして前記突出部を構成してもよい。   The resonance type sound absorbing panel according to an aspect of the present invention includes a thin sheet-like member having a hole having a smaller diameter than the through hole, and the small hole is positioned in the through hole. The protrusion may be configured such that the sheet-like member is attached to the surface of the surface plate or the back wall, and the sheet-like member protrudes into the through hole.

本発明の一形態に係る共鳴型吸音パネルは、前記突出部の厚さが、前記貫通孔の孔長の5%以下であってもよい。   In the resonance type sound absorbing panel according to an aspect of the present invention, the thickness of the protruding portion may be 5% or less of the hole length of the through hole.

本発明により、できる限り簡易な形状変更をもって、吸音性能を高め、形状変更による大幅な重量増加をすることがなく、しかも既存の吸音パネルへの適用も容易にできる。   According to the present invention, it is possible to improve the sound absorption performance by changing the shape as simple as possible, without increasing the weight significantly by changing the shape, and to be easily applied to an existing sound absorption panel.

本発明の一実施形態に係る共鳴型吸音パネルの分解斜視図である。It is a disassembled perspective view of the resonance type sound absorption panel which concerns on one Embodiment of this invention. 図1に示した共鳴型吸音パネルの一部断面図である。FIG. 2 is a partial cross-sectional view of the resonance type sound absorbing panel shown in FIG. 1. 図1及び図2に示した共鳴型吸音パネルの貫通孔付近の拡大断面図である。It is an expanded sectional view of the through-hole vicinity of the resonance type sound absorption panel shown in FIG.1 and FIG.2. 図1及び図2に示した共鳴型吸音パネルの貫通孔付近の平面図である。FIG. 3 is a plan view of the vicinity of a through hole of the resonance type sound absorbing panel shown in FIGS. 1 and 2. 本発明の他の実施形態に係る突出部であって、突出部が次第に薄くなるように構成された場合を示す断面図である。FIG. 10 is a cross-sectional view showing a protrusion according to another embodiment of the present invention, wherein the protrusion is configured to become gradually thinner. 本発明の他の実施形態に係る突出部であって、突出部の先端が鋭角となるように構成された場合を示す断面図である。FIG. 10 is a cross-sectional view illustrating a case where the protrusion is configured to have an acute angle at the tip of the protrusion according to another embodiment of the present invention. 本発明の他の実施形態に係る突出部であって、突出部が外側に反りを有する場合の断面図である。It is a protrusion part which concerns on other embodiment of this invention, Comprising: It is sectional drawing in case a protrusion part has curvature outside. 本発明の他の実施形態に係る突出部であって、突出部が内側に反りを有する場合の断面図である。It is a protrusion part which concerns on other embodiment of this invention, Comprising: It is sectional drawing in case a protrusion part has curvature inside. 本発明の他の実施形態に係る突出部であって、突出部がR形状を有する場合の断面図である。It is a protrusion concerning other embodiments of the present invention, and is a sectional view in case a protrusion has an R shape. 本発明の他の実施形態に係る突出部であって、突出部が多角形状を有する場合の断面図である。It is a protrusion part which concerns on other embodiment of this invention, Comprising: It is sectional drawing in case a protrusion part has polygonal shape. 本発明の他の実施形態に係る突出部であって、突出部が貫通孔の壁側より貫通孔の中心軸方向に突出する複数の突出部材から構成された場合の断面図である。FIG. 11 is a cross-sectional view illustrating a protrusion according to another embodiment of the present invention, in which the protrusion includes a plurality of protrusion members that protrude in the direction of the central axis of the through hole from the wall side of the through hole. 図10Aの平面図である。FIG. 10B is a plan view of FIG. 10A. 本発明の他の実施形態に係る突出部であって、突出部を円環部材として、座刳りに嵌め込む場合を説明するための断面図である。It is a protrusion part which concerns on other embodiment of this invention, Comprising: It is sectional drawing for demonstrating the case where a protrusion part is used as a ring member, and it fits into a seat. 本発明の他の実施形態に係る突出部であって、突出部を円筒部材から構成した場合を説明するための断面図である。It is a protrusion part which concerns on other embodiment of this invention, Comprising: It is sectional drawing for demonstrating the case where a protrusion part is comprised from the cylindrical member. 本発明の他の実施形態に係る突出部であって、突出部をシート状の部材から構成した場合を説明するための断面図である。It is a protrusion part which concerns on other embodiment of this invention, Comprising: It is sectional drawing for demonstrating the case where a protrusion part is comprised from a sheet-like member. 本発明の効果を確認するために行った数値解析結果を説明するための図である。It is a figure for demonstrating the numerical-analysis result performed in order to confirm the effect of this invention. 突出部がない場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution when there is no protrusion part. 突出部の突出量(突出長)を0.2mmとした場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution when the protrusion amount (protrusion length) of the protrusion is 0.2 mm. 突出部の突出量(突出長)を0.4mmとした場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution at the time of the protrusion amount (protrusion length) of a protrusion part being 0.4 mm. 突出部の突出量(突出長)を0.6mmとした場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution when the protrusion amount (protrusion length) of the protrusion is 0.6 mm. 突出部の突出量(突出長)を0.8mmとした場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution when the protrusion amount (protrusion length) of a protrusion part is 0.8 mm. 突出部の突出量(突出長)と吸音率との関係を示したグラフである。It is the graph which showed the relationship between the protrusion amount (protrusion length) of a protrusion part, and a sound absorption rate. 突出部の厚さゼロの場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution in case the thickness of a protrusion part is zero. 突出部の厚さ0.05mmの場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution in case the thickness of a protrusion part is 0.05 mm. 突出部の厚さ0.1mmの場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution in case the thickness of a protrusion part is 0.1 mm. 突出部の厚さ0.2mmの場合の粒子速度分布とエントロピー分布を示す図である。It is a figure which shows the particle velocity distribution and entropy distribution in case the thickness of a protrusion part is 0.2 mm. 突出部の厚さをゼロとした場合の粒子速度分布とエントロピー分布を示す。The particle velocity distribution and entropy distribution when the thickness of the protrusion is zero are shown. 突出部の厚さを0.05mmとした場合の粒子速度分布とエントロピー分布を示す。The particle velocity distribution and entropy distribution when the thickness of the protrusion is 0.05 mm are shown. 突出部の厚さをゼロとし、形状をシャープエッジとした場合の粒子速度分布とエントロピー分布を示す。The particle velocity distribution and entropy distribution when the thickness of the protrusion is zero and the shape is a sharp edge are shown. 突出部の厚さを0.05mmとし、形状をシャープエッジとした場合の粒子速度分布とエントロピー分布を示す。The particle velocity distribution and entropy distribution when the thickness of the protrusion is 0.05 mm and the shape is a sharp edge are shown. 本発明に係る共鳴型吸音パネルの適用例を示す図である。It is a figure which shows the example of application of the resonance type sound absorption panel which concerns on this invention. 本発明の変形例に係る突出部の断面図である。It is sectional drawing of the protrusion part which concerns on the modification of this invention. 本発明の別の変形例に係る突出部の断面図である。It is sectional drawing of the protrusion part which concerns on another modification of this invention. 本発明の更に別の変形例に係る突出部の断面図である。It is sectional drawing of the protrusion part which concerns on another modification of this invention.

以下、図面を参照しながら、本発明の実施形態を説明する。   Hereinafter, embodiments of the present invention will be described with reference to the drawings.

<共鳴型吸音パネルの構成>
図1は、本発明の一実施形態に係る共鳴型吸音パネルの分解斜視図,図2はその共鳴型吸音パネルの一部断面図、図3Aはその共鳴型吸音パネルの貫通孔付近の拡大断面図、図3Bはその共鳴型吸音パネルの貫通孔付近の平面図である。
<Configuration of resonance type sound absorbing panel>
1 is an exploded perspective view of a resonance type sound absorbing panel according to an embodiment of the present invention, FIG. 2 is a partial sectional view of the resonance type sound absorbing panel, and FIG. 3A is an enlarged cross section near the through hole of the resonance type sound absorbing panel. FIG. 3B is a plan view of the vicinity of the through hole of the resonance type sound absorbing panel.

