TWI454005B - Packaging structure and method for butterfly laser module - Google Patents
Packaging structure and method for butterfly laser module Download PDFInfo
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- 238000000034 method Methods 0.000 title claims description 30
- 238000004806 packaging method and process Methods 0.000 title 1
- 239000000835 fiber Substances 0.000 claims description 33
- 230000008878 coupling Effects 0.000 claims description 20
- 238000010168 coupling process Methods 0.000 claims description 20
- 238000005859 coupling reaction Methods 0.000 claims description 20
- 238000003466 welding Methods 0.000 claims description 19
- 239000000758 substrate Substances 0.000 claims description 18
- 239000013307 optical fiber Substances 0.000 claims description 8
- 238000012545 processing Methods 0.000 claims description 3
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- 238000004891 communication Methods 0.000 description 9
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- JVPLOXQKFGYFMN-UHFFFAOYSA-N gold tin Chemical compound [Sn].[Au] JVPLOXQKFGYFMN-UHFFFAOYSA-N 0.000 description 1
- LQBJWKCYZGMFEV-UHFFFAOYSA-N lead tin Chemical compound [Sn].[Pb] LQBJWKCYZGMFEV-UHFFFAOYSA-N 0.000 description 1
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- NJPPVKZQTLUDBO-UHFFFAOYSA-N novaluron Chemical compound C1=C(Cl)C(OC(F)(F)C(OC(F)(F)F)F)=CC=C1NC(=O)NC(=O)C1=C(F)C=CC=C1F NJPPVKZQTLUDBO-UHFFFAOYSA-N 0.000 description 1
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Description
本發明係有關於一種蝶式雷射模組構裝結構與方法,尤其是指一種構裝過程時間短、成本花費低、耦光效率較佳且同時可提高良率的雷射模組構裝結構,藉由將構裝過程簡化為經二次耦光來完成,以達到上述功效為發明應用者。The invention relates to a butterfly laser module assembly structure and method, in particular to a laser module assembly with short assembly process time, low cost, good coupling efficiency and improved yield. The structure is accomplished by simplifying the fabrication process to secondary coupled light to achieve the above-described effects.
按,現今通訊科技日新月異,藉由電話、網路等通訊設施的架設,人與人的距離愈來愈近,而通訊設施之傳輸係以無線或有線的方式進行,但無線傳輸會因使用之天候、地形等因素影響,使得通訊時之干擾問題無法有效控制與解決,所以有線傳輸在目前通訊上仍是最有效、穩定的訊號傳輸方式。According to the news, today's communication technology is changing with each passing day. With the establishment of communication facilities such as telephone and Internet, the distance between people is getting closer and closer, and the transmission of communication facilities is carried out wirelessly or by wire, but wireless transmission will be used. The influence of weather and terrain makes the interference problem during communication unable to be effectively controlled and solved. Therefore, wired transmission is still the most effective and stable signal transmission method in current communication.
然而,有線傳輸為將電子信號或光信號透過纜線來作為訊號之傳輸路徑,其中,尤以光信號之傳輸方式最為快速(可超過11次方個bit-per-second),而光信號的傳輸介質為光纖(Fiber Optics)纜線,光纖通訊為存在有頻寬高、重量輕、訊號正確性高、傳輸距離遠,且不會被外界電磁波干擾等優點;而光纖通訊的系統中,於發射端必須有一個光發射模組將電信號換成光信號,當光信號到達接收後,亦經光接收模組將光信號轉換成電信號,如此才能建構出一光纖通信系統。However, the wired transmission is to transmit an electronic signal or an optical signal through the cable as a transmission path of the signal, wherein the transmission mode of the optical signal is the fastest (more than 11 bit-per-second), and the optical signal The transmission medium is a fiber optic (Fiber Optics) cable, and the optical fiber communication has the advantages of high bandwidth, light weight, high signal correctness, long transmission distance, and no external electromagnetic interference; and in the optical fiber communication system, The transmitting end must have a light emitting module to convert the electrical signal into an optical signal. When the optical signal arrives at the receiving, the optical receiving signal is also converted into an electrical signal by the optical receiving module, so that a fiber-optic communication system can be constructed.
