M422177 五、新型說明： 【新型所屬之技術領域】 [0001] [0002] 特別是一種小型化之 本創作係有關於一種衛星集波器， 衛星集波器。 【先前技術】 衛星集波器又稱為低雜訊降頻放大器（1〇w noise block downconverter，通常簡稱為LNB)，是由低雜 訊放大器（low noise ampUfier，通常簡稱為 及 LNC (low block down converter)降頻器兩也 D啊者所 合併而來的。 [0003]衛星集波器的作用是將衛星信號放大和降頻；衛星矩離 地面約三萬多公里，所傳送之衛星信號在抵達碟型天線 前已相當微弱’所以需要衛星集波器來做信號放大的動 作；衛星集波器會先將高頻的衛星信號放大數十萬倍之 後，再利用本地震盪電路將高頻轉換至中頻，以利於同 軸電纜的傳輸及衛星接收機的解調工作。 [0004]同軸電纜連接於衛星集波器與衛星接收機之間；由於同 轴電纜傳輸的頻率越高，信號損耗越大，所以需要衛星 集波器利用本地振盪電路將衛星信號從高頻轉換至中頻 ，以利於同軸電纜的傳輸及衛星接收機的解調工作。衛 星集波器可將衛星訊號由3.4〜4.2GHz (C band)或 0.7〜12.75GHz (Ku band)降頻到衛星接收機所需要 的中頻（ 950MHz〜2050MHz，依衛星集波器種類決定中 頻範圍最後，才能將聲音與影像在電視機上顯示。 表單編號A0101 第4頁/共32頁 [0005] 請參考第一圖，其係為習知衛星集波器剖視透明圖。一 習知衛星集波器60包含一主骨架602、一L型骨架604、 一第一印電路板606、一第二印刷電路板608及一L型外殼 610。該第一印電路板606係安置於該L型骨架604的一面 ) ，該第二印刷電路板608係安置於該L型骨架604的另一面 ;該1^型骨架604係安置於該主骨架602之上；該L型外殼 610係包覆該主骨架602、該L型骨架604、該第一印電路 板606及該第二印刷電路板608。 [0006] 衛星（未圖示）所傳送之衛星信號經過一碟型天線（未 圖示）反射後，進入該習知衛星集波器60，以進行放大 及降頻的動作；最後經由同軸電纜（未圖示〉傳送至衛 星接收機（未圖示），以在電視機（未圖示）上顯示出 衛星節目的晝面影像及聲音。 [0007] 在一具體之實施例，係包含多數之該習知衛星集波器60 架設在該碟形天線之前，以揍收衛星信號；該習知衛星 集波器60的數量越多，該碟形天線的碟面面積就需要越 大；該碟形天線的碟面面積越大，該碟形天線的價格就 越高。 [0008] 如第一圖所示之該習知衛星集波器60，因為該L型骨架 604及該L型外殼610的L型設計，將使得該習知衛星集波 器60的體積相當龐大；當該習知衛星集波器60的體積龐 大且需要有多數之該習知衛星集波器60被應用時，該碟 形天線的碟面面積就需要越大，因而該碟形天線的價格 就越1¾。 [0009] 因此，為了減少該碟形天線的碟面面積以降低該碟形天 表單編號A0101 第5頁/共32頁 M422177 線的價格，如何能研發出體積較小的衛星集波器，實為 當前之一重要課題。 【新型内容】 [0010] 為改善上述習知技術之缺點，本創作之目的在於提供一 種小型化之衛星集波器。 [0011] 為達成本創作之上述目的，本創作之小型化之衛星集波 器，包含：一承載體，包含一承載體第一面及一承載體 第二面，該承載體第一面及該承載體第二面係為反向設 置；一空心凸塊，係設置於該承載體第一面的一端；一 空心筒狀頸部，係設置於該空心凸塊的一端；一末端凸 塊，係相對於該空心凸塊設置於該承載體第一面的另一 端；至少一前端凸塊，係相鄰該空心凸塊設置於該承載 體第一面的一端；一第一印刷電路板，係設置於該承載 體第一面；一第二印刷電路板，係設置於該前端凸塊及 該末端凸塊；及至少一可撓導線，焊接於該第一印刷電 路板及該第二印刷電路板之間，以達成該第一印刷電路 板及該第二印刷電路板之間的電性連接。 [0012] 本創作之功效在於使衛星集波器小型化。 【實施方式】 [0013] 請參考第二圖，其係為本創作之小型化之衛星集波器立 體分解圖；並請同時參考第三圖，其係為本創作之小型 化之衛星集波器另一角度之立體分解圖；並請同時參考 第四圖，其係為本創作之小型化之衛星集波器透視圖； 並請同時參考第五圖，其係為本創作之小型化之衛星集 波器另一角度之透視圖。 表單編號A0101 第6頁/共32頁 [0014] 本創作之小型化之衛星集波器7〇包含一承载體7〇2、一空 心凸塊704、一空心筒狀頸部7〇6、至少一前端凸塊⑶ 、一末端凸塊708、一第一印刷電路板71〇、一第二印刷 電路板Π2及至少一可撓導線714 ^ [0015] 該承載體702包含一承載體第一面7〇22及一承載體第二面 7024，該承載體第一面7022及該承載體第二面7〇24係為 反向設置。 [0016] 該空心凸塊704係設置於該承載體第一面7022的一端；該 空心筒狀頸部706係設置於該空心凸塊704的一端；該前 端凸塊734係相鄰該空心凸塊704設置於該承載體第一面 7022的一端；該末端凸塊708係相對於該空心凸塊7〇4設 置於該承載體第一面7022的另一端。 [0017] 該第一印刷電路板710係設置於該承載體第一面7022 ;該 第二印刷電路板712係設置於該前端凸塊734及該末端凸 塊708 ;該可撓導線714焊接於該第一印刷電路板71〇及 該第二印刷電路板712之間’以達成該第一印刷電路板 710及該第二印刷電路板712之間的電性連接》 [0018] 本創作之小型化之衛星集波器7〇更包含至少一徵線接頭 716、一第三印刷電路板718、一保護蓋體720、一隔離 蓋體722、一筒狀外殼724、一散熱II片726、複數之螺 絲728、一第四印刷電路板736、一第五印刷電路板738 及一金屬板塊740。 該可撓導線714焊接於該續*線接頭716及該第二印刷電路 板712之間，以達成該纜線接頭716及該第二印刷電路板 表單編號A0101 第7頁/共32頁 [0019] M422177 712之間的電性連接；該第三印刷電路板718係設置於該 承載體第二面7024，該可撓導線714焊接於該第三印刷電 路板718及該第二印刷電路板712之間，以達成該第=印 刷電路板718及該第二印刷電路板712之間的電性連接. 該保護蓋體720係設置於該第三印刷電路板718 ;該隔離 蓋體722係設置於該第一印刷電路板710及該第二印刷電 路板712之間；該第四印刷電路板736螺固於該承載體 702的側面；該第五印刷電路板738與該第二印刷電路板 712及該第四印刷電路板736焊接；該金屬板塊740係用 以焊接固定該第二印刷電路板712、該第五印刷電路板 738及該第四印刷電路板736。 [0020] 該散熱鰭片726覆蓋住該筒狀外殼724的一端，該空心筒 狀頸部706覆蓋住該筒狀外殼724的另一端；該筒狀外殼 724包覆該承載體7〇2、該空心凸塊704、該前端凸塊734 、該末端凸塊708、該第一印刷電路板710、該第二印刷 電路板712、該可撓導線714、該第三印刷電路板718、 該保護蓋體720、該第四印刷電路板736、該第五印刷電 路板738、該金屬板塊740、該隔離蓋體722及該些螺絲 728 ° [0021] 本創作之小型化之衛星集波器70更包含至少一開孔殼體 730及至少一墊片732。 [0022] 該筒狀外殼724包含至少一開孔7242 ;該纜線接頭716係 穿過該開孔7242，藉由該開孔殼體730及該墊片732固定 於該筒狀外殼724的表面。 [0023] 此外，該承載體702包含至少一承載體螺絲孔7026 ;該前 表單編號A0101 第8頁/共32頁 [0024] 端凸塊734包含至少一前端凸塊螺絲孔？342，該末端凸塊 708包含至少一末端凸塊螺絲孔7082。 該第一印刷電路板7iG包含至少-第1刷電路板螺絲孔 7102，該螺絲728通過該第一印刷電路板螺 ⑽及 該承載體螺絲孔7〇26將該第-印刷電路板71㈣㈣該承 載體第一面7022。 [0025] 該隔離蓋體722包含至少-隔離蓋體螺絲孔？222，該螺絲 728通過該隔離蓋體螺絲孔7222、該第—印刷電路板螺絲 孔71 02及該承載體螺絲孔7026將該隔離蓋體722螺固於 該第一印刷電路板71〇。 [0026] 該第二印刷電路板712包含至少一第二印刷電路板螺絲孔 7122 ’該螺絲728通過該第二印刷電路板螺絲孔7122及 該前端凸塊螺絲孔7342將該第二印刷電路板712螺固於該 前端凸塊734 ;該螺絲728通過該第二印刷電路板螺絲孔 7122及該末端凸塊螺絲孔7082將該第二印刷電路板712 螺固於該末端凸塊708。 [0027] 該第三印刷電路板718包含至少一第三印刷電路板螺絲孔 7182 ’該螺絲728通過該第三印刷電路板螺絲孔7182及 該承載體螺絲孔7026將該第三印刷電路板718螺固於該承 載體第二面7024 » [0028] 該保護蓋體720包含至少一保護蓋體螺絲孔7202，該螺絲 728通過該保護蓋體螺絲孔7202、該第三印刷電路板螺絲 孔7182及該承載體螺絲孔7〇26將該保護蓋體720螺固於 該第三印刷電路板718。 表單编號Α0101 第9頁/共32頁 M422177 [0029] 該第四印刷電路板736包含至少一第四印刷電路板螺絲孔 7362，該螺絲728通過該第四印刷電路板螺絲孔7362將 該第四印刷電路板736螺固於該承載體702的侧面。 [0030] 該金屬板塊740包含至少一金屬板塊螺絲孔7402，該螺絲 7 2 8通過該金屬板塊螺絲孔7 4 0 2、該前端凸塊螺絲孔 7342及該末端凸塊螺絲孔7082將該金屬板塊740螺固於 該前端凸塊734及該末端凸塊708。 [0031] 該承載體7〇2的材質係為金屬；該空心凸塊m的材質係 為金屬；該空心筒狀頸部706的材質係為金屬；該前端凸 塊734的材質係為金屬；該末端凸塊708的材質係為金屬 ;該第一印刷電路板710佈有複數之電子零件（未圖示） ;該第二印刷電路板712佈有複數之電子‘零伴（未圖示） ;該可撓導線714可為例如RF cable線；該第三印刷電 路板718佈有複數之電子零件（未圖不），該保護蓋體 720的材質係為金屬；該隔離蓋體722的材質係為金屬； 該筒狀外殼724的材質係為金屬；該散熱鰭片726的材質 係為金屬。 [0〇32]本創作之小塑化之衛星集波器70更包含一衛星集波器之 介質結構30，設置於該空心筒狀頸部706的一端，該衛星 集波器之介質結構30係用以使衛星信號能良好地折射傳 遞進入衛星集波器，茲詳述如下。 C〇〇33]請參考第九圖，其係為本創作之衛星集波器之介質結構 之一應用實施例外觀立體示意圖。請參考第十圖，其係 為本創作之衛星集波器之介質結構之一應用實施例剖視 示意圖。 表單編號A0101 第10頁/共32頁 [0034] [0034] [0035] [0036] [0037] [0038] [0039] 考第'、圖，其係為本創作之衛星集波器之介質結構 之一實施例外觀立體示意圖（導波本體與導波外罩結合 刖）’並請同時參考第七圖’其係為本創作之衛星集波 斋之介質結構之-實施例剖視示意圖（導波本體與導波 外罩結合前）；並請同時參考第八圖，其係為本創作之 访生集波器之；丨質結構之一實施例剖視示意圖（導波本 體與導波外罩結合後）。 該衛星集波器之介質結構30包含一導波本體1〇及一導波 外罩20。 該導波本體10包含一本體結構1〇2、一第一凸柱1〇4、一 第二凸枉106、一導波凸體108、一第一環狀溝槽112、 一第二環狀溝槽114及一環狀卡掣部116。 該第一凸柱104係延伸自該本體結構丨〇2的一端；該第二 凸柱106係與該第一凸柱1〇4反向延伸自該本體結構1〇2 的另一端。 該第一凸柱104開設一第一開口 1042 ;該本體結構1〇2向 該第一開口 1042方向延伸出該導波凸體1〇8。該第二凸柱 106開設一第二開口 1〇62 ;該第二開口 1062與該第一開 口 1042反向；該本體結構1〇2向該第二開口 1〇62方向開 設出一導波通道110。該導波通道11〇係為由窄到寬而連 至該第二開口 1 062。 該第一環狀溝槽112設置於該第一凸柱104及該本體結構 102之間的表面；該第二環狀溝槽114設置於該第二凸柱 10 6及該本體結構10 2之間的表面；該環狀卡掣部116設 表單編號A0101 第11頁/共32頁 M422177 置於該本體結構102的表面》 [0040] 在一具體之實施例，該本體結構102係為—圓柱體；該第 —凸柱104係為一圓柱體；該第二凸柱1〇6係為—圓柱體 ，該皮凸體1〇8係為一圓錐體，其頂點可與該第一開口 1042切齊，或是低於該第一開口 1〇42 ,或是高於該第一 開口 1042 ;該第一開口 1 〇42係為一圓形；該第二開口 1062係為一圓形。本創作上述元件部位並不y上述之圓 柱體、圓錐體或圓形為限，亦可為圓台體或方形、橢圓 形等等幾何形體達成。 [0041] 在一具體之實施例，該導波通道no係為由窄到寬分成三 等份’前段及中段為空心圓柱體，中段的空心圓柱體的 . / 直徑大於前段的空心圓柱體的直徑，末段今空心圓台； 然本創作之該導波通道110並不以上述為限，亦可為由窄 到寬分成兩等份或超過三等份’甚至可為一喇„八形狀； 且每一段並不限定如上述為空心圓柱罈尽空心圓台，亦 • ' : · · 可為空心圓錐體、空心圓柱體及窣心圓台等等之組合。 [0042] 該導波外罩20可為空心圓柱體或空心圓台體，用以罩蓋 住該導波本體10 ;衛星集波器係設置於戶外，難免會有 雨水殘留於介質結構上而影響電磁波之接收，或是有不 可預期的外力而造成介質結構的損壞；而該導波外罩2〇 罩蓋住該導波本體10將可兼具防水及保護該導波本體10 的功效。 [0043] 該導波外罩20包含一外罩頂面202、一外罩開口 204、至 少一凸肋條206、一凸塊208及一環狀抵掣部210。 表單編號A0101 第12頁/共32頁 M422177 [0044] 該外罩開口 204係相對於該外罩頂面202開設；該凸肋條 206設置於該導波外罩20内壁環繞該外罩開口 204，藉以 使該衛星集波器之介質結構30與跟該衛星集波器40結合 時產生緊扣的效果；該凸塊208設置於該導波外罩20内壁 靠近該外罩開口 204 ;該環狀抵掣部210設置於該導波外 罩20内壁，係用以擋掣該環狀卡掣部116。 [0045] 在一具體之實施例’該導波本體10的材質為非金屬材質 (例如塑膠、玻璃、壓克力等等，以使衛星信號能折射 傳遞進入衛星集波器）；該導波外罩20的材質為非金屬 • 材質（例如塑膠、玻璃、壓克力等等，以使衛星信號能 折射傳遞進入衛星集波器）。該外罩頂面202為透明，藉 以增加介質結構内部之辨識度。 [〇〇46] 該衛星集波器之介質結構30係設置在衛星集波器前端’ 藉以使衛星信號（電磁波）可經過折射後進入LNB的頸部 金屬結構，再經過LNB承載體空心凸塊中的兩隻接收pin 針’以進入LNB的電路；該衛星集波器之介質結構30的特 隹殊構造將使電磁波折射傳遞效果優良，因此衛星集波器 能接收到良好的衛星信號，以進行後續之信號放大及降 頻。 [0047] 本創作之/丨、开〗. < i 化之衛星集波器係將傳統之衛星集波器外 ^縮]以達到最佳化的multi-feed的應用；本創作之 J 化之衛星集波器係將傳統印刷電路板以功能分割成 數個印刷雷!^ 1 $格板’再利用RF cable達成彼此之間的電性 連接*利用D Ε» cable的可撓性達成小型化的目的；再者 些輸出輪入的連接器傳統作法是直接焊接在印刷電 表單編號A0101 第13頁/共32頁 M422177 路板上’本創作則亦是利用RF cable予以連接，如此輸 出輸入的連接器的位置可隨外型而放置在適當位置；本 創作之外觀採用圓管式，將可創造出最有效利用的空間 ，以縮小整體體積。 麵综上所述，當知本_已具有產業利雜、賴性與進 步性，又本創作之構造亦未曾見於同類產品及公開使用 ，完全符合新型專射請要件，爰依專利法提出申請。 【圖式簡單說明】 [0049]第一圖為習知衛星集波器剖視透明圖。 圆帛三圖為本創作之小型化之衛星集㈣立體分解圖。 [0051]帛三圖為本創作之小型化之衛星集波器另一角度之立體 分解圖。 剛第四目為本創作之小型化讀星驗S透視圖。 [0053] 第五圖為本創作之小型化之衛星集波器另一角度之透視 圖。 [0054] 第六圖為本創作之衛星集波器之介質結構之一實施例外 觀立體示意圖（導波本體與導波外罩結合前）。 闺第*b ®為賴作之衛星集波器之介諸構之—實施例剖 視示意圖（導波本體與導波外罩結合前）。 [0056] 第八圖為本創作之衛星集波器之介質結構之一實施例剖 視示意圖（導波本體與導波外罩結合後）。 [0057] 第九圖為本創作之衛星集波器之介質結構之一應用實施 例外觀立體示意圖。 表單編號A0101 第14頁/共32頁 M422177M422177 V. New description: [New technology field] [0001] [0002] In particular, a miniaturization of this creation department is related to a satellite wave collector and a satellite wave collector. [Prior Art] Satellite concentrator, also known as low noise down-converter (L )w noise block downconverter, commonly referred to as LNB), is a low noise amp Ufier (commonly referred to as LNC (low block). Down converter) The frequency reducer is also merged by D. [0003] The role of the satellite wave collector is to amplify and down-convert the satellite signal; the satellite moment is about 30,000 kilometers away from the ground, and the transmitted satellite signal It is quite weak before arriving at the dish antenna. So the satellite wave collector is needed for signal amplification. The satellite wave collector will first amplify the high-frequency satellite signal by hundreds of thousands of times, and then use this seismic circuit to convert the high frequency. Switch to intermediate frequency to facilitate coaxial cable transmission and satellite receiver demodulation. [0004] Coaxial cable is connected between satellite wave collector and satellite receiver; due to the higher frequency of coaxial cable transmission, signal loss The larger the satellite collector