JP3007766B2 - Mixed flow fan - Google Patents

Mixed flow fan

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Publication number
JP3007766B2
JP3007766B2 JP5091119A JP9111993A JP3007766B2 JP 3007766 B2 JP3007766 B2 JP 3007766B2 JP 5091119 A JP5091119 A JP 5091119A JP 9111993 A JP9111993 A JP 9111993A JP 3007766 B2 JP3007766 B2 JP 3007766B2
Authority
JP
Japan
Prior art keywords
blade
outlet
flow fan
inlet
mixed flow
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.)
Expired - Fee Related
Application number
JP5091119A
Other languages
Japanese (ja)
Other versions
JPH06299998A (en
Inventor
務 加藤
和郎 荻野
Original Assignee
松下精工株式会社
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Publication date
Application filed by 松下精工株式会社 filed Critical 松下精工株式会社
Priority to JP5091119A priority Critical patent/JP3007766B2/en
Publication of JPH06299998A publication Critical patent/JPH06299998A/en
Application granted granted Critical
Publication of JP3007766B2 publication Critical patent/JP3007766B2/en
Anticipated expiration legal-status Critical
Expired - Fee Related legal-status Critical Current

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Description

【発明の詳細な説明】DETAILED DESCRIPTION OF THE INVENTION

【0001】[0001]

【産業上の利用分野】本発明は、排気送風機器および空
気調和機器に使用される斜流ファンに関する。
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a mixed flow fan used for an exhaust blower and an air conditioner.

【0002】[0002]

【従来の技術】近年、居住および非居住空間で使用され
る排気送風機器および空気調和機器は運転時に発生する
騒音を低下することが求められている。
2. Description of the Related Art In recent years, it is required that exhaust air blowers and air conditioners used in living and non-living spaces reduce noise generated during operation.

【0003】従来、この種の斜流ファンは、図6に示す
ものが一般的であった。以下、その構成について図を参
照しながら説明する。
Conventionally, this kind of mixed flow fan is generally shown in FIG. Hereinafter, the configuration will be described with reference to the drawings.

【0004】図に示すように、複数枚の動翼羽根101
を略円錐台形のハブ102に取り付けた動翼が、外周縁
103に沿った環状のケーシング112に周方向におい
て一定のクリアランスを保ちながら配置されている。そ
して、前記動翼羽根101の根元部104から前記外周
縁103に行くにしたがって翼弦の中心を回転方向に前
進させた動翼羽根101の形状を有している。また、動
翼羽根101の下流にケーシング112とケーシング1
12内の内筒113の間に、内筒113を支持するよう
に静翼羽根108が配置されている。
As shown in FIG. 1, a plurality of blades 101
Are attached to an annular casing 112 along the outer peripheral edge 103 while maintaining a constant clearance in the circumferential direction. The blade 101 has a shape in which the center of the chord is advanced in the rotation direction from the root portion 104 of the blade 101 toward the outer peripheral edge 103. Further, the casing 112 and the casing 1 are provided downstream of the rotor blade 101.
The stationary blades 108 are arranged between the inner cylinders 113 in the inner tube 12 so as to support the inner cylinder 113.

【0005】上記構成において斜流ファンが回転したと
きの一般的な通風方向は、斜流ファンを介して通風され
ることになる。
[0005] In the above configuration, the general ventilation direction when the mixed flow fan rotates is that air is passed through the mixed flow fan.

【0006】[0006]

【発明が解決しようとする課題】このような従来の斜流
ファンでは、翼面上の空気の流れが前縁から後縁に向か
う際、理論と完全に一致して流体が流れないため動翼羽
根101に沿わない流れとなる場合がある。また流体の
粘性により表面近くで減速されることにより羽根の負圧
面では剥離が生じやすいという問題があり、しかも動翼
羽根101の回転による回転騒音が生じると言う問題が
あった。また、流体がハブ102に衝突する際の乱れも
騒音を増大する原因の一つである。
In such a conventional mixed flow fan, when the air flows on the blade surface from the leading edge to the trailing edge, the fluid does not flow completely in accordance with the theory, so that the moving blade There is a case where the flow does not follow the blade 101. In addition, there is a problem that separation is likely to occur on the negative pressure surface of the blade due to deceleration near the surface due to the viscosity of the fluid, and furthermore, there is a problem that rotation noise is generated due to rotation of the moving blade 101. Also, turbulence when the fluid collides with the hub 102 is one of the causes for increasing noise.