共鳴型吸音パネル1は、パネル本体10、表面板20及び背後壁30を含む。   The resonance type sound absorbing panel 1 includes a panel body 10, a surface plate 20, and a back wall 30.

パネル本体10は、多数のセル11を有し、これらセル11は、隔壁12により区画されている。   The panel body 10 has a large number of cells 11, and these cells 11 are partitioned by partition walls 12.

パネル本体10の表面側には、表面板20が貼り付けられ、パネル本体10の裏面側には、背後壁30が貼り付けられている。これにより、共鳴型吸音パネル1は、セル11を区画する隔壁12と、区画されたセル11の上下に設けられ、表面板20と、背後壁30とからなる、多数のセル構造40を構成する。   A surface plate 20 is affixed to the front side of the panel body 10, and a back wall 30 is affixed to the back side of the panel body 10. Thereby, the resonance type sound absorbing panel 1 is provided on the upper and lower sides of the partition wall 12 partitioning the cell 11 and the partitioned cell 11, and constitutes a large number of cell structures 40 including the surface plate 20 and the back wall 30. .

表面板20は、外部の空気層とセル11とを貫通する貫通孔21が設けられている。実施形態では、1つセル11について7つの貫通孔21が設けられているが、本発明はこれに限定されず、貫通孔21の数は1つでもよく、また2つ以上のいずれであってもよい。   The surface plate 20 is provided with a through hole 21 that penetrates the external air layer and the cell 11. In the embodiment, seven through holes 21 are provided for one cell 11, but the present invention is not limited to this, and the number of through holes 21 may be one, or any of two or more. Also good.

貫通孔21の表面側端部21aには、その壁側より貫通孔21の中心軸方向に円環状に突出する突出部50が設けられている。突出部50の突出長εは、貫通孔21の直径dの20%以下、すなわち、
ε/d≦0.2
の関係を有する。
これにより、貫通孔21に突出部50を設けない場合に比べて吸音率が高くなる。この点については後述する。
A protruding portion 50 that protrudes in an annular shape in the central axis direction of the through hole 21 from the wall side is provided at the surface side end portion 21 a of the through hole 21. The protrusion length ε of the protrusion 50 is 20% or less of the diameter d of the through hole 21, that is,
ε / d ≦ 0.2
Have the relationship.
Thereby, compared with the case where the protrusion part 50 is not provided in the through-hole 21, a sound absorption rate becomes high. This point will be described later.

共鳴型吸音パネル1は、その表面に入射する音波のエネルギーを吸収する機能を有している。共鳴型吸音パネル1の表面は、音波が入射する空間側から見れば、平面のみならず、曲面、任意の形状を有していてもよい。   The resonance type sound absorbing panel 1 has a function of absorbing energy of sound waves incident on the surface thereof. The surface of the resonance type sound absorbing panel 1 may have not only a flat surface but also a curved surface and an arbitrary shape as viewed from the space where the sound wave enters.

共鳴型吸音パネル1は、パネル表面から三層の構造で成り立つ。これらは、表面板20、多数のセル(cell)11からなるパネル本体10、背後壁30として認識される。表面板20には貫通孔21が開けられており、表面板20に接する空気とセル構造40とを連通する。セル構造40は、表面板20、背後壁30及びセル11を区画する隔壁12に囲まれた小空間である。共鳴型吸音パネル1の用途によっては、セル11を区画する隔壁12の一部にセル内に浸入した水を抜くための小孔が設けられる場合もある。また、後述するように、背後壁30に小孔を設けてその背後にセル11と背後層を設ける多層吸音パネル、所謂マルチレイヤー吸音パネルという構造も存在する。セル構造40が貫通孔21空き表面板20と背後壁30によって挟まれていることから、「サンドイッチ構造」と呼ばれることもある。   The resonance type sound absorbing panel 1 has a three-layer structure from the panel surface. These are recognized as a surface plate 20, a panel body 10 composed of a large number of cells 11, and a back wall 30. A through-hole 21 is formed in the surface plate 20, and air that contacts the surface plate 20 communicates with the cell structure 40. The cell structure 40 is a small space surrounded by the surface plate 20, the back wall 30, and the partition wall 12 that partitions the cell 11. Depending on the application of the resonance type sound absorbing panel 1, a small hole for removing water that has entered the cell may be provided in a part of the partition wall 12 that partitions the cell 11. In addition, as will be described later, there is a so-called multi-layer sound absorbing panel structure in which a small hole is provided in the back wall 30 and the cell 11 and the back layer are provided behind the small hole. Since the cell structure 40 is sandwiched between the free surface plate 20 of the through-hole 21 and the back wall 30, it may be called a “sandwich structure”.

個々のセル構造40の断面形状は任意であって、三角形、四角形、多角形でも円形でもよい。六角形のものを特に「ハニカム(honeycomb)」構造と呼ぶ。セル構造40は、原則として表面板20に設けた貫通孔21を介してのみ外部と連通する。背後壁30は空気の振動に対して十分剛性を有するものと仮定する。また、通常の扱いでは、セル構造40を取り囲む隔壁12はすべて、内部の空気に比べて十分剛性があるものとして扱われる。   The cross-sectional shape of each cell structure 40 is arbitrary, and may be triangular, quadrangular, polygonal or circular. Hexagonal ones are called “honeycomb” structures. The cell structure 40 communicates with the outside only through the through hole 21 provided in the surface plate 20 in principle. It is assumed that the back wall 30 is sufficiently rigid against air vibration. Further, in normal handling, all the partition walls 12 surrounding the cell structure 40 are treated as having sufficient rigidity as compared with the internal air.

共鳴型吸音パネル1は、上記構造から定まる音響的な共鳴周波数の下で、吸音性能を高める働きを有する。一般に空気中を伝播する音は、周波数によって時間的に再現性のある波を形成する。音には複数の周波数とそれに伴う振幅や位相を有する音が含まれていることが通常である。共鳴型吸音パネル1は、特定の周波数を中心とする周波数帯域で吸音性能を高める。   The resonance type sound absorbing panel 1 has a function of improving sound absorbing performance under an acoustic resonance frequency determined from the above structure. In general, sound propagating in the air forms a wave having time reproducibility depending on the frequency. In general, a sound includes a sound having a plurality of frequencies and accompanying amplitudes and phases. The resonance type sound absorbing panel 1 enhances sound absorbing performance in a frequency band centered on a specific frequency.

共鳴型吸音パネル1の共鳴周波数fは、セル構造40の体積V、セル11に対応する表面の貫通孔21の面積の合計S、貫通孔21の長さ(言い換えれば表面板20の厚さに相当)dによって、次のように定義される。ここで、d'はdに対して開口端補正量を加えたものである。
f〜c/2π√(s/Vd')
The resonance frequency f of the resonance type sound absorbing panel 1 includes the volume V of the cell structure 40, the total area S of the surface through holes 21 corresponding to the cells 11, and the length of the through holes 21 (in other words, the thickness of the surface plate 20). Equivalent) d is defined as follows. Here, d ′ is obtained by adding an opening end correction amount to d.
f to c / 2π√ (s / Vd ′)

共鳴型吸音パネル1の表面板20に音波、即ち微小な圧力変動が到達すると、表面板20の貫通孔21の空部内部の空気が変位する。この貫通孔21の空部内部の空気がセル構造40側に押されるとセル構造40の内部の空気が圧縮され、貫通孔21の空部内部の空気が引っ張られるとセル構造40の内部の空気が膨張する。ただし、貫通孔21の空部内部の体積は、セル構造40の体積に比べて十分小さいので、上記圧縮と膨張による体積変化量はセル構造40の体積に比べて十分小さい。入射音は周期(或いは周波数)で変動するため、貫通孔21の空部内部の空気も入射音波の周波数で変位し、結果としてセル構造40の内部の微小圧力も入射音波の周波数で変動することとなる。   When sound waves, that is, minute pressure fluctuations reach the surface plate 20 of the resonance type sound absorbing panel 1, the air inside the empty portion of the through hole 21 of the surface plate 20 is displaced. When the air inside the empty part of the through hole 21 is pushed toward the cell structure 40 side, the air inside the cell structure 40 is compressed, and when the air inside the empty part of the through hole 21 is pulled, the air inside the cell structure 40 is compressed. Expands. However, since the volume inside the through hole 21 is sufficiently smaller than the volume of the cell structure 40, the volume change amount due to the compression and expansion is sufficiently smaller than the volume of the cell structure 40. Since the incident sound fluctuates with the period (or frequency), the air inside the cavity of the through hole 21 is also displaced with the frequency of the incident sound wave, and as a result, the micro pressure inside the cell structure 40 also fluctuates with the frequency of the incident sound wave. It becomes.

