JP2004214095A - Airway beacon light - Google Patents

Airway beacon light Download PDF

Info

Publication number
JP2004214095A
JP2004214095A JP2003001436A JP2003001436A JP2004214095A JP 2004214095 A JP2004214095 A JP 2004214095A JP 2003001436 A JP2003001436 A JP 2003001436A JP 2003001436 A JP2003001436 A JP 2003001436A JP 2004214095 A JP2004214095 A JP 2004214095A
Authority
JP
Japan
Prior art keywords
light
phosphor
ultraviolet
prism
lamp body
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.)
Pending
Application number
JP2003001436A
Other languages
Japanese (ja)
Inventor
Yasushi Ishida
康史 石田
Katsuyuki Ide
勝幸 井手
Junji Hasegawa
潤治 長谷川
Atsuya Murata
淳哉 村田
Shingo Shinno
真吾 新野
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.)
Toshiba Lighting and Technology Corp
Original Assignee
Toshiba Lighting and Technology Corp
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 Toshiba Lighting and Technology Corp filed Critical Toshiba Lighting and Technology Corp
Priority to JP2003001436A priority Critical patent/JP2004214095A/en
Publication of JP2004214095A publication Critical patent/JP2004214095A/en
Pending legal-status Critical Current

Links

Images

Abstract

<P>PROBLEM TO BE SOLVED: To provide an airway beacon light capable of assuring a predetermined brightness and light distribution, even if the projecting height from ground is limited. <P>SOLUTION: The light body 14 is mounted on a base embedded in the ground, and a part of the light body 14 is projecting from the ground. Inside the light body 14, an ultraviolet light LED 15 for emitting ultraviolet light is housed, and a phosphor 17 to which ultraviolet light is radiated from the ultraviolet light LED 15 is attached to a prism 16. When the ultraviolet light from the ultraviolet LED 15 is radiated to the phosphor 17, the phosphor 17 emits from the light body 14 through the prism 16 a light having a narrow vertical width in the elevation direction and a wide horizontal width in right and left direction, allowing a certain brightness and light distribution to be assured even if the projecting height from the ground is limited. <P>COPYRIGHT: (C)2004,JPO&NCIPI