【0007】本発明は上記課題を解決するもので、運転
時に発生する騒音の低下をさせることを第1の目的とす
る。
[0007] The present invention has been made to solve the above problems, and has as its first object to reduce noise generated during operation.

【0008】第2の目的は、風量を増大させ、効率を向
上することにある。
A second object is to increase the air flow and improve the efficiency.

【0009】[0009]

【課題を解決するための手段】本発明の斜流ファンは上
記第1の目的を達成するために第1の手段は、ハブの外
周に複数枚の動翼羽根を備え、前記動翼羽根の形状にお
いて入口外径をD2i、出口外径をD2oとしたとき、
D2i/D2oが0.85〜0.9の範囲であり、入口
内径をD1i、出口内径D1oとしたとき、D1i/D
1oが0.45〜0.55の範囲であり、かつ前記動翼
羽根の回転中心軸の方向での幅をLとしたとき、L/D
2oが0.28〜0.3の範囲であり、かつ前記動翼羽
根の内周縁の回転中心軸となす取付角の平均が52°〜
55°の範囲である構成をしている。
In order to achieve the first object, a mixed flow fan according to the present invention comprises a plurality of moving blades on an outer periphery of a hub. When the inlet outer diameter is D2i and the outlet outer diameter is D2o in the shape,
When D2i / D2o is in the range of 0.85 to 0.9 and the inlet inner diameter is D1i and the outlet inner diameter is D1o, D1i / D
When 1o is in the range of 0.45 to 0.55 and the width of the moving blade in the direction of the rotation center axis is L, L / D
2o is in the range of 0.28 to 0.3, and the average of the mounting angles with the rotation center axis of the inner peripheral edge of the bucket blade is 52 ° to
It is configured to have a range of 55 °.

【0010】また、第1の目的および第2の目的を達成
するために第2の手段は、動翼羽根の形状において内周
縁及び外周縁での取付角の差が3°〜10°の範囲であ
り、羽根を回転中心軸の方向から見て外径が最大となる
点の羽根間のピッチ角をθt、最大となる前記外周縁の
両端点が前記回転中心軸と半径方向の断面においてなす
角をθsとしたとき、θs/θtが0.94である構成
をしている。
In order to achieve the first object and the second object, the second means is that the difference in the mounting angle between the inner peripheral edge and the outer peripheral edge in the shape of the moving blade is in the range of 3 ° to 10 °. When the blades are viewed from the direction of the rotation center axis, the pitch angle between the blades at the point where the outer diameter becomes the maximum is θt, and both end points of the outer peripheral edge that make the maximum are formed in the radial cross section with the rotation center axis. When the angle is θs, θs / θt is 0.94.

【0011】また、第1の目的を達成するために第3の
手段は、ハブの入口径をD3i、出口径をD3oとした
とき、D3i/D3oが0.4〜0.43の範囲であ
り、流線型形状を持つ構成をしている。
A third means for achieving the first object is that when the inlet diameter of the hub is D3i and the outlet diameter is D3o, D3i / D3o is in the range of 0.4 to 0.43. , And has a streamlined configuration.

【0012】また、第1の目的を達成するために第4の
手段は、動翼羽根の下流にあり、ケーシングとこのケー
シング内にある略円錐台形の内筒との間にあり、前記内
筒を支持する静翼羽根の半径方向の断面での入口面積を
Si、出口面積をSoとしたとき、So/Siが1.2
〜1.4の範囲であり、前記静翼羽根の入口部の速度を
Vi、前記静翼羽根の出口部の速度をVoとしたとき、
前記静翼羽根の入口部から前記静翼羽根の出口部までの
流体速度比Vo/Viが0.9以下となる構成をしてい
る。
In order to achieve the first object, a fourth means is provided downstream of the moving blade, between the casing and the substantially frustoconical inner cylinder in the casing, When the inlet area and the outlet area in the radial cross section of the stator vane blade that supports
When the speed at the inlet of the stator blade is Vi and the speed at the outlet of the stator blade is Vo,
The fluid velocity ratio Vo / Vi from the inlet of the stationary blade to the outlet of the stationary blade is 0.9 or less.