而一般常見的半導體雷射模組構裝型式,可分為下列三種類型:同軸構裝、雙排線式構裝及蝶式構裝,其中蝶式雷射模用於高速度、高功率光訊號傳輸。然而,在雷射的構裝過程中,最重要的部份是光纖與雷射之間的耦光對準與固定,一般光通訊雷射模組都是使用雷射銲接作固定結合,雷射銲接具有構裝速度快、重複性高與可靠度高等優點,但在雷射銲接的過程中,金屬材料吸收雷射所發出的光能,將之轉換成熱能,而材料因熱能而熔化並且瞬間冷凝,產生了型態上的變化,這種型態上的變化,會產生不小的熱應力,使得光纖改變原本最佳的位置,造成了耦光功率的改變,而光纖經焊接前後所產生的位移,稱為銲後位移,銲後位移越大相對會影響整個雷射模組的耦光效率。The general semiconductor laser module construction type can be divided into the following three types: coaxial structure, double-row line structure and butterfly structure, in which butterfly laser mode is used for high speed and high power. Optical signal transmission. However, in the laser assembly process, the most important part is the coupling and fixing of the coupling between the optical fiber and the laser. Generally, the optical communication laser module uses laser welding as a fixed combination, and the laser Welding has the advantages of fast assembly speed, high repeatability and high reliability. However, in the process of laser welding, the metal material absorbs the light energy emitted by the laser and converts it into heat energy, and the material melts due to heat energy and instantaneously. Condensation, resulting in a change in the type, this type of change, will produce a lot of thermal stress, so that the fiber changes the original optimal position, resulting in a change in the coupling power, and the fiber is produced before and after welding The displacement, called the post-weld displacement, the greater the displacement after welding, which will affect the coupling efficiency of the entire laser module.
而傳統之蝶式雷射模組於實際構裝時,一個雙光束的雷射焊接系統被用於把光纖套管和雷射二極體連結起來,而其中絕大部分在於光對準與構裝,由於光纖本身為細小且容易斷裂破損的玻璃材質,因此在光纖對準與固定前(尤其以雷射銲接技術固定光纖)經常需將光纖固定在一個可提供保護的套管內,製作方法係以銲錫(鉛錫或金錫)技術將外表鍍金光纖銲接於金屬管內,形成光纖-銲錫-套管之光纖套管,因此,在操作光纖對準步驟,僅處理光纖套管與雷射對準,待光纖對準後,鞍型扣件扣住光纖套管,再利用一個雙光束的雷射銲接方式將鞍型扣件、光纖套管與基座固定。由於銲後位移(postweld PWS)的凝固收縮過程變換造成蝶式雷射模組構裝耦光效率低,良率不高且構裝技術門檻高,其關鍵技術為鞍型扣件與光纖套管與基座結合;在傳統的蝶式雷射模組構裝方面,當鞍型扣件與光纖套管被雷射 (被調整好之後)焊接接合時,PWS是很大的。因此,耦合效率和收益率是低的,為了使耦光效率增加並必須結合的雷射鐵錘(laser hammer)補救而增長製程時間,且良率不高。While the traditional butterfly laser module is actually assembled, a two-beam laser welding system is used to connect the fiber ferrule and the laser diode, and most of them are in light alignment and structure. Because the fiber itself is a small and easily broken glass material, it is often necessary to fix the fiber in a protective sleeve before the fiber is aligned and fixed (especially by laser welding). The outer surface of the gold-plated fiber is soldered into the metal tube by solder (lead tin or gold tin) technology to form a fiber-solder-sleeve fiber sleeve. Therefore, only the fiber sleeve and the laser are processed in the operation of the fiber alignment step. Alignment, after the fiber is aligned, the saddle fastener is fastened to the fiber sleeve, and the two-beam laser welding method is used to fix the saddle fastener, the fiber sleeve and the base. Due to the transformation of the post-weld displacement (postweld PWS), the butterfly laser module has low coupling efficiency, low yield and high threshold. The key technologies are saddle fasteners and fiber ferrules. In combination with the pedestal; in the conventional butterfly laser module construction, the PWS is large when the saddle fastener is soldered to the fiber ferrule by the laser (after being adjusted). Therefore, the coupling efficiency and the yield are low, and the process time is increased in order to increase the coupling efficiency and must be combined with the laser hammer recovery, and the yield is not high.
緣是,發明人有鑑於此,秉持多年該相關行業之豐富設計開發及實際製作經驗,針對現有之結構再予以研究改良,因而發明出一種蝶式雷射模組構裝結構與方法,以期達到更佳實用價值性之目的者。The reason is that the inventor has in view of this, and has been researching and improving the existing structure for many years of rich design and development and practical production experience of the relevant industry, thus inventing a butterfly laser module construction structure and method, in order to achieve The purpose of better practical value.