Description

【0001】
【発明の属する技術分野】本発明は、空港における滑走路や誘導路に埋め込まれて通行区分等を表示する埋込型の航空標識灯に関する。
【0002】
【従来の技術】埋込型の航空標識灯は空港の滑走路や誘導路に基台を形成し、その基台に灯体を装着して使用される。基台は地中に位置するように形成される。通常、基台と灯体との間には調整リングが設けられ、調整リングで灯体の設置の方向を調整するようにしている。埋込深さに制限がある場合には、基台に直接的に灯体が設置される場合もある。
【0003】
このような航空標識灯では、地表面には基台に設けられた調整リングや灯体の上面が露出し、複数個の航空標識灯の群列を空港の滑走路や誘導路に設置し、所定の明るさで点灯して、航空機の離発着および走行に視覚ガイダンスを与える。
【0004】
灯体の発光部にはハロゲン電球やLEDが用いられプリズムを介して地表面を照射するようにしている。
【0005】
一方、発光部としては紫外線LEDを用いた面発光LED光源があり、反射体に被着した蛍光体に紫外線LEDから紫外線を照射し、均一で発光強度が強く紫外線LEDを使用した場合でも紫外線の漏れが生じないようにしたものがある(例えば特許文献1参照)。
【0006】
【特許文献1】特開2001−243821号公報(図1)
【0007】
【発明が解決しようとする課題】ところが、航空標識灯においては、地面に埋設されて使用されるため、地面からの突出高さに制限がある場合が考えられる。この場合、発光部の大きさは比較的小さくする必要があり、地表面を適正に照射するために方向性を持ってハロゲン電球やLEDを配列させるには困難を伴うことがある。すなわち、直接的にプリズムに向かってハロゲン電球を配置することができなくなったり、直接的にプリズムに向かってLEDを配列させると有効に使用できるLEDの数が制限され、所定の明るさが得られない場合がある。
【0008】
本発明の目的は、地面からの突出高さに制限がある場合であっても所定の明るさおよび配光を確保できる航空標識灯を提供するものである。
【0009】
【課題を解決するための手段】請求項1の発明に係る航空標識灯は、路中に埋設された基台に取り付けられ一部が路面から突出するように設けられる灯体と;前記灯体の内部に収納され紫外線を出力する紫外線LEDと;前記紫外線LEDからの紫外線が照射されるにように配置され、その照射面側に蛍光体が被着され、蛍光体によって変換された可視光を外部に放射するように設けられたプリズムと;を備えたことを特徴とする。
【0010】
本発明および以下の発明において、特に指定しない限り用語の定義および技術的意味は以下による。
【0011】
航空標識灯は、例えば高強度アルミニウム合金鋳物で成形した灯体を有し、路中に埋設された基台に直接または調整リングを介して灯体のフランジ部で灯体全体を支持し装着される。灯体の内部には発光部が設けられる。発光部は、紫外線LEDとプリズムに被着された蛍光体とから形成され、発光部からの光は灯体の上部に設けられたプリズムを通して外部に出射される。蛍光体は紫外線LEDからの紫外線が照射されるプリズムの入射面側に被着され、紫外線LEDからの紫外線が蛍光体に照射されると蛍光体が発光する。プリズムは蛍光体で発光した光を仰角方向には上下幅が狭く水平な左右には幅広い光に偏光して灯体の外部に放射する。
【0012】
本発明によれば、外部に照射される光は蛍光体から発光するので紫外線LEDの配置に方向性を考慮する必要がなくなる。従って、灯体の突出高さに制限があり灯体の内部が狭い空間であっても所定個数の紫外線LEDを配置できるので、所定の明るさを確保できる。
【0013】
請求項2の発明に係る航空標識灯は、路中に埋設された基台に取り付けられ一部が路面から突出するように設けられる灯体と;前記灯体の内部に収納され紫外線を出力する紫外線LEDと;前記紫外線LEDの紫外線が照射される前記灯体内部の内面に被着された蛍光体と;前記蛍光体によって変換された可視光を外部に放射するプリズムと;を備えたことを特徴とする。
【0014】
本発明は、請求項1の発明に対し、蛍光体をプリズムの入射面側に代えて、紫外線LEDの紫外線が照射される灯体内部の内面に被着するようにしたものである。本発明によれば、光の発光する位置が灯体内部の内面となるがその発光はプリズムの出射角度で調整され外部に放射されるので、請求項1と同様な効果が得られる。
【0015】
【発明の実施の形態】
図1は、本発明の実施の形態に係る航空標識灯11の説明図であり、図1(a)は航空標識灯11の平面図、図1(b)は灯体の一部切り欠き断面図である。図示省略の基台は空港の滑走路や誘導路の路中に形成され、その基台の上部に調整リング12a、12bがボルト13aで装着される。そして、その調整リング12aの上部に灯体14がボルト13bで装着される。
【0016】
灯体14の内部には紫外線LED15が設けられ、また、灯体14の上部には外部に光を放射するプリズム16が設けられている。さらに、プリズム16の紫外線LED15からの紫外線が照射される入射面側には蛍光体17が被着され、紫外線LED15からの紫外線が蛍光体17に照射されると蛍光体17が発光する。蛍光体17で発光した光はプリズム16を通って、仰角方向には上下幅が狭く水平な左右には幅広い光に偏光して灯体14の外部に放射され、滑走路や誘導路の路面を照明する。
【0017】
一般に、航空標識灯においては発光部にはプリズム16を備えており、灯体14内部の地面下に位置させた光源からの発光をプリズム16の出射角度で調整するようにしている。これは、プリズム16を使用することで地面からの突出高さを低くすることを可能とするためである。そこで、本発明の実施の形態では、このプリズム16の入射面側に蛍光体17を被着し、光源を紫外線LED15とする。そして、光の発光は蛍光体17で発光させ、光源である紫外線LED15の配置位置によらず外部に照射される光の方向性を確保する。
【0018】
また、蛍光体17は、紫外線の照射により赤色光を発する蛍光体R、緑色光を発光する蛍光体G、青色光を発光する蛍光体Bのうち、一つまたは複数を混合させたものを使用する。蛍光体Rは例えばピーク波長が619nmのYVO:Eu、Biを使用し、蛍光体Gは例えばピーク波長が543nmのYSiOCe、Tbを使用し、蛍光体Bは例えばピーク波長が450nmのBaMgAl1627:Euを使用する。これらを適宜混合することにより各種の発光色を得ることができる。
【0019】
以上の説明では、蛍光体17をプリズム16の入射面側に被着したが、紫外線LED15の紫外線が照射される灯体内部の内面に被着するようにしてもよい。
【0020】
この場合は、光の発光する位置が灯体14の内部の内面となるが、その発光はプリズム16の出射角度で調整されるので、外部に放射される光は所定の方向性を保つことができる。
【0021】
以上述べたように、本発明の実施の形態によれば、外部に照射される光は蛍光体17から発光するので紫外線LED15の配置に方向性を考慮する必要がなく、紫外線LED15をプリズム16の入射面に対し対向させずとも良い。従って、光源としての紫外線LED15の数を入射面以上の投影面積に対して設けることができる。
【0022】
また、蛍光体を適宜選択することにより各種の発光色の光を持つ航空標識灯を提供できる。すなわち、蛍光体の種類を変え、外部に放射される光を所望の発光色とすることができる。例えば、紫外線の照射により赤色光を発する蛍光体R、緑色光を発光する蛍光体G、青色光を発光する蛍光体Bのうち、一つまたは複数を混合させたものを使用する。これにより、航空標識灯の使用目的に応じて適宜適切な発光色を選択することができる。
【0023】
【発明の効果】
請求項1の発明によれば、外部に照射される光は蛍光体から発光するので紫外線LEDの配置に方向性を考慮する必要がなくなり、灯体の突出高さに制限があり灯体の内部が狭い空間であっても所定個数の紫外線LEDを配置できる。従って、所定の明るさを確保できる。
【0024】
請求項2の発明によれば、光の発光する位置は灯体内部の内面となるがその発光はプリズムの出射角度で調整され外部に放射されるので、請求項1と同様な効果が得られる。
【図面の簡単な説明】
【図1】図1は、本発明の実施の形態に係る航空標識灯の説明図。
【符号の説明】
11…航空標識灯、12…調整リング、13…ボルト、14…灯体、15…紫外線LED、16…プリズム、17…蛍光体
[0001]
BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to an embedded type of aeronautical traffic light which is embedded in a runway or a taxiway at an airport and displays a traffic division or the like.
[0002]
2. Description of the Related Art Recessed aerial beacon lights are used by forming a base on a runway or taxiway of an airport and mounting a light body on the base. The base is formed to be located underground. Usually, an adjustment ring is provided between the base and the lamp, and the direction of installation of the lamp is adjusted by the adjustment ring. If the embedding depth is limited, a lamp may be directly installed on the base.
[0003]
In such an aerial beacon light, an adjustment ring or a light body provided on a base is exposed on the ground surface, and a group of a plurality of aerial beacon lights is installed on an airport runway or taxiway, Lights up at a predetermined brightness to provide visual guidance for taking off, landing and traveling of the aircraft.
[0004]