共鳴型吸音パネル1をバネ・マス・ダンパ系と等価とした場合、エネルギー散逸(吸音)はダンパが担っており、貫通孔21の空部内部の空気の変位の時間変動(粒子速度)と相関がある。入射音波がパネルの共鳴周波数に近い周波数を有する場合、バネ・マス・ダンパ系の周波数応答と同じように変位の一次時間微分である粒子速度は大きくなる。マクロな系で見れば、粒子速度の増大は、ダンパによるエネルギー散逸を増加させ、外部加振である入射音波のエネルギーの散逸を増大させる結果となり、吸音パネルでの入射音波の減衰となって現れる。   When the resonance type sound absorbing panel 1 is equivalent to a spring / mass / damper system, the energy dissipation (sound absorption) is carried by the damper, and is correlated with the time variation (particle velocity) of the displacement of the air inside the through hole 21. There is. When the incident sound wave has a frequency close to the resonance frequency of the panel, the particle velocity, which is the first time derivative of the displacement, is increased as in the frequency response of the spring-mass-damper system. In a macro system, an increase in particle velocity results in an increase in energy dissipation by the damper and an increase in energy dissipation of the incident sound wave, which is an external excitation, and appears as attenuation of the incident sound wave in the sound absorbing panel. .

このように共鳴型吸音パネル1は、機械系のバネ・マス・ダンパのモデルに等値できる。貫通孔21の空気はマス(質量)に相当し、外力である入射音に対して変位する。変位を受けてセル構造40の内部の空気は圧縮・膨張して貫通孔21の空気に対する復元力をもたらす(バネ)の役割を果たす。ダンパは、貫通孔21の空気が変位するのに伴って生ずため、変位の時間微分(粒子速度)によって発生する。つまり、理論的には共鳴型吸音パネル1の減衰効果は、セル構造40の内部よりも表面板20の貫通孔21の空気の変動によるものが支配的といえる。   Thus, the resonance type sound absorbing panel 1 can be equivalent to a mechanical spring, mass, and damper model. The air in the through-hole 21 corresponds to a mass (mass) and is displaced with respect to incident sound that is an external force. In response to the displacement, the air inside the cell structure 40 plays a role of (spring) that compresses and expands and brings a restoring force to the air of the through hole 21. Since the damper does not occur as the air in the through hole 21 is displaced, the damper is generated by time differentiation (particle velocity) of the displacement. That is, theoretically, it can be said that the attenuation effect of the resonance type sound absorbing panel 1 is dominated by the fluctuation of the air in the through hole 21 of the surface plate 20 rather than the inside of the cell structure 40.

貫通孔21の空気層が運動することによって励起される粒子速度によって発生するエネルギー散逸とマクロな視点での吸音効果とを関連付けて、エネルギー散逸が支配的である貫通孔21の、しかも粒子速度振幅が大きくなると予想される開口部(表面側端部21a)の孔形状に着目する。本発明は、典型的には、貫通孔21の表面側端部21aの孔形状に僅かな変化を与える、つまり突出部50を設けることで、吸音パネル1の主たる性質を変更することなく、吸音性能(ここでは、入射音波のエネルギーに対する反射音波のエネルギーの比として吸音率を例に取る)を改善するものである。ここで、吸音パネルの主たる性質とは、共鳴周波数、重量や嵩、表面粗さなどを含む。   The energy dissipation generated by the particle velocity excited by the movement of the air layer of the through-hole 21 and the sound absorption effect from a macro viewpoint are related to each other, and the particle velocity amplitude of the through-hole 21 in which the energy dissipation is dominant. Attention is paid to the hole shape of the opening portion (surface side end portion 21a) that is expected to increase. Typically, the present invention provides a slight change in the hole shape of the surface-side end portion 21a of the through-hole 21, that is, by providing the protruding portion 50, without changing the main properties of the sound-absorbing panel 1, the sound-absorbing sound. The performance (here, the sound absorption rate is taken as an example of the ratio of the energy of the reflected sound wave to the energy of the incident sound wave) is improved. Here, the main properties of the sound absorbing panel include resonance frequency, weight and bulk, surface roughness, and the like.

ここで、表面板20の表面及び背面に対して、貫通孔21の内面の接線が垂直をなす場合、つまり図1から図3の共鳴型吸音パネル1において突出部50がない場合を、基準(ベースライン)形状と定義する。ベースラインは、いわば、貫通孔21が表面板20に垂直に空けられていて、横から見ると貫通孔21側面と表面板20の板表面並びに板裏面とが直角をなすものである。   Here, the case where the tangent of the inner surface of the through hole 21 is perpendicular to the front and back surfaces of the surface plate 20, that is, the case where there is no protrusion 50 in the resonance type sound absorbing panel 1 of FIGS. Baseline) shape. In other words, the base line is such that the through hole 21 is formed perpendicular to the surface plate 20, and when viewed from the side, the side surface of the through hole 21 and the surface of the surface plate 20 and the back surface of the surface plate form a right angle.

このベースライン形状に対して、本実施形態に係る共鳴型吸音パネル1は貫通孔21に上記の突出部50を設けたものである。   With respect to this baseline shape, the resonance type sound absorbing panel 1 according to the present embodiment is such that the protruding portion 50 is provided in the through hole 21.

すなわち、この共鳴型吸音パネル1は、表面板20の貫通孔21、或いは後述するようにパネルのセル内部の中間隔壁の貫通孔の裏面側端部及び/又は表面側端部に突起をなす突出部50を設けて貫通孔21を部分的に塞いだ孔とし、突出部50である突起物の高さである突出長は、貫通孔21の直径(非円形孔では等価直径)の20%以下とする。   That is, the resonance type sound absorbing panel 1 is a protrusion that forms protrusions on the back surface side end portion and / or the surface side end portion of the through hole 21 of the surface plate 20 or the through hole of the intermediate partition wall inside the cell of the panel as will be described later. The projecting length, which is the height of the projection that is the projecting portion 50, is 20% or less of the diameter of the through hole 21 (equivalent diameter for a non-circular hole). And

例えば、貫通孔21が円形で、貫通孔21の直径が1.65mmで12%高さの突起を想定すると、内径1.65×0.12=0.2mmの同心円状の微小突起(突出部50)を形成する。突出部50の突起形状は、貫通孔21の流路(直線部)から孔に直角な方向に滑らかに接続してもよいし、直角に変化してもよい。   For example, assuming that the through-hole 21 is circular, the diameter of the through-hole 21 is 1.65 mm, and a 12% -high protrusion, concentric minute protrusions (projections) having an inner diameter of 1.65 × 0.12 = 0.2 mm 50). The protrusion shape of the protrusion 50 may be smoothly connected in a direction perpendicular to the hole from the flow path (straight portion) of the through hole 21 or may be changed to a right angle.

より具体的には、突出部50は、表面板20の貫通孔21の開口端部に薄い突起があり、その突出部50は端部の角から貫通孔21の中心軸方向に伸張している。突出部50の厚さは孔径に比べて工学的に十分薄いものを想定する。例えば、その厚さは、貫通孔21の直径の5%以下、端部角からの突出量は、最大でも貫通孔21の直径の20%とする。突出部50を貫通孔21の中心軸から見ると貫通孔に対して同心円状となっている。すなわち、突出部50は円環状の形状をなしている。   More specifically, the protrusion 50 has a thin protrusion at the opening end of the through hole 21 of the surface plate 20, and the protrusion 50 extends from the corner of the end toward the central axis of the through hole 21. . The thickness of the protrusion 50 is assumed to be sufficiently thin in terms of engineering compared to the hole diameter. For example, the thickness is 5% or less of the diameter of the through hole 21, and the protrusion amount from the end corner is 20% of the diameter of the through hole 21 at the maximum. When the protrusion 50 is viewed from the central axis of the through hole 21, it is concentric with the through hole. That is, the protrusion 50 has an annular shape.