本發明之主要目的為提供一種蝶式雷射模組構裝結構與方法,為指一種構裝過程時間短、成本花費低、耦光效率較佳且同時可提高良率的雷射模組構裝結構,藉由將構裝過程簡化為經二次耦光來完成,以達到上述功效為目的者。The main object of the present invention is to provide a structure and a method for constructing a butterfly laser module, which is a laser module structure with short assembly process time, low cost, good coupling light efficiency and improved yield. The mounting structure is completed by simplifying the assembly process to the secondary coupling light to achieve the above effects.
本發明蝶式雷射模組構裝結構與方法的目的與功效係由以下之技術所實現:The purpose and function of the structure and method of the butterfly laser module of the present invention are achieved by the following technologies:
其模組包含有上、下部組件,該下部組件為包含有建構光源發射構件的基板、與結合固定於基板上的弧形扣件,而該上部組件為由一可與弧形扣件結合的套筒對應嵌入一組裝光纖的套管所構成;藉此,以利用於上部組件之光纖與套筒的第一次耦光及上、下部組件之套筒與弧形扣件結合的第二次耦光,達到構裝過程時間短、成本花費低、耦光效率較佳以及提高良率的功效者。The module comprises upper and lower components, the lower component is a substrate comprising a light source emitting component and a curved fastener fixedly coupled to the substrate, and the upper component is combined with a curved fastener. The sleeve is formed by a sleeve embedded in an assembled optical fiber; thereby, the first coupling of the optical fiber and the sleeve for the upper component and the sleeve of the upper and lower components are combined with the curved fastener for the second time Coupling light, achieving the effect of short assembly process time, low cost, better coupling efficiency and improved yield.
本發明蝶式雷射模組構裝結構與方法中之光源發射構件進一步包含有雷射二極體、檢光二極體及熱敏電阻者。The light source emitting member in the structure and method of the butterfly laser module of the present invention further comprises a laser diode, a light detecting diode and a thermistor.
本發明蝶式雷射模組構裝結構與方法中之弧形扣件進一步藉以該弧形扣件的形狀設計,而能達到易與蝶式外殼作連線(電路)結合者,並與原傳統蝶式雷射模組電性一樣。The curved fastener in the structure and method of the butterfly laser module of the present invention is further designed by the shape of the curved fastener, and can be easily connected with the butterfly casing (circuit), and the original The traditional butterfly laser module is electrically identical.
本發明蝶式雷射模組構裝結構與方法中之光纖套管結構進一步可以構裝成橢圓形光纖透鏡,以可作為光纖放大器的構裝者。The fiber-optic sleeve structure in the structure and method of the butterfly laser module of the present invention can further be configured as an elliptical fiber lens to serve as a constructor of the fiber amplifier.
為令本發明所運用之技術內容、發明目的及其達成之功效有更完整且清楚的揭露,茲於下詳細說明之,並請一併參閱所揭之圖式及圖號:For a more complete and clear disclosure of the technical content, the purpose of the invention and the effects thereof achieved by the present invention, it is explained in detail below, and please refer to the drawings and drawings:
首先,請參閱第一~三圖,本發明蝶式雷射模組構裝結構與方法分解示意圖,主要於基殼(3)內焊接有雷射模組(A),其係包含有:
一下部組件(1),為由一基板(11)與弧形扣件(12)所構成,於基板(11)上係建構有雷射二極體(131)、電光二極體(132)及熱敏電阻(133)的光源發射組件(13),而其弧形扣件(12)為對應覆蓋在基板(11)上方且卡固在基板(11)兩側,於弧形扣件(12)兩側設有供線路穿設的透孔(121);
一上部組件(2),為由一與弧形扣件(12)結合的套筒(21)對應嵌入一組裝光纖的套管(22)所構成者。First, please refer to the first to third figures. The schematic diagram of the structure and method of the butterfly laser module structure of the present invention is mainly welded to the base shell (3) with a laser module (A), which includes:
A lower assembly (1) is composed of a substrate (11) and a curved fastener (12), and a laser diode (131) and an electro-optical diode (132) are constructed on the substrate (11). And a light source emitting component (13) of the thermistor (133), and the curved fastener (12) is correspondingly covered on the substrate (11) and fastened on both sides of the substrate (11), and the curved fastener ( 12) There are through holes (121) for the passage of the lines on both sides;
An upper assembly (2) is formed by a sleeve (21) that is coupled to the curved fastener (12) and correspondingly fitted with a sleeve (22) for assembling the optical fiber.