Halogen bulbs or LEDs are used for the light emitting portion of the lamp body, and the ground surface is illuminated via a prism.
[0005]
On the other hand, as a light emitting unit, there is a surface emitting LED light source using an ultraviolet LED, and a phosphor attached to a reflector is irradiated with ultraviolet light from the ultraviolet LED. There is one that does not cause leakage (for example, see Patent Document 1).
[0006]
[Patent Document 1] Japanese Patent Application Laid-Open No. 2001-243821 (FIG. 1)
[0007]
However, in the case of an aerial sign lamp, since it is used buried in the ground, there may be a case where the height of protrusion from the ground is limited. In this case, the size of the light emitting unit needs to be relatively small, and it may be difficult to arrange the halogen bulbs or LEDs with directionality in order to properly irradiate the ground surface. In other words, the halogen bulb cannot be arranged directly toward the prism, or if LEDs are arranged directly toward the prism, the number of LEDs that can be used effectively is limited, and a predetermined brightness can be obtained. May not be.
[0008]
SUMMARY OF THE INVENTION An object of the present invention is to provide an aeronautical beacon light capable of securing a predetermined brightness and light distribution even when the height of the protrusion from the ground is limited.
[0009]
According to a first aspect of the present invention, there is provided an aeronautical signage lamp which is mounted on a base buried in a road and partially provided so as to protrude from a road surface; A UV LED housed inside the LED and outputting UV light; a UV light which is disposed so as to be irradiated with the UV light from the UV LED; And a prism provided to radiate to the outside.
[0010]
In the present invention and the following inventions, definitions and technical meanings of terms are as follows unless otherwise specified.
[0011]
An aerial sign lamp has a lamp body formed of, for example, a high-strength aluminum alloy casting, and is mounted on a base buried in the road by directly supporting the entire lamp body at a flange portion of the lamp body or via an adjustment ring. You. A light emitting unit is provided inside the lamp body. The light emitting section is formed of an ultraviolet LED and a phosphor attached to the prism, and light from the light emitting section is emitted to the outside through a prism provided on an upper part of the lamp body. The phosphor is attached to the incident surface side of the prism to which the ultraviolet rays from the ultraviolet LED are irradiated, and the phosphor emits light when the ultraviolet rays from the ultraviolet LED are irradiated on the phosphor. The prism polarizes the light emitted from the phosphor into narrow light in the vertical direction and narrow horizontal light in the elevation direction, and radiates the light outside the lamp body.
[0012]
According to the present invention, since the light emitted to the outside is emitted from the phosphor, it is not necessary to consider the directionality of the arrangement of the ultraviolet LEDs. Accordingly, a predetermined number of ultraviolet LEDs can be arranged even in a narrow space inside the lamp body, since the height of the projection of the lamp body is limited, so that a predetermined brightness can be secured.
[0013]
An aerial signage lamp according to the invention of claim 2 is a lamp body attached to a base buried in a road and partially provided so as to protrude from a road surface; and is housed inside the lamp body and outputs ultraviolet rays. An ultraviolet LED; a phosphor adhered to the inner surface of the lamp body to which the ultraviolet light of the ultraviolet LED is irradiated; and a prism which emits visible light converted by the phosphor to the outside. Features.
[0014]
The present invention is different from the first aspect in that the phosphor is attached to the inner surface inside the lamp body to which the ultraviolet rays of the ultraviolet LED are irradiated, instead of the phosphor on the incident surface side of the prism. According to the present invention, the position where light is emitted is the inner surface inside the lamp body, but the emitted light is adjusted by the exit angle of the prism and radiated to the outside, so that the same effect as in claim 1 can be obtained.
[0015]
BEST MODE FOR CARRYING OUT THE INVENTION
FIG. 1 is an explanatory view of an aeronautical sign light 11 according to an embodiment of the present invention. FIG. 1A is a plan view of the aerial sign light 11, and FIG. FIG. A base (not shown) is formed on the runway or taxiway of the airport, and adjustment rings 12a and 12b are mounted on the base with bolts 13a. Then, the lamp body 14 is mounted on the upper part of the adjustment ring 12a with the bolt 13b.