<突出部の態様>
この実施形態では、突出部50は円環状の形状をなしているが、本発明に係る突出部は図4〜図13に示すように様々形態で実現できる。
<Aspect of protrusion>
In this embodiment, the protrusion 50 has an annular shape, but the protrusion according to the present invention can be realized in various forms as shown in FIGS.

例えば、図4に示すように、突出部50は、貫通孔21の壁側より貫通孔21の中心軸方向になるに従い薄くなるように構成してもよい。その場合に、図5に示すように、突出部50の先端が鋭角となるように構成してもよい。更に、図6及び図7に示すように、突出部50は、貫通孔21の軸方向のいずれか一方の方向に反りを有してもよい。すなわち、図6に示したように、突出部50は貫通孔21の外側(空気層側)に反っていてもよいし、図7に示したように、突出部50は貫通孔21の内側に反っていてもよい。また、突出部50は、その貫通孔21内側の面が、図8に示すようにR形状であってもよいし、図9に示すように多角形状であってもよい。   For example, as shown in FIG. 4, the protrusion 50 may be configured to become thinner from the wall side of the through hole 21 toward the center axis direction of the through hole 21. In that case, you may comprise so that the front-end | tip of the protrusion part 50 may become an acute angle, as shown in FIG. Further, as shown in FIGS. 6 and 7, the protrusion 50 may have a warp in any one of the axial directions of the through hole 21. That is, as shown in FIG. 6, the protruding portion 50 may be warped on the outer side (air layer side) of the through hole 21, and as shown in FIG. 7, the protruding portion 50 is on the inner side of the through hole 21. It may be warped. Moreover, as for the surface inside the through-hole 21, the protrusion part 50 may be R shape as shown in FIG. 8, and may be polygonal shape as shown in FIG.

図10A及び図10Bに示すように、突出部50を、貫通孔21の径方向に沿って間隔をもって配置され、貫通孔21の壁側より貫通孔21の中心軸方向に突出する複数の突出部材51から構成してもよい。   As shown in FIG. 10A and FIG. 10B, a plurality of projecting members 50 are arranged at intervals along the radial direction of the through hole 21 and project from the wall side of the through hole 21 toward the central axis of the through hole 21. You may comprise from 51.

図11に示すように、突出部50を有する円環部材52を有し、表面板20の貫通孔21の周囲に座刳り22を設け(図11(a))、座刳り22に円環部材52を嵌め込んでもよい(図11(b))。   As shown in FIG. 11, it has an annular member 52 having a protrusion 50, and a countersink 22 is provided around the through hole 21 of the surface plate 20 (FIG. 11A). 52 may be fitted (FIG. 11B).

図12に示すように、突出部50を有する円筒部材53を用意し(図12(a))、貫通孔21に円筒部材53を嵌め込んでもよい(図12(b))。   As shown in FIG. 12, a cylindrical member 53 having a protruding portion 50 may be prepared (FIG. 12 (a)), and the cylindrical member 53 may be fitted into the through hole 21 (FIG. 12 (b)).

図13に示すように、貫通孔21より穴径の小さい孔55が空けられた薄いシート状の部材54を用意し(図13(a))、貫通孔21内に小さい孔55が位置するように、表面板20の表面にシート状の部材54を張り付けて(図13(b))、貫通孔21内にシート状の部材54が張り出すようにして突出部50を構成してもよい。   As shown in FIG. 13, a thin sheet-like member 54 having a hole 55 smaller in diameter than the through hole 21 is prepared (FIG. 13A), and the small hole 55 is positioned in the through hole 21. In addition, the sheet-like member 54 may be attached to the surface of the surface plate 20 (FIG. 13B), and the protruding portion 50 may be configured so that the sheet-like member 54 protrudes into the through hole 21.

<突出部による効果>
本発明に係る突出部50を設けたときに音波の入射に伴う粒子速度変動を数値流体解析によって算出した例を図14に示す。
<Effects of protrusions>
FIG. 14 shows an example in which the particle velocity fluctuation accompanying the incidence of sound waves is calculated by numerical fluid analysis when the protrusion 50 according to the present invention is provided.

図14は、孔径1.65mmの貫通孔21、突出長0.4mmの突出部50(突出部の厚さは0とした。)と共鳴周波数2150Hzを有する共鳴型吸音パネル1をモデルとし、120dBの音波を垂直入射させたときの貫通孔21周辺の粒子速度並びに生成エンタルピーを数値流体解析した結果である。瞬時粒子速度分布は矢印、瞬時エントロピー生成はグレースケールの濃淡で表している。   FIG. 14 shows a model of a resonance type sound absorbing panel 1 having a through hole 21 having a hole diameter of 1.65 mm, a protrusion 50 having a protrusion length of 0.4 mm (the thickness of the protrusion is 0) and a resonance frequency of 2150 Hz, and 120 dB. 3 is a result of numerical fluid analysis of the particle velocity around the through hole 21 and the generation enthalpy when a normal sound wave is vertically incident. The instantaneous particle velocity distribution is represented by arrows, and the instantaneous entropy generation is represented by grayscale shading.

図は軸対象セル構造の貫通孔21近傍を表しており、段差の左側が貫通孔21を意味する。段差下部がセル11と呼ばれる空間に繋がっており、段差上部は管路、つまり音波の通路を意味し、上から段差に向かって音波が入射する。
この瞬間、セル11の音圧が高い位相にあるので、セル11から管路に向かって粒子速度ベクトルが形成され、突出部50で循環する部分がある。突出部50の先端Aで剥離が起こっていることが判る。損失(吸音)が大きく生じるのは、この突出部50の先端Aでの剥離流れに起因している。
The figure shows the vicinity of the through-hole 21 of the axis target cell structure, and the left side of the step means the through-hole 21. The lower part of the step is connected to a space called a cell 11, and the upper part of the step means a pipe line, that is, a sound wave passage, and a sound wave enters from the top toward the step.
At this moment, since the sound pressure of the cell 11 is in a high phase, a particle velocity vector is formed from the cell 11 toward the pipeline, and there is a portion that circulates in the protrusion 50. It can be seen that peeling occurs at the tip A of the protrusion 50. The large loss (sound absorption) is caused by the separation flow at the tip A of the protrusion 50.

図15A〜図15Eは、突出部50の突出量(突出長)をゼロから0.8mmまで0.2mmずつ増やしつつ、孔直径を増やした時の粒子速度分布とエントロピー分布を示す。ベースラインの貫通孔21の直径は1.65mmである。
図15Aは突出部50の突出量(突出長)をゼロ、図15Bは突出部50の突出量(突出長)を0.2mm、図15Cは突出部50の突出量(突出長)を0.4mm、図15Dは突出部50の突出量(突出長)を0.6mm、図15Eは突出部50の突出量(突出長)を0.8mmとした場合である。以下の表は最大吸音率を整理したものである。
15A to 15E show the particle velocity distribution and the entropy distribution when the hole diameter is increased while increasing the protrusion amount (protrusion length) of the protrusion 50 from zero to 0.8 mm by 0.2 mm. The diameter of the baseline through-hole 21 is 1.65 mm.
15A shows a protrusion amount (projection length) of the protrusion portion 50 of zero, FIG. 15B shows a protrusion amount (protrusion length) of the protrusion portion 50 of 0.2 mm, and FIG. 4D, FIG. 15D shows a case where the protrusion amount (protrusion length) of the protrusion 50 is 0.6 mm, and FIG. 15E shows a case where the protrusion amount (protrusion length) of the protrusion 50 is 0.8 mm. The table below summarizes the maximum sound absorption rate.

図16はこれらの結果から、突出部50の突出量(突出長)と吸音率との関係を示したグラフである。 FIG. 16 is a graph showing the relationship between the protrusion amount (protrusion length) of the protrusion 50 and the sound absorption rate based on these results.