請參閱第一~四圖所示,當於構裝時,其步驟如下:Please refer to the first to fourth figures. When constructing, the steps are as follows:
(a)將架構有光源發射組件(13)的基板(11)對應弧形扣件(12),讓弧形扣件(12)使用緊配方式與基板(11)進行結合,而完成下部組件(1)的配置;(a) The substrate (11) having the light source emitting component (13) is corresponding to the curved fastener (12), and the curved fastener (12) is combined with the substrate (11) in a tightly fitting manner to complete the lower component. (1) configuration;
(b)將組裝光纖的套管(22)(Fiber Ferrule)放入套筒(21)(Sleeve)中與雷射二極體(131)進行耦光;(b) placing a fiber optic sleeve (22) (Fiber Ferrule) into the sleeve (21) (Sleeve) to couple with the laser diode (131);
(c)找到最佳耦光位置,將套管(22)與套筒(21)進行雷射銲接,將光纖套管(22)與套筒(21)重新進行耦光,完成上部組件(2)的配置;(c) Find the best coupling position, perform laser welding on the sleeve (22) and the sleeve (21), and recouple the fiber sleeve (22) and the sleeve (21) to complete the upper assembly (2) )Configuration;
(d)將配置完成之上、下部組件(2)、(1)放至於加工機台,驅動雷射,當光纖套管(22)與金屬套筒(21)在最佳耦光效率狀況下,再利用機台上之平台進行耦光至最佳位置,以雷射銲接將上、下部組件(2)、(1)固定。
當上述之上、下部組件(2)、(1)固定後構成一雷射模組(A),再將該雷射模組(A)與基殼(3)結合,如下步驟:(d) Place the upper and lower components (2) and (1) above the configuration on the processing machine to drive the laser. When the fiber ferrule (22) and the metal sleeve (21) are in the optimal coupling efficiency. Then, the platform on the machine is used to couple light to the optimal position, and the upper and lower components (2) and (1) are fixed by laser welding.
When the upper and lower components (2), (1) are fixed to form a laser module (A), and then the laser module (A) is combined with the base shell (3), the following steps are as follows:
(e)該基殼(3)內備設有熱電致冷器(31),再將雷射模組(A)置入基殼(3)之熱電致冷器(31)上利用打線機結合,成為一完整之蝶式雷射模組。(e) The base case (3) is provided with a thermoelectric cooler (31), and the laser module (A) is placed in the thermoelectric cooler (31) of the base case (3) by a wire bonding machine. Become a complete butterfly laser module.
本發明雷射構裝技術在構裝過程中,為光纖頭端與雷射二極體(131)之對準與結合,此為決定該模組的良率。而本發明之雷射模組其製程時間較原本蝶式雷射模組構裝方式要短、花費較為便宜、耦光效率較佳以及良率較高;利用雷射模組(A)分上、下部組件(2)、(1)部分獨立進行,再結合高速蝶式雷射模組之新構裝技術應用,將高速蝶式雷射模組以TO-Butterfly TOSA方式進行構裝,將會大幅減少製程所需時間,並降低成本。In the structure of the laser structure of the present invention, the alignment and bonding of the fiber tip and the laser diode (131) are performed, which determines the yield of the module. The laser module of the present invention has a shorter processing time than the original butterfly laser module, is cheaper, has better coupling efficiency and higher yield; and is divided by a laser module (A). The lower components (2) and (1) are independently carried out, and combined with the new construction technology of the high-speed butterfly laser module, the high-speed butterfly laser module is constructed by TO-Butterfly TOSA. Significantly reduce the time required for the process and reduce costs.
然而前述之實施例或圖式並非限定本發明之產品結構或使用方式,任何所屬技術領域中具有通常知識者之適當變化或修飾,皆應視為不脫離本發明之專利範疇。However, the above-described embodiments or drawings are not intended to limit the structure or the use of the present invention, and any suitable variations or modifications of the invention will be apparent to those skilled in the art.