is, the local oscillator circuit is used to convert the satellite signal from high frequency to intermediate frequency to facilitate the transmission of the coaxial cable and the demodulation of the satellite receiver. The waver can down-convert the satellite signal from 3.4~4.2GHz (C band) or 0.7~12.75GHz (Ku band) to the intermediate frequency required by the satellite receiver (950MHz~2050MHz, and determine the intermediate frequency range according to the type of satellite wave collector. Finally, the sound and image can be displayed on the TV. Form No. A0101 Page 4 of 32 [0005] Please refer to the first figure, which is a transparent view of the conventional satellite wave collector. The wave concentrator 60 includes a main frame 602, an L-shaped frame 604, a first printed circuit board 606, a second printed circuit board 608, and an L-shaped housing 610. The first printed circuit board 606 is disposed on the L One side of the skeleton 604, the second printed circuit board 608 is disposed on the other side of the L-shaped skeleton 604; the frame 604 is disposed on the main frame 602; the L-shaped casing 610 is coated The main skeleton 602, the L-shaped bobbin 604, the first printed circuit board 606, and the second printed circuit board 608. [0006] Satellite signals transmitted by satellites (not shown) pass through a dish antenna (not shown) After reflection, enter the conventional satellite wave collector 60 to perform amplification and down-conversion operations; A shaft cable (not shown) is transmitted to a satellite receiver (not shown) to display a facial image and sound of the satellite program on a television (not shown). [0007] In a specific embodiment, The conventional satellite wave concentrator 60 is mounted in front of the dish to collect satellite signals; the more the conventional satellite concentrator 60, the larger the disk area of the dish antenna needs to be. The larger the dish area of the dish antenna, the higher the price of the dish antenna. The conventional satellite wave concentrator 60 as shown in the first figure, because of the L-shaped skeleton 