突出量なしの場合(Baseline)に比べて、貫通孔21の孔径の10%で概ね最大の吸音率増加が得られており、同20%に相当でも吸音率の増加は認められる。   Compared to the case where there is no protrusion (Baseline), the maximum increase in the sound absorption coefficient is obtained at 10% of the hole diameter of the through-hole 21, and an increase in the sound absorption coefficient is recognized even when it is equivalent to 20%.

解析では、垂直入射管を模擬して、表面板20に入射する音波を仮定したときの垂直入射管内に生成される定在波を求めている。定在波の振幅比に基づいて、吸音パネルでの垂直入射吸音率を求めている。計算結果によれば、本発明の解決手段を講じたケースでは、講じないケース(つまり単純に表面板に垂直に貫通孔21を設けたケース)に比べて吸音率が増加する結果を得た(図15A〜図15E)。   In the analysis, a standing wave generated in the vertical incident tube when a sound wave incident on the surface plate 20 is assumed is obtained by simulating the vertical incident tube. Based on the amplitude ratio of the standing wave, the normal incident sound absorption coefficient in the sound absorption panel is obtained. According to the calculation result, in the case where the solution of the present invention was taken, the sound absorption coefficient was increased as compared with the case where the solution was not taken (that is, the case where the through hole 21 was simply provided perpendicular to the surface plate). 15A to 15E).

また、貫通孔21端部周辺でのエントロピーの生成量に注目すると、図15A〜図15Eの濃淡から、本発明に係る突出部50を設けた場合の方がエントロピーの生成量が増加している傾向が認められる。このことは、粒子速度によって生じる熱散逸の増加を説明しており、巨視的観点では吸音率増加を裏付けている。同じことは、多層吸音パネルの中間板に設けられた貫通孔形状についても適用可能と考えられる。   Further, when attention is paid to the amount of entropy generated around the end portion of the through-hole 21, the amount of entropy generated is increased in the case where the protruding portion 50 according to the present invention is provided from the shades of FIGS. 15A to 15E. A trend is observed. This explains the increase in heat dissipation caused by the particle velocity and supports the increase in sound absorption from a macroscopic point of view. The same can be applied to the shape of the through-hole provided in the intermediate plate of the multilayer sound-absorbing panel.

以上のことから、微小突起である突出部50を貫通孔21の表面側端部である開口部に設けた表面板20の貫通孔21の形状(表面板20の断面形状)は、単純な孔を空けた場合に比べて、入射する音波のエネルギー減衰を促進する働きがあること、即ち吸音率を増加させる効果があることを示唆している。
なお、Baselineから20%以上の吸音率増加を目安とすると少なくとも15%の突出量であれば、より有意な吸音率の増加が見込まれると考えられる。
From the above, the shape of the through-hole 21 of the surface plate 20 (the cross-sectional shape of the surface plate 20) in which the protruding portion 50 that is a minute protrusion is provided in the opening that is the surface side end of the through-hole 21 is a simple hole. This suggests that it has a function of promoting energy attenuation of the incident sound wave, that is, an effect of increasing the sound absorption rate, as compared with the case where a gap is made.
In addition, if a sound absorption rate increase of 20% or more from Baseline is taken as a guide, it is considered that a more significant increase in the sound absorption rate is expected if the protruding amount is at least 15%.

図17A〜17Dは突出部50の突出長を0.4mmとして突出部50の厚さを変化させた場合の粒子速度分布とエントロピー分布を示す。貫通孔21の直径は1.65mmである。
図17Aは突出部50の厚さがゼロ、図17Bは突出部50の厚さが0.05mm、図17Cは突出部50の厚さが0.1mm、図17Dは突出部50の厚さが0.2mmの場合である。
下表はその場合の最大吸音率を整理したものである。
17A to 17D show the particle velocity distribution and entropy distribution when the protrusion length of the protrusion 50 is 0.4 mm and the thickness of the protrusion 50 is changed. The diameter of the through hole 21 is 1.65 mm.
17A shows zero thickness of the protrusion 50, FIG. 17B shows that the thickness of the protrusion 50 is 0.05 mm, FIG. 17C shows that the thickness of the protrusion 50 is 0.1 mm, and FIG. This is the case of 0.2 mm.
The table below summarizes the maximum sound absorption rate.

以上より突出部50の厚さが増すと吸音率は減少する傾向を示すことが分かる。 From the above, it can be seen that the sound absorption rate tends to decrease as the thickness of the protrusion 50 increases.

図18A〜18Dは突出部50の突起形状を現実的なものに変更した時の粒子速度分布とエントロピー分布を示す。貫通孔21の直径は1.65mm、突出部50の突起高さ(突出長)は0.4mmである。
図18Aは突出部50の厚さをゼロとした場合で吸音率は0.997となった。図18Bは突出部50の厚さを0.05mmとした場合で吸音率は0.991となった。図18Cは突出部50の先端に向かって薄くしたシュープエッジの場合であって基部の厚さをゼロとした場合で吸音率は0.991となった。図18Cは突出部50の先端に向かって薄くしたシュープエッジの場合であって基部の厚さを0.05mmとした場合で吸音率は0.977となった。突起部50の厚さが0.05mm(現実的には薄い)とシャープエッジ(現実的な形状)とが同様な吸音率である。
18A to 18D show the particle velocity distribution and entropy distribution when the protrusion shape of the protrusion 50 is changed to a realistic one. The diameter of the through hole 21 is 1.65 mm, and the protrusion height (protrusion length) of the protrusion 50 is 0.4 mm.
FIG. 18A shows the case where the thickness of the protrusion 50 is zero, and the sound absorption coefficient is 0.997. FIG. 18B shows the case where the thickness of the protrusion 50 is 0.05 mm, and the sound absorption coefficient is 0.991. FIG. 18C shows a case where the shoe edge is thinned toward the tip of the protrusion 50, and the sound absorption coefficient is 0.991 when the thickness of the base is zero. FIG. 18C shows a case where the shoe edge is thinned toward the tip of the protrusion 50, and the sound absorption coefficient is 0.977 when the thickness of the base is 0.05 mm. The thickness of the protrusion 50 is 0.05 mm (really thin) and the sharp edge (realistic shape) is the same sound absorption coefficient.

<本発明に係る共鳴型吸音パネルの適用例>
以下のとおりの本発明に係る共鳴型吸音パネルの適用の類型が考えられる。なお、簡略化して、共鳴型吸音パネルを吸音パネルと記載する。
<Application example of resonance type sound absorbing panel according to the present invention>
The following types of application of the resonance type sound absorbing panel according to the present invention are conceivable. For simplicity, the resonance type sound absorbing panel is referred to as a sound absorbing panel.

その1)伝播経路の壁面に設置して、騒音の伝播を妨げる。   1) Install on the wall of the propagation path to prevent noise propagation.

伝播経路は通常、ダクトのような流路である。本類型では、伝播経路の壁面に孔空き表面板が設置され、その背後にセル構造と背後壁が存在する。伝播経路内部に気流が存在してもよく、気流には経路断面方向に速度分布や温度分布が存在してもよい。騒音は気流と同じ方向に伝播する場合と反対方向に伝播する場合がある。また、騒音に経路断面形状に応じた音響モード(音圧の腹と節が存在する音圧分布であって、同一の周波数に複数の音圧分布が存在することや、音圧分布の空間的位置が時間変化することを含む)が存在することがある。具体的には、航空機用ターボファンエンジンの吸入ダクトや排気ダクト内壁に吸音パネルを設置することで、ファンで発生する騒音をエンジンの外部に放出される前にその音圧レベルを軽減する例が挙げられる。ジェットエンジンの地上運転設備では、冷却後の高速排気ジェットを導入して外部に排気するダクト内壁に吸音パネルを設置することで、ジェット騒音による高音圧騒音を軽減する例が挙げられる。発電プラントでは、同じく空気吸入側ダクト内壁に吸音パネルを設置して、ブロアや圧縮機から発生する騒音を外部に放出する前に減衰させる例が挙げられる。   The propagation path is usually a flow path such as a duct. In this type, a perforated surface plate is installed on the wall surface of the propagation path, and the cell structure and the back wall exist behind it. An air flow may exist inside the propagation path, and a velocity distribution and a temperature distribution may exist in the path cross-sectional direction. Noise may propagate in the same direction as the airflow or in the opposite direction. Also, the acoustic mode corresponding to the cross-sectional shape of the noise (sound pressure distribution with the antinodes and nodes of the sound pressure, where there are multiple sound pressure distributions at the same frequency, and the spatial distribution of the sound pressure In some cases, including a time-varying position). Specifically, there is an example in which the sound pressure level is reduced before noise generated by the fan is released to the outside of the engine by installing a sound absorbing panel on the inner wall of the intake duct or exhaust duct of an aircraft turbofan engine. Can be mentioned. In the ground operation facility of a jet engine, there is an example in which high sound pressure noise due to jet noise is reduced by installing a sound absorbing panel on the inner wall of a duct that introduces a cooled high-speed exhaust jet and exhausts it to the outside. In a power plant, there is also an example in which a sound absorbing panel is installed on the inner wall of the air intake side duct to attenuate the noise generated from the blower or compressor before it is released to the outside.