[0016]
An ultraviolet LED 15 is provided inside the lamp 14, and a prism 16 for emitting light to the outside is provided above the lamp 14. Further, a phosphor 17 is attached on the incident surface side of the prism 16 to which the ultraviolet rays from the ultraviolet LED 15 are irradiated, and the phosphor 17 emits light when the ultraviolet rays from the ultraviolet LED 15 are irradiated to the phosphor 17. The light emitted from the phosphor 17 passes through the prism 16 and is polarized outside the lamp body 14 in the elevation direction with a narrow vertical width and wide horizontal light to be radiated to the outside of the lamp body 14, and the light passes through the road surface of the runway or taxiway. Light up.
[0017]
In general, an aeronautical beacon lamp includes a prism 16 in a light-emitting portion, and the light emission from a light source located below the ground inside the lamp body 14 is adjusted by the emission angle of the prism 16. This is to make it possible to reduce the protruding height from the ground by using the prism 16. Therefore, in the embodiment of the present invention, the phosphor 17 is attached to the incident surface side of the prism 16 and the light source is the ultraviolet LED 15. Then, the light is emitted by the phosphor 17 to ensure the directionality of the light to be radiated to the outside irrespective of the arrangement position of the ultraviolet LED 15 as the light source.
[0018]
The phosphor 17 is a mixture of one or more of a phosphor R that emits red light, a phosphor G that emits green light, and a phosphor B that emits blue light when irradiated with ultraviolet light. I do. The phosphor R uses, for example, YVO 4 : Eu, Bi having a peak wavelength of 619 nm, the phosphor G uses, for example, Y 2 SiO 5 Ce, Tb having a peak wavelength of 543 nm, and the phosphor B uses, for example, a peak wavelength of 450 nm. BaMgAl 16 O 27 : Eu is used. By appropriately mixing these, various luminescent colors can be obtained.
[0019]
In the above description, the phosphor 17 is attached to the incident surface side of the prism 16, but may be attached to the inner surface inside the lamp body to which the ultraviolet rays of the ultraviolet LED 15 are irradiated.
[0020]
In this case, the position where the light is emitted is on the inner surface of the interior of the lamp body 14, but the emitted light is adjusted by the exit angle of the prism 16, so that the light radiated to the outside can keep a predetermined directionality. it can.
[0021]
As described above, according to the embodiment of the present invention, since the light emitted to the outside is emitted from the phosphor 17, there is no need to consider the directionality of the arrangement of the ultraviolet LED 15, and the ultraviolet LED 15 It is not necessary to face the incident surface. Therefore, the number of the ultraviolet LEDs 15 as the light source can be provided for the projection area larger than the incident surface.
[0022]
Also, by appropriately selecting the phosphor, it is possible to provide an aerial sign lamp having light of various emission colors. That is, the type of the phosphor can be changed, and the light emitted to the outside can be set to a desired emission color. For example, a mixture of one or more of a phosphor R that emits red light, a phosphor G that emits green light, and a phosphor B that emits blue light when irradiated with ultraviolet light is used. Thereby, an appropriate emission color can be appropriately selected according to the purpose of use of the aeronautical sign lamp.
[0023]
【The invention's effect】
According to the first aspect of the present invention, since the light emitted to the outside is emitted from the fluorescent material, it is not necessary to consider the directionality of the arrangement of the ultraviolet LED. Even in a narrow space, a predetermined number of ultraviolet LEDs can be arranged. Therefore, a predetermined brightness can be secured.
[0024]
According to the second aspect of the invention, the light emission position is on the inner surface inside the lamp body, but the emission is adjusted by the exit angle of the prism and radiated to the outside, so that the same effect as the first aspect is obtained. .
[Brief description of the drawings]
FIG. 1 is an explanatory diagram of an aeronautical sign light according to an embodiment of the present invention.
[Explanation of symbols]
11: Aviation sign light, 12: Adjusting ring, 13: Bolt, 14: Lamp body, 15: Ultraviolet LED, 16: Prism, 17: Phosphor