【0013】[0013]

【作用】本発明は上記した第1の手段の構成により、翼
面上に流れる流体を急激に増速させることなく円滑に導
くことが出来るため、翼面での剥離を少なくすることが
できる。
According to the first aspect of the present invention, the fluid flowing on the wing surface can be smoothly guided without abruptly increasing the speed, so that separation on the wing surface can be reduced.

【0014】また、第2の手段の構成により、翼面上で
は強制渦流れを仮定することで、羽根外周部での仕事量
を増やし、風量を増加すると共に翼面上に流れる流体を
滑らかに流して騒音を増加させないことができる。
According to the configuration of the second means, by assuming a forced vortex flow on the blade surface, the amount of work at the outer periphery of the blade is increased, the air flow is increased, and the fluid flowing on the blade surface is smoothed. The noise can not be increased by flowing.

【0015】また、第3の手段の構成により、ハブに衝
突する空気乱れを減少させることができる。
[0015] Further, according to the configuration of the third means, air turbulence colliding with the hub can be reduced.

【0016】また、第4の手段の構成により、動翼羽根
より流れてきた流体を乱すことなく軸と平行な状態に安
定させると共に、旋回成分を排除し管路抵抗を減少させ
ることができる。
In addition, the configuration of the fourth means makes it possible to stabilize the fluid flowing from the rotor blades in a state parallel to the axis without disturbing the fluid, to eliminate a swirl component, and to reduce the pipeline resistance.

【0017】[0017]

【実施例】以下、本発明の第1実施例について、図1を
参照しながら説明する。
DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS A first embodiment of the present invention will be described below with reference to FIG.

【0018】図に示すように、ハブ2の外周に複数枚の
動翼羽根1を備え、取付角の平均をθ、出口外径をD2
o、入口外径をD2i、出口内径をD1o、入口内径を
D1i、動翼羽根1の軸方向の幅をLとしたとき、θが
52°〜55°の範囲であり、D2i/D2oが0.8
5〜0.9の範囲であり、D1i/D1oが0.45〜
0.55の範囲であり、L/D2oが0.28〜0.3
の範囲で構成されている。
As shown in the figure, a plurality of rotor blades 1 are provided on the outer periphery of a hub 2, the average of the mounting angles is θ, and the outer diameter of the outlet is D2.
o, when the inlet outer diameter is D2i, the outlet inner diameter is D1o, the inlet inner diameter is D1i, and the axial width of the moving blade 1 is L, θ is in the range of 52 ° to 55 °, and D2i / D2o is 0. .8
5 to 0.9, and D1i / D1o is 0.45 to
0.55, and L / D2o is 0.28 to 0.3.
It consists of the range.

【0019】上記構成により、動翼羽根1が回転動作時
に翼面上の流れを、急激に増速することなく滑らかに流
すことができ、騒音を低減できる。
With the above configuration, the moving blade 1 can smoothly flow the flow on the blade surface during the rotating operation without abruptly increasing the speed, thereby reducing noise.

【0020】つぎに本発明の第2実施例について図2〜
図3を参照しながら説明する。なお、第1実施例と同一
箇所には同一番号を付けて詳細な説明は省略する。
Next, a second embodiment of the present invention will be described with reference to FIGS.
This will be described with reference to FIG. The same parts as those in the first embodiment are denoted by the same reference numerals, and detailed description is omitted.

【0021】図に示すように、第1実施例の構成に内周
縁4と外周縁3での取付角の平均値の差が3°〜10°
の範囲であり、羽根間のピッチ角をθt、外周縁の両端
点がなす角θsとしたとき、θs/θtが0.94とし
た形で構成されている。
As shown in the drawing, the difference between the average values of the mounting angles at the inner peripheral edge 4 and the outer peripheral edge 3 is 3 ° to 10 ° in the configuration of the first embodiment.
Where θt is the pitch angle between the blades and θs is the angle formed between both ends of the outer peripheral edge, and θs / θt is 0.94.