その2)騒音が入射する壁面に設置して、騒音の反射を妨げる。   2) Install it on the wall where noise enters and prevent reflection of noise.

本類型は、開放空間に置かれた壁や塀、構造物の表面にパネルを設置するものである。パネル表面に気流があってもよい。入射騒音の進行方向は、パネル表面板と垂直方向でなくともよい。具体例として、静粛性を要求する部屋の壁面に吸音パネルを設置し、室内の反響を抑制すること、高速車両が通行する路線に設けた塀の表面に吸音パネルを設置して、車両、路面から発生して塀に入射する騒音の反射を弱めて、周囲への騒音暴露量を減らすこと、航空機の機体(胴体表面、フラップなどの高揚力装置、脚や格納ドアなどの着陸装置)表面に吸音パネルを設置することで、空力騒音やエンジン騒音を騒音発生源で極力抑制して遠方への騒音放射を抑制すること、などが挙げられる。   In this type, panels are installed on the surfaces of walls, walls, and structures placed in open spaces. There may be airflow on the panel surface. The traveling direction of incident noise may not be perpendicular to the panel surface plate. As a specific example, a sound absorbing panel is installed on the wall surface of a room that requires quietness to suppress the echo in the room, a sound absorbing panel is installed on the surface of the fence provided on the route through which the high-speed vehicle passes, and the vehicle, road surface To reduce the reflection of noise generated from the incident and incident on the kite to reduce the amount of noise exposure to the surroundings, on the surface of the aircraft body (the fuselage surface, high lift devices such as flaps, landing devices such as legs and storage doors) By installing a sound-absorbing panel, aerodynamic noise and engine noise can be suppressed as much as possible with a noise generation source, and noise emission to a distant location can be exemplified.

その3)閉空間を覆う境界面の全部または一部に設置して、内部の騒音を低減する。   3) Install it on all or part of the boundary surface covering the closed space to reduce internal noise.

閉空間であって、騒音源を含むゆえに騒音場が形成される場合と、騒音源を含まないが、外部騒音源から振動を通じて導入された騒音場が形成される場合を想定する。閉空間の全部または一部にパネルを設置することで、閉空間内を伝播する騒音の振幅をパネル表面で減衰させることで、閉空間内の騒音をパネルがない場合に比べて低減させることを想定する。具体例として、ボイラや燃焼器の内壁に耐熱性吸音パネルを設置して、燃焼室内部で発生する不安定燃焼振動や燃焼騒音を吸音することで、不安定振動の抑制や外部に伝播する燃焼騒音低減を図ること、ロケットフェアリング内壁に吸音パネルを設置することで、ロケット打上時に発生する外部音響がフェアリングの振動を介してフェアリング内部に励起する音場を軽減すること、航空機の機内壁に吸音パネルを設置して、外部から伝搬するエンジン騒音、機体騒音、境界層騒音を機内で軽減すること、などが挙げられる。   It is assumed that the noise field is formed because it is a closed space and includes a noise source, and the case where a noise field that does not include a noise source but is introduced from an external noise source through vibration is formed. By installing a panel in all or part of the closed space, the noise amplitude propagating in the closed space is attenuated on the panel surface, thereby reducing the noise in the closed space compared to when there is no panel. Suppose. As a specific example, by installing a heat-resistant sound absorbing panel on the inner wall of a boiler or combustor and absorbing unstable combustion vibration and combustion noise generated inside the combustion chamber, it suppresses unstable vibration and combustion propagates outside. By reducing noise, installing a sound absorbing panel on the inner wall of the rocket fairing, reducing the sound field in which the external sound generated when launching the rocket is excited inside the fairing through the vibration of the fairing, For example, installing a sound absorbing panel on the inner wall to reduce engine noise, airframe noise, and boundary layer noise propagating from the outside.

(実施例1)
航空機用ジェットエンジン吸入及び排気ダクトに本発明に係る吸音パネル1を設置する。
Example 1
The sound absorbing panel 1 according to the present invention is installed in an aircraft jet engine intake and exhaust duct.

図19に示すように、ダクト61の内壁面に本発明に係る吸音パネル1を設置する。ダクト61の内壁は通常円形であって吸音パネル1は曲率を有するとともに、ダクト61の軸方向に半径が変化する。なお、図19において、符号62はエンジンの空気吸引口を示し、63はファン動翼、64はファン静翼を示す。   As shown in FIG. 19, the sound absorbing panel 1 according to the present invention is installed on the inner wall surface of the duct 61. The inner wall of the duct 61 is usually circular, the sound absorbing panel 1 has a curvature, and the radius changes in the axial direction of the duct 61. In FIG. 19, reference numeral 62 denotes an air suction port of the engine, 63 denotes a fan rotor blade, and 64 denotes a fan stationary blade.

表面板20、セル構造40、背後壁30が単層の場合(シングルレイヤ吸音パネルの場合)、本発明に係る貫通孔21は表面板20に加工する。複層の場合(ダブルレイヤ吸音パネル、トリプルレイヤ吸音パネルなど)、本発明に係る貫通孔は、表面板20の貫通孔21のみならず、セプタムと呼ばれる層間隔壁に設ける貫通孔に適用することも含む。このとき、表面板20の貫通孔21とセプタムとで孔の閉塞部(突出部50)の形状を変更してもよい。表面板20にはファン吸気あるいは排気が通過するため、孔形状を大幅に変更すると流れ場が変わり、ダクト内の圧力損失への影響が避けられない。本発明のように、直線状或いは他の小さな突起を使って、貫通孔の孔径の高々15%程度の部分的な閉塞を施す場合には、流れ場への影響を減らすことが見込まれ、圧力損失を維持したまま吸音性能を向上できると推測される。   When the surface plate 20, the cell structure 40, and the back wall 30 are single layers (in the case of a single layer sound absorbing panel), the through hole 21 according to the present invention is processed into the surface plate 20. In the case of multiple layers (double layer sound absorbing panel, triple layer sound absorbing panel, etc.), the through hole according to the present invention can be applied not only to the through hole 21 of the surface plate 20 but also to a through hole provided in an interlayer partition called a septum. Including. At this time, you may change the shape of the obstruction | occlusion part (protrusion part 50) of a hole with the through-hole 21 and septum of the surface board 20. FIG. Since the fan intake or exhaust passes through the surface plate 20, if the hole shape is significantly changed, the flow field changes, and the influence on the pressure loss in the duct is inevitable. As in the present invention, when a partial blockage of about 15% of the hole diameter of the through hole is applied using a straight line or other small protrusion, it is expected that the influence on the flow field is reduced. It is estimated that the sound absorption performance can be improved while maintaining the loss.

(実施例2)
発電プラント等の吸入・排気ダクトに本発明に係る吸音パネル1を設置する。
(Example 2)
The sound absorbing panel 1 according to the present invention is installed in an intake / exhaust duct of a power plant or the like.

発電用プラントや一般プラントでは、作動流体として外気を導入し、熱機関等で用いた後で排気している。外気を吸入する流路(ダクト)或いは排出する流路(ダクト)の内壁に本発明に係る吸音パネル1を設置する。この場合に、例えば既存の吸音パネルに孔空き薄膜を後付けで設置することで(図13参照)、吸音性能の改善を図ることができる。   In power generation plants and general plants, outside air is introduced as a working fluid and exhausted after being used in a heat engine or the like. The sound absorbing panel 1 according to the present invention is installed on the inner wall of a flow path (duct) for sucking outside air or a flow path (duct) for discharging air. In this case, for example, by installing a perforated thin film on an existing sound absorbing panel as a retrofit (see FIG. 13), the sound absorbing performance can be improved.