Claims (2)

路中に埋設された基台に取り付けられ一部が路面から突出するように設けられる灯体と;
前記灯体の内部に収納され紫外線を出力する紫外線LEDと;
前記紫外線LEDからの紫外線が照射されるにように配置され、その照射面側に蛍光体が被着され、蛍光体によって変換された可視光を外部に放射するように設けられたプリズムと;
を備えたことを特徴とする航空標識灯。
A lamp body mounted on a base buried in the road and partially provided so as to protrude from the road surface;
An ultraviolet LED that is housed inside the lamp body and outputs ultraviolet light;
A prism disposed so as to be irradiated with ultraviolet rays from the ultraviolet LED, a phosphor attached to an irradiation surface thereof, and a prism provided to emit visible light converted by the phosphor to the outside;
An air traffic sign light comprising:
路中に埋設された基台に取り付けられ一部が路面から突出するように設けられる灯体と;
前記灯体の内部に収納され紫外線を出力する紫外線LEDと;
前記紫外線LEDの紫外線が照射される前記灯体内部の内面に被着された蛍光体と;
前記蛍光体によって変換された可視光を外部に放射するプリズムと;
を備えたことを特徴とする航空標識灯。
A lamp body mounted on a base buried in the road and partially provided so as to protrude from the road surface;
An ultraviolet LED that is housed inside the lamp body and outputs ultraviolet light;
A phosphor adhered to an inner surface of the lamp body to which the ultraviolet LED is irradiated with ultraviolet rays;
A prism that emits visible light converted by the phosphor to the outside;
An air traffic sign light comprising:
JP2003001436A 2003-01-07 2003-01-07 Airway beacon light Pending JP2004214095A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
JP2003001436A JP2004214095A (en) 2003-01-07 2003-01-07 Airway beacon light