藉由上述可知,本發明之組成與使用實施說明相較於一般現有裝置,我們可以知道蝶式雷射模組構裝結構與方法,具有下列幾項優點,如下:From the above, it can be seen that the composition of the present invention and the implementation description are comparable to the conventional devices, and we can know the structure and method of the butterfly laser module assembly, which have the following advantages, as follows:
- 傳統蝶式雷射模組所使用之鞍型扣件,價格昂貴,其設計形狀為方便用於雷射補償所設計,當銲接後整體結構強度較新型蝶式雷射模組構裝方式低且構裝技術門檻高;本發明蝶式雷射模組構裝技術其元件材料便宜、元件結構強、銲接方式技術低,且具有較高之可靠度。The saddle fastener used in the traditional butterfly laser module is expensive, and its design shape is convenient for laser compensation design. When welded, the overall structural strength is lower than that of the new butterfly laser module. The threshold of the structure technology is high; the butterfly laser module assembly technology of the invention has the advantages of low component materials, strong component structure, low welding technique and high reliability.
- 相較於傳統蝶式模組之構裝,此本發明蝶式雷射模組構裝將雷射模組分上、下部組件部分獨立進行,完成後再與外盒結合,減少製程之困難度,進而減少製程時間。Compared with the traditional butterfly module, the butterfly laser module of the present invention independently carries out the upper and lower components of the laser module component, and then combines with the outer casing to reduce the difficulty of the process. , thereby reducing process time.
- 傳統之蝶式雷射模組構裝時,其產生主要之銲後位移方向,影響耦光功率甚鉅(Y軸);相較之下,本發明蝶式雷射模組構裝,其主要銲後位移方向,不僅存在著拘束,且對於耦光效率之影響較小(Z軸)。When the traditional butterfly laser module is assembled, it generates the main post-weld displacement direction, which affects the coupled light power (Y-axis). In contrast, the butterfly laser module of the present invention is mainly composed. The direction of displacement after welding is not only limited, but also has little effect on the coupling efficiency (Z-axis).
- 雷射模組之構裝可利用三光束雷射銲接系統(3-beam laser welding system)取代雙光束雷射銲接系統(2-beam laser welding system),因雙光束雷射銲接系統為特殊設計,相對的成本比三光束雷射銲接系統貴,所以可減少成本,使蝶式雷射模組更具有競增力。The laser module is designed to replace the 2-beam laser welding system with a 3-beam laser welding system, which is specially designed for the dual beam laser welding system. The relative cost is more expensive than the three-beam laser welding system, so the cost can be reduced and the butterfly laser module can be more competitive.
- 傳統之蝶式雷射模組構裝,因無法構裝具有橢圓形光纖透鏡的光纖套管,而本發明則可利用旋轉耦光,而可以構裝橢圓形光纖透鏡,進一步作為光纖放大器的構裝者。In the conventional butterfly type laser module assembly, since the fiber ferrule having the elliptical fiber lens cannot be constructed, the present invention can utilize the rotational coupling light to construct the elliptical fiber lens, and further serve as the structure of the fiber amplifier. Installer.
綜上所述,本發明實施例確能達到所預期之使用功效,又其所揭露之具體構造,不僅未曾見諸於同類產品中,亦未曾公開於申請前,誠已完全符合專利法之規定與要求,爰依法提出發明專利之申請,懇請惠予審查,並賜准專利,則實感德便。In summary, the embodiments of the present invention can achieve the expected use efficiency, and the specific structure disclosed therein has not been seen in similar products, nor has it been disclosed before the application, and has completely complied with the provisions of the Patent Law. And the request, the application for the invention of a patent in accordance with the law, please forgive the review, and grant the patent, it is really sensible.