(実施例3)
部屋の壁、建物の外壁、沿線の塀に本発明に係る吸音パネル1を設置する。
(Example 3)
The sound absorbing panel 1 according to the present invention is installed on the wall of the room, the outer wall of the building, and the fence along the line.

壁面や塀に吸音パネル1を設置する。パネル1に入射する騒音を軽減して、壁周囲の騒音を吸音パネルがない場合に比べて低減する。自動車道路や鉄道路の沿線に設けた塀内面に吸音パネル1を取り付けることで、路線の騒音を抑制し、周囲環境への騒音暴露量を軽減する。   The sound absorbing panel 1 is installed on the wall or wall. The noise incident on the panel 1 is reduced, and the noise around the wall is reduced compared to the case where there is no sound absorbing panel. By installing the sound-absorbing panel 1 on the inner surface of the fence provided along the roads of automobiles and railways, the noise on the route is suppressed and the amount of noise exposure to the surrounding environment is reduced.

(実施例4)
機内、車内の内壁に本発明に係る吸音パネル1を設置する。
Example 4
The sound-absorbing panel 1 according to the present invention is installed on the interior walls of the cabin and the vehicle.

航空機の機内、車両の車室内、ロケットフェアリング内など閉空間の内壁に吸音パネル1を設置する。航空機や車両の内部は、原動機による音、気流音などが隔壁を伝搬する結果、内部の騒音が残存する。内壁に吸音パネル1を付けることで騒音を軽減することが期待され、既存の吸音パネルの効果を向上させることが見込まれる。   The sound absorbing panel 1 is installed on the inner wall of a closed space such as an aircraft cabin, a vehicle cabin, or a rocket fairing. Inside the aircraft or vehicle, noise from the prime mover, airflow sound, etc. propagates through the partition wall, resulting in internal noise remaining. It is expected to reduce noise by attaching the sound absorbing panel 1 to the inner wall, and it is expected to improve the effect of the existing sound absorbing panel.

ロケット打上時には高振幅の音源や振動源が存在し、機体を介してフェアリング内部に伝搬する。その結果、フェアリング内部のペイロードに不要な振動をもたらす。吸音パネル1の表面板20の貫通孔21に僅かな突起である突出部50をつけることで、重量増加なくフェアリング内壁の吸音量を増加させることが期待される。   When launching a rocket, there are high-amplitude sound sources and vibration sources that propagate through the aircraft into the fairing. This results in unwanted vibrations in the payload inside the fairing. It is expected that the sound absorption volume of the inner wall of the fairing can be increased without increasing the weight by attaching the protruding portion 50 that is a slight protrusion to the through hole 21 of the surface plate 20 of the sound absorbing panel 1.

以上のとおり、本発明に係る共鳴型吸音パネル1を自動車、プラント、航空機の騒音伝播経路に適用して、環境騒音の低減を図ることができる。   As described above, it is possible to reduce environmental noise by applying the resonance type sound absorbing panel 1 according to the present invention to a noise propagation path of an automobile, a plant, and an aircraft.

また、本発明に係る共鳴型吸音パネル1を交通機械の車内、機内の内壁などに適用して、客室騒音を低減し、快適性改善を図ることができる。   In addition, the resonance type sound absorbing panel 1 according to the present invention can be applied to the interior of a traffic machine, the interior wall of the cabin, etc., to reduce cabin noise and improve comfort.

更に、本発明に係る共鳴型吸音パネル1を建築物、道路などの壁面や塀に適用して、環境騒音を低減して、生活・労働環境改善を図る。   Furthermore, the resonance type sound absorbing panel 1 according to the present invention is applied to walls and walls of buildings, roads and the like to reduce environmental noise and improve the living and working environment.

また、本発明に係る共鳴型吸音パネル1をロケットフェアリングや宇宙機に適用して、機器の損傷回避を図る。   Further, the resonance type sound absorbing panel 1 according to the present invention is applied to a rocket fairing or a spacecraft to avoid damage to equipment.

<その他>
本発明は上記の実施形態に限定されず、その技術思想の範囲内で様々な変形が可能であり、その変形の範囲も本発明の技術的範囲に属する。
<Others>
The present invention is not limited to the above embodiments, and various modifications are possible within the scope of the technical idea, and the scope of the modifications also belongs to the technical scope of the present invention.

例えば、図20に示すように、突出部50は、貫通孔21の裏面側端部に設けてもよい。また、図21に示すように、突出部50は貫通孔21の表面側端部及び裏面側端部の両方に設けてもよい。   For example, as shown in FIG. 20, the protrusion 50 may be provided at the end on the back surface side of the through hole 21. Further, as shown in FIG. 21, the protrusions 50 may be provided at both the front surface side end portion and the back surface side end portion of the through hole 21.

また、図22に示すように、多層吸音パネルの中間板70に設けられた貫通孔71の表面側端部に突出部50を設けてもよい。突出部50は貫通孔71の裏面側端部に設けてもよく、貫通孔71の表面側端部及び裏面側端部の両方に設けてもよい。表面板20の貫通孔21に突出部50を設け、更に中間板70の貫通孔71に突出部50を設けてもよい。   Moreover, as shown in FIG. 22, you may provide the protrusion part 50 in the surface side edge part of the through-hole 71 provided in the intermediate board 70 of the multilayer sound-absorption panel. The protruding portion 50 may be provided at the back surface side end portion of the through hole 71, or may be provided at both the front surface side end portion and the back surface side end portion of the through hole 71. The protrusion 50 may be provided in the through hole 21 of the surface plate 20, and the protrusion 50 may be provided in the through hole 71 of the intermediate plate 70.

1 共鳴型吸音パネル
11 セル
12 隔壁
20 表面板
21 貫通孔
30 背後壁
40 セル構造
DESCRIPTION OF SYMBOLS 1 Resonant type sound absorption panel 11 Cell 12 Partition 20 Surface plate 21 Through-hole 30 Back wall 40 Cell structure

Claims (10)