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
JP2003001436A JP2004214095A (en) 2003-01-07 2003-01-07 Airway beacon light

Publications (1)

Publication Number Publication Date
JP2004214095A true JP2004214095A (en) 2004-07-29

Family

ID=32819463

Family Applications (1)

Application Number Title Priority Date Filing Date
JP2003001436A Pending JP2004214095A (en) 2003-01-07 2003-01-07 Airway beacon light

Country Status (1)

Country Link
JP (1) JP2004214095A (en)

Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07114904A (en) * 1993-10-18 1995-05-02 Hitachi Ltd Fluorescent discharge lamp for back-light source
JP2000057488A (en) * 1998-08-12 2000-02-25 Ruminooba Seiko:Kk Traffic signal lamp
JP2001243821A (en) * 2000-02-28 2001-09-07 Mitsubishi Electric Lighting Corp Surface light source with led
JP2002050203A (en) * 2000-08-04 2002-02-15 Toshiba Lighting & Technology Corp Indicating light
JP2002304903A (en) * 2001-04-04 2002-10-18 Matsushita Electric Works Ltd Luminaire

Patent Citations (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
JPH07114904A (en) * 1993-10-18 1995-05-02 Hitachi Ltd Fluorescent discharge lamp for back-light source
JP2000057488A (en) * 1998-08-12 2000-02-25 Ruminooba Seiko:Kk Traffic signal lamp
JP2001243821A (en) * 2000-02-28 2001-09-07 Mitsubishi Electric Lighting Corp Surface light source with led
JP2002050203A (en) * 2000-08-04 2002-02-15 Toshiba Lighting & Technology Corp Indicating light
JP2002304903A (en) * 2001-04-04 2002-10-18 Matsushita Electric Works Ltd Luminaire

Similar Documents

Publication Publication Date Title
CN103392093B (en) Light emitting module and lamps apparatus for vehicle
US9599307B2 (en) Multi-colored vehicle rear lamp
US20050242711A1 (en) Multi-color solid state light emitting device
TWI461100B (en) Led signal lamp
JP5808840B2 (en) Light emitting module and vehicle lamp
KR20080092452A (en) Shifting spectral content in solid state light emitters by spatially separating lumiphor films
US10053214B2 (en) Layer material for arranging on a rotor blade tip of a helicopter, helicopter light system, and helicopter comprising the same
JP2011108589A (en) Light emitting module and automotive lamp
JP2001243807A (en) Led electric bulb
TW201502244A (en) Red lamp and lighting system for vehicle
CN104515069A (en) Red lamp and vehicle lighting fixture
TWI638029B (en) Lighting device
JP2002008414A (en) Lamp for marker light and aircraft warning light
EP1600559A1 (en) Carriageway-marking device and system
US11415282B2 (en) LED module for flashing lamp and flashing lamp
KR20080104708A (en) Lamp using light emitting devices
JP6199710B2 (en) Gaze guidance device
WO2009083853A1 (en) Lighting system
JP2004214095A (en) Airway beacon light
JP6894737B2 (en) Vehicle lighting
JP2000045237A (en) Marker lamp
JP2013073677A (en) Airway beacon
JP2013026163A (en) Light-emitting device, vehicular headlight and lighting device
JP2007270468A (en) Embedded marker light equipment
JP2005259466A (en) Led type runway light

Legal Events

Date Code Title Description
A621 Written request for application examination

Free format text: JAPANESE INTERMEDIATE CODE: A621

Effective date: 20051202

A977 Report on retrieval

Free format text: JAPANESE INTERMEDIATE CODE: A971007

Effective date: 20080528

A131 Notification of reasons for refusal

Free format text: JAPANESE INTERMEDIATE CODE: A131

Effective date: 20080603

A02 Decision of refusal

Free format text: JAPANESE INTERMEDIATE CODE: A02

Effective date: 20081111