【0022】上記構成により、動翼羽根1が回転動作時
に外周縁3近くの部分の仕事量が増えるため風量が増加
し、しかも動翼羽根1のそりが少ない形状としているた
め、負圧面10の流体を滑らかに流すことができる。ま
た正圧面11の外周部3の流体を確実に仕事させるため
動翼羽根1の途中の負圧面10への流体巻き込みも生じ
ない。
With the above configuration, the work volume of the portion near the outer peripheral edge 3 increases during the rotating operation of the moving blade 1, so that the air volume increases, and the moving surface of the moving blade 1 is less warped. Fluid can flow smoothly. Further, since the fluid on the outer peripheral portion 3 of the positive pressure surface 11 is made to work reliably, no fluid is entrapped on the negative pressure surface 10 in the middle of the moving blade 1.

【0023】つぎに本発明の第3実施例について図4を
参照しながら説明する。なお、第1実施例と同一箇所に
は同一番号を付けて詳細な説明は省略する。
Next, a third embodiment of the present invention will be described with reference to FIG. The same parts as those in the first embodiment are denoted by the same reference numerals, and detailed description is omitted.

【0024】図に示すように、第1実施例および第2実
施例の構成にハブ2の入口径をD3i、ハブ2の出口径
をD3oとすると、D3i/D3oが0.4〜0.43
とした形で構成されている。
As shown in the drawing, if the inlet diameter of the hub 2 is D3i and the outlet diameter of the hub 2 is D3o in the structure of the first and second embodiments, D3i / D3o is 0.4 to 0.43.
It is composed in the form.

【0025】上記構成により、動翼羽根1が回転動作時
にハブ2に衝突する流体を滑らかに流すことができる。
またハブ2の表面上に流れる流体も剥離しにくい。
According to the above configuration, the fluid that collides with the hub 2 during the rotating operation of the bucket blade 1 can be made to flow smoothly.
Further, the fluid flowing on the surface of the hub 2 is not easily separated.

【0026】つぎに本発明の第4実施例について図5を
参照しながら説明する。なお、第1実施例と同一箇所に
は同一番号を付けて詳細な説明は省略する。
Next, a fourth embodiment of the present invention will be described with reference to FIG. The same parts as those in the first embodiment are denoted by the same reference numerals, and detailed description is omitted.

【0027】図に示すように、第1実施例および第2実
施例および第3実施例の構成にケーシング12とケーシ
ング12内の内筒13との間に設置している静翼羽根8
の半径方向の断面での出口面積をSo、入口面積をSi
としたとき、So/Siが1.2〜1.4の範囲であ
り、入口部の速度をVi、出口部の速度をVoとしたと
き、入口部から出口部までの流体速度比Vo/Viが
0.9以下となるように構成されている。
As shown in the drawing, the stationary blade 8 installed between the casing 12 and the inner cylinder 13 in the casing 12 has the structure of the first, second, and third embodiments.
The exit area at the radial cross section is So, and the entrance area is Si
Where So / Si is in the range of 1.2 to 1.4, and when the speed of the inlet portion is Vi and the speed of the outlet portion is Vo, the fluid speed ratio Vo / Vi from the inlet portion to the outlet portion. Is 0.9 or less.

【0028】上記構成により、動翼羽根1より流れてき
た流体を乱すことなく回転中心軸9と平行な状態に安定
させると共に、静翼羽根8の出口に流体が放出される際
に旋回成分を排除し管路抵抗を減少できる。
With the above configuration, the fluid flowing from the moving blade 1 is stabilized without being disturbed in a state parallel to the rotation center axis 9, and a swirl component is generated when the fluid is discharged to the outlet of the stationary blade 8. Elimination can reduce pipeline resistance.

【0029】[0029]

【発明の効果】以上のように実施例から明らかなよう
に、本発明によれば動翼羽根の面およびハブの面上およ
び静翼羽根の出口に流れる流体を急激に増速させること
なく円滑に導くことができ、剥離を少なくすることがで
き、騒音を増加させない斜流ファンが提供できる。
As is apparent from the embodiments, as described above, according to the present invention, the fluid flowing on the surface of the moving blade and the surface of the hub and at the outlet of the stationary blade is smoothly increased without abrupt increase in speed. Can be provided, a separation can be reduced, and a mixed flow fan which does not increase noise can be provided.

【0030】また、動翼羽根の外周部の仕事量を増や
し、風量を増大させる斜流ファンが提供できる。
Further, it is possible to provide a mixed flow fan that increases the amount of work on the outer peripheral portion of the moving blade and increases the air flow.