セルを区画する隔壁と、前記区画されたセルの上下に設けられ、少なくとも一方に貫通孔が設けられた表面板及び背後壁とから構成されるセル構造と、
前記貫通孔の表面側端部及び裏面側端部の少なくとも一方の壁側より前記貫通孔の中心軸方向に突出し、前記貫通孔の直径の20%以下の突出長の突出部と
を具備する共鳴型吸音パネル。
A cell structure composed of a partition wall that divides a cell, and a surface plate and a back wall that are provided above and below the partitioned cell and at least one of which has a through hole;
A resonance projecting from at least one wall side of the front-side end and the back-side end of the through-hole in the direction of the central axis of the through-hole and having a protruding length of 20% or less of the diameter of the through-hole. Type sound absorbing panel.
請求項1に記載の共鳴型吸音パネルであって、
前記突出部は、前記壁側より前記貫通孔の中心軸方向に円環状に突出する
共鳴型吸音パネル。
The resonance type sound absorbing panel according to claim 1,
The projecting portion projects in an annular shape from the wall side toward the central axis of the through hole.
請求項1に記載の共鳴型吸音パネルであって、
前記突出部は、前記貫通孔の中心軸方向に沿って間隔をもって配置され、前記壁側より前記貫通孔の中心軸方向に突出する複数の突出部材から構成される
共鳴型吸音パネル。
The resonance type sound absorbing panel according to claim 1,
The said protrusion part is arrange | positioned at intervals along the central-axis direction of the said through-hole, and is comprised from the several protrusion member which protrudes in the central-axis direction of the said through-hole from the said wall side.
請求項2又は3に記載の共鳴型吸音パネルであって、
前記突出部は、前記壁側より前記貫通孔の中心軸方向になるに従い薄くなる
共鳴型吸音パネル。
The resonance type sound absorbing panel according to claim 2 or 3,
The projecting portion becomes thinner from the wall side toward the center axis direction of the through hole.
請求項2乃至4のいずれかに記載の共鳴型吸音パネルであって、
前記突出部は、前記貫通孔の軸方向のいずれか一方の方向に反りを有する
共鳴型吸音パネル。
The resonance type sound absorbing panel according to any one of claims 2 to 4,
The protrusion has a warp in any one of axial directions of the through hole.
請求項2乃至5のいずれかに記載の共鳴型吸音パネルであって、
前記突出部は、前記貫通孔内側の面が多角形状又はR形状である
共鳴型吸音パネル。
A resonance type sound absorbing panel according to any one of claims 2 to 5,
The protrusion has a polygonal shape or an R shape on the inner surface of the through hole.
請求項1乃至6のいずれかに記載の共鳴型吸音パネルであって、
前記突出部を有する円環部材を有し、
前記表面板又は背後壁の前記貫通孔の周囲に座刳りを設け、
前記座刳りに前記円環部材を嵌め込む
共鳴型吸音パネル。
The resonance type sound absorbing panel according to any one of claims 1 to 6,
An annular member having the protrusion,
Provide a countersink around the through hole in the surface plate or back wall,
A resonance type sound absorbing panel in which the annular member is fitted into the seat.
請求項1乃至6のいずれかに記載の共鳴型吸音パネルであって、
前記突出部を有する円筒部材を有し、
前記貫通孔に前記円筒部材を嵌め込む
共鳴型吸音パネル。
The resonance type sound absorbing panel according to any one of claims 1 to 6,
A cylindrical member having the protruding portion;
A resonance type sound absorbing panel in which the cylindrical member is fitted into the through hole.
請求項1乃至6のいずれかに記載の共鳴型吸音パネルであって、
前記貫通孔より穴径の小さい孔が空けられた薄いシート状の部材を有し、
前記貫通孔内に前記小さい孔が位置するように、前記表面板又は背後壁の表面に前記シート状の部材を張り付けて、前記貫通孔内に前記シート状の部材が張り出すようにして前記突出部を構成した
共鳴型吸音パネル。
The resonance type sound absorbing panel according to any one of claims 1 to 6,
A thin sheet-like member having a hole having a smaller hole diameter than the through hole is provided,
The sheet-like member is attached to the surface of the surface plate or the back wall so that the small hole is positioned in the through-hole, and the sheet-like member protrudes into the through-hole. Resonance-type sound absorbing panel.
請求項1乃至9のいずれかに記載の共鳴型吸音パネルであって、
前記突出部の厚さは、前記貫通孔の孔長の5%以下である
共鳴型吸音パネル。
A resonance type sound absorbing panel according to any one of claims 1 to 9,
The thickness of the protrusion is 5% or less of the hole length of the through hole.
JP2018020323A 2018-02-07 2018-02-07 Resonance type sound absorption panel Active JP7064236B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2018020323A JP7064236B2 (en) 2018-02-07 2018-02-07 Resonance type sound absorption panel

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2018020323A JP7064236B2 (en) 2018-02-07 2018-02-07 Resonance type sound absorption panel

Publications (2)

Publication Number Publication Date
JP2019138977A true JP2019138977A (en) 2019-08-22
JP7064236B2 JP7064236B2 (en) 2022-05-10

Family

ID=67693826

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2018020323A Active JP7064236B2 (en) 2018-02-07 2018-02-07 Resonance type sound absorption panel

Country Status (1)

Country Link
JP (1) JP7064236B2 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022091542A1 (en) 2020-10-30 2022-05-05 国立研究開発法人宇宙航空研究開発機構 Pressure fluctuation absorbing structural body

Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07210172A (en) * 1993-12-03 1995-08-11 Yamakawa Ind Co Ltd Sound absorbing wall structure
JP2005023619A (en) * 2003-07-01 2005-01-27 Nakanishi Metal Works Co Ltd Sound absorbing panel and sound absorber
JP2005031240A (en) * 2003-07-09 2005-02-03 Nakanishi Metal Works Co Ltd Panel and device for sound absorption
JP2010519103A (en) * 2007-02-20 2010-06-03 エアバス フランス Silencer processing panel
JP2017015972A (en) * 2015-07-02 2017-01-19 大成建設株式会社 Adapter for resonance frequency adjustment
JP2017151325A (en) * 2016-02-25 2017-08-31 岐阜プラスチック工業株式会社 Sound insulation panel

Patent Citations (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07210172A (en) * 1993-12-03 1995-08-11 Yamakawa Ind Co Ltd Sound absorbing wall structure
JP2005023619A (en) * 2003-07-01 2005-01-27 Nakanishi Metal Works Co Ltd Sound absorbing panel and sound absorber
JP2005031240A (en) * 2003-07-09 2005-02-03 Nakanishi Metal Works Co Ltd Panel and device for sound absorption
JP2010519103A (en) * 2007-02-20 2010-06-03 エアバス フランス Silencer processing panel
JP2017015972A (en) * 2015-07-02 2017-01-19 大成建設株式会社 Adapter for resonance frequency adjustment
JP2017151325A (en) * 2016-02-25 2017-08-31 岐阜プラスチック工業株式会社 Sound insulation panel

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
WO2022091542A1 (en) 2020-10-30 2022-05-05 国立研究開発法人宇宙航空研究開発機構 Pressure fluctuation absorbing structural body

Also Published As

Publication number Publication date
JP7064236B2 (en) 2022-05-10

Similar Documents

Publication Publication Date Title
US11915679B2 (en) Continuous degree of freedom acoustic cores
US6182787B1 (en) Rigid sandwich panel acoustic treatment
EP1714871B1 (en) Acoustic dampers
US11434826B2 (en) Acoustic treatment panel for a turbojet engine
JP2010085994A (en) Sound attenuation system
US11353240B2 (en) Low drag, variable-depth acoustic liner
US10677163B2 (en) Noise attenuation structures
JP2010526231A (en) Acoustic panel with variable acoustic characteristics
US9670878B2 (en) Cellular acoustic structure for a turbojet engine and turbojet engine incorporating at least one such structure
JP2002156978A (en) Active sound absorption panel system using movement control reflecting plate
US6766985B2 (en) Structural assembly of part of an aircraft and aircraft, particularly rotary-wing aircraft, comprising such a structural assembly
JP7064236B2 (en) Resonance type sound absorption panel
CN116806353A (en) Reduced volume acoustic treatment panel for turbojet engine
JP7475368B2 (en) Thrust reverser cascade including acoustic treatment
US20230407775A1 (en) Propulsion flow path duct systems and methods
JP2003015656A (en) Fine jet control type sound absorption system
US11472565B2 (en) Turbomachine nacelle having acoustically porous walls
US10723476B2 (en) Ring of turbojet vanes including an acoustic treatment structure
WO2022091542A1 (en) Pressure fluctuation absorbing structural body
CN104246868A (en) Thin panel for absorbing sound waves emitted by a turbofan of an aircraft nacelle, and nacelle provided with such a panel
JP7352925B2 (en) Pressure fluctuation absorption structure
CN113895098B (en) Acoustic liner, method of manufacture, powered propulsion system, and honeycomb core
US20220099022A1 (en) Noise reducing device having an obliquely pierced honeycomb structure
CN113811681B (en) Thrust reverser cascade including acoustic treatment
US10662876B2 (en) Turbomachine vane comprising an electroacoustic source with improved assembly mode, row of outlet guide vanes and turbomachine comprising such a vane

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20201214

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20211014

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20211102

A521 Request for written amendment filed

Free format text: JAPANESE INTERMEDIATE CODE: A523

Effective date: 20211124

RD02 Notification of acceptance of power of attorney

Free format text: JAPANESE INTERMEDIATE CODE: A7422

Effective date: 20211124

TRDD Decision of grant or rejection written
A01 Written decision to grant a patent or to grant a registration (utility model)

Free format text: JAPANESE INTERMEDIATE CODE: A01

Effective date: 20220412

A61 First payment of annual fees (during grant procedure)

Free format text: JAPANESE INTERMEDIATE CODE: A61

Effective date: 20220415

R150 Certificate of patent or registration of utility model

Ref document number: 7064236

Country of ref document: JP

Free format text: JAPANESE INTERMEDIATE CODE: R150