(A)...雷射模組(A). . . Laser module
(1)...下部組件(1). . . Lower component
(11)...基板(11). . . Substrate
(12)...弧形扣件(12). . . Curved fastener
(121)...透孔(121). . . Through hole
(13)...光源發射組件(13). . . Light source emitting component
(131)...雷射二極體(131). . . Laser diode
(132)...光二極體(132). . . Light diode
(133)...熱敏電阻(133). . . Thermistor
(2)...上部組件(2). . . Upper component
(21)...套筒(twenty one). . . Sleeve
(22)...套管(twenty two). . . casing
(3)...基殼(3). . . Base shell
(31)...熱電致冷器(31). . . Thermoelectric cooler
第一圖:本發明之上部組件分解示意圖First figure: exploded view of the upper component of the present invention
第二圖:本發明之下部組件分解示意圖Second figure: exploded view of the lower part of the present invention
第三圖:本發明之組合示意圖Third figure: a schematic diagram of the combination of the present invention
第四圖:本發明之組裝基殼狀態示意圖Fourth: Schematic diagram of the assembled base of the present invention
(A)...雷射模組(A). . . Laser module
(1)...下部組件(1). . . Lower component
(11)...基板(11). . . Substrate
(12)...弧形扣件(12). . . Curved fastener
(121)...透孔(121). . . Through hole
(131)...雷射二極體(131). . . Laser diode
(2)...上部組件(2). . . Upper component
(21)...套筒(twenty one). . . Sleeve
(22)...套管(twenty two). . . casing
Claims (10)
一下部組件,為由一基板與弧形扣件所構成,於基板上係建構有光源發射組件,而其弧形扣件為對應覆蓋在基板上方且卡固在基板兩側,於弧形扣件兩側設有供線穿設的透孔,以藉透孔對應基殼作連線結合;
一上部組件,為由一與弧形扣件結合的套筒對應嵌入一組裝光纖的套管所構成者。A butterfly laser module structure is mainly characterized in that a laser module is soldered in a base shell, and the system comprises:
A lower assembly is composed of a substrate and a curved fastener. The light source emitting component is constructed on the substrate, and the curved fastener is correspondingly covered on the substrate and fastened on both sides of the substrate. Both sides of the piece are provided with through holes for threading, so that the through holes are connected with the base shell;
An upper assembly is formed by a sleeve that is assembled with an optical fiber by a sleeve that is coupled to the curved fastener.
(a)將架構有光源發射組件的基板對應弧形扣件,讓弧形扣件使用緊配方式與基板進行結合,而完成下部組件的配置;
(b)將組裝光纖的套管(Fiber Ferrule)放入套筒 (Sleeve)中與光源發射組件進行耦光;
(c)找到最佳耦光位置,將套管與套筒進行雷射銲接,完成上部組件的配置;
(d)將配置完成之上、下部組件放至於加工機台,再利用機台上之平台進行耦光,以雷射銲接將上、下部組件固定。A butterfly laser module assembly method, the steps are as follows:
(a) the substrate with the light source emitting component is corresponding to the curved fastener, and the curved fastener is combined with the substrate by using a tight fitting manner to complete the configuration of the lower component;
(b) placing a fiber-optic jacket (Fiber Ferrule) into the sleeve (Sleeve) to couple with the light source emitting component;
(c) Find the best coupling position, perform laser welding on the sleeve and the sleeve, and complete the configuration of the upper assembly;
(d) Place the upper and lower components of the configuration on the processing machine, and then use the platform on the machine to couple the light, and fix the upper and lower components by laser welding.
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| TW101109360A TWI454005B (en) | 2012-03-19 | 2012-03-19 | Packaging structure and method for butterfly laser module |
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Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5430820A (en) * | 1993-04-06 | 1995-07-04 | U.S. Philips Corporation | Optoelectronic device with a coupling between an optoelectronic component, in particular a semiconductor diode laser, and an optical glass fibre, and method of manufacturing such a device |
| TW200403455A (en) * | 2002-05-28 | 2004-03-01 | Intel Corp | Methods of sealing electronic, optical and electro-optical packages and related package and substrate designs |
| US7478955B2 (en) * | 2005-08-12 | 2009-01-20 | Applied Optoelectronics, Inc. | Modular laser package system |
| TW201028751A (en) * | 2009-01-22 | 2010-08-01 | Univ Nat Sun Yat Sen | Saddle-shaped fastener for assembling a butterfly laser module |
-
2012
- 2012-03-19 TW TW101109360A patent/TWI454005B/en not_active IP Right Cessation
Patent Citations (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US5430820A (en) * | 1993-04-06 | 1995-07-04 | U.S. Philips Corporation | Optoelectronic device with a coupling between an optoelectronic component, in particular a semiconductor diode laser, and an optical glass fibre, and method of manufacturing such a device |
| TW200403455A (en) * | 2002-05-28 | 2004-03-01 | Intel Corp | Methods of sealing electronic, optical and electro-optical packages and related package and substrate designs |
| US7478955B2 (en) * | 2005-08-12 | 2009-01-20 | Applied Optoelectronics, Inc. | Modular laser package system |
| TW201028751A (en) * | 2009-01-22 | 2010-08-01 | Univ Nat Sun Yat Sen | Saddle-shaped fastener for assembling a butterfly laser module |
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