【図面の簡単な説明】[Brief description of the drawings]

【図1】本発明の第1実施例の斜流ファンの側断面図FIG. 1 is a side sectional view of a mixed flow fan according to a first embodiment of the present invention.

【図2】同第2実施例の斜流ファンの側断面図FIG. 2 is a side sectional view of the mixed flow fan according to the second embodiment.

【図3】同正面図FIG. 3 is a front view of the same.

【図4】同第3実施例の斜流ファンの側断面図FIG. 4 is a side sectional view of the mixed flow fan according to the third embodiment.

【図5】同第4実施例の斜流ファンの側断面図FIG. 5 is a side sectional view of the mixed flow fan according to the fourth embodiment.

【図6】従来の斜流ファンの側断面図FIG. 6 is a side sectional view of a conventional mixed flow fan.

【符号の説明】[Explanation of symbols]

1 動翼羽根 2 ハブ 3 外周縁 4 内周縁 8 静翼羽根 9 回転中心軸 12 ケーシング 13 内筒 REFERENCE SIGNS LIST 1 rotor blade 2 hub 3 outer peripheral edge 4 inner peripheral edge 8 stator blade 9 rotating center axis 12 casing 13 inner cylinder

───────────────────────────────────────────────────── フロントページの続き (56)参考文献 特開 平2−136597(JP,A) 特開 平1−118000(JP,A) 実開 昭54−167807(JP,U) 実開 昭56−20100(JP,U) 実開 昭54−101506(JP,U) (58)調査した分野(Int.Cl.7,DB名) F04D 29/18 - 29/38 F04D 23/00 F04D 11/00 101 ──────────────────────────────────────────────────続 き Continuation of the front page (56) References JP-A-2-136597 (JP, A) JP-A-1-118000 (JP, A) Fully open 1979-167807 (JP, U) Fully open 1979 20100 (JP, U) Actually open 1979-101506 (JP, U) (58) Fields investigated (Int. Cl. 7 , DB name) F04D 29/18-29/38 F04D 23/00 F04D 11/00 101

Claims (4)

(57)【特許請求の範囲】(57) [Claims] 【請求項1】 ハブの外周に複数枚の動翼羽根を備え、
前記動翼羽根の形状において入口外径をD2i、出口外
径をD2oとしたとき、D2i/D2oが0.85〜
0.9の範囲であり、入口内径をD1i、出口内径をD
1oとしたとき、D1i/D1oが0.45〜0.55
の範囲であり、かつ前記動翼羽根の回転中心軸の方向で
の幅をLとしたとき、L/D1oが0.28〜0.3の
範囲であり、かつ前記動翼羽根の内周縁の前記回転中心
軸となす取付角の平均が52°〜55°の範囲であるこ
とを特徴とする斜流ファン。
A plurality of rotor blades provided on an outer periphery of a hub;
When the inlet outer diameter is D2i and the outlet outer diameter is D2o in the shape of the bucket blade, D2i / D2o is 0.85 to 0.85.
0.9, the inner diameter of the inlet is D1i, and the inner diameter of the outlet is D1i.
When 1o, D1i / D1o is 0.45 to 0.55
And L / D1o is in the range of 0.28 to 0.3, and L / D1o is in the range of 0.28 to 0.3, and the width of the inner peripheral edge of the blade is A mixed flow fan characterized in that the average of the mounting angle with the rotation center axis is in the range of 52 ° to 55 °.
【請求項2】 動翼羽根の形状において内周縁及び外周
縁での回転中心軸となす各々の取付角の差が3°〜10
°の範囲であり、前記動翼羽根を回転中心軸の方向から
見て外径が最大となる点の前記動翼羽根の間のピッチ角
をθt、最大となる前記外周縁の両端点が前記回転中心
軸と半径方向の断面においてなす角をθsとしたとき、
θs/θtが0.94であることを特徴とする請求項1
記載の斜流ファン。
2. A difference in mounting angle between a rotation center axis at an inner peripheral edge and an outer peripheral edge in a shape of a rotor blade is 3 ° to 10 °.
°, the pitch angle between the moving blades at the point where the outer diameter is maximum when the moving blades are viewed from the direction of the rotation center axis is θt, and both end points of the outer peripheral edge that are the maximum are When the angle between the rotation center axis and the cross section in the radial direction is θs,
2. The method according to claim 1, wherein θs / θt is 0.94.
Mixed flow fan as described.
【請求項3】 ハブの入口径をD3i、出口径をD3o
としたとき、D3i/D3oが0.4〜0.43の範囲
であり、流線型形状を持つことを特徴とする請求項1ま
たは請求項2記載の斜流ファン。
3. The hub has an inlet diameter of D3i and an outlet diameter of D3o.
The mixed flow fan according to claim 1 or 2, wherein D3i / D3o is in a range of 0.4 to 0.43, and has a streamlined shape.
【請求項4】 動翼羽根の下流にあり、ケーシングとこ
のケーシング内にある略円錐台形の内筒との間にあり、
前記内筒を支持する静翼羽根の半径方向の断面での入口
面積をSi、出口面積をSoとしたとき、So/Siが
1.2〜1.4の範囲であり、前記静翼羽根の入口部の
速度をVi、前記静翼羽根の出口部の速度をVoとした
とき、前記静翼羽根の入口部から前記静翼羽根の出口部
までの流体速度比Vo/Viが0.9以下となることを
特徴とする請求項1または請求項2または請求項3記載
の斜流ファン。
4. A downstream of the bucket blade, between the casing and a substantially frustoconical inner cylinder within the casing,
When the inlet area of the stator blade supporting the inner cylinder in the radial cross section is Si and the outlet area is So, So / Si is in the range of 1.2 to 1.4. Assuming that the speed of the inlet portion is Vi and the speed of the outlet portion of the stator blade is Vo, the fluid velocity ratio Vo / Vi from the inlet portion of the stator blade to the outlet portion of the stator blade is 0.9 or less. The mixed flow fan according to claim 1, 2 or 3, wherein
JP5091119A 1993-04-19 1993-04-19 Mixed flow fan Expired - Fee Related JP3007766B2 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP5091119A JP3007766B2 (en) 1993-04-19 1993-04-19 Mixed flow fan

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP5091119A JP3007766B2 (en) 1993-04-19 1993-04-19 Mixed flow fan

Publications (2)

Publication Number Publication Date
JPH06299998A JPH06299998A (en) 1994-10-25
JP3007766B2 true JP3007766B2 (en) 2000-02-07

Family

ID=14017641

Family Applications (1)

Application Number Title Priority Date Filing Date
JP5091119A Expired - Fee Related JP3007766B2 (en) 1993-04-19 1993-04-19 Mixed flow fan

Country Status (1)

Country Link
JP (1) JP3007766B2 (en)

Cited By (4)

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Publication number Priority date Publication date Assignee Title
US8557877B2 (en) 2009-06-10 2013-10-15 Honeywell International Inc. Anti-reflective coatings for optically transparent substrates
US8642246B2 (en) 2007-02-26 2014-02-04 Honeywell International Inc. Compositions, coatings and films for tri-layer patterning applications and methods of preparation thereof
US8864898B2 (en) 2011-05-31 2014-10-21 Honeywell International Inc. Coating formulations for optical elements
US8992806B2 (en) 2003-11-18 2015-03-31 Honeywell International Inc. Antireflective coatings for via fill and photolithography applications and methods of preparation thereof

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Publication number Priority date Publication date Assignee Title
KR100765195B1 (en) * 2006-04-10 2007-10-09 삼성전자주식회사 Diffuser

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US8992806B2 (en) 2003-11-18 2015-03-31 Honeywell International Inc. Antireflective coatings for via fill and photolithography applications and methods of preparation thereof
US8642246B2 (en) 2007-02-26 2014-02-04 Honeywell International Inc. Compositions, coatings and films for tri-layer patterning applications and methods of preparation thereof
US8557877B2 (en) 2009-06-10 2013-10-15 Honeywell International Inc. Anti-reflective coatings for optically transparent substrates
US8784985B2 (en) 2009-06-10 2014-07-22 Honeywell International Inc. Anti-reflective coatings for optically transparent substrates
US8864898B2 (en) 2011-05-31 2014-10-21 Honeywell International Inc. Coating formulations for optical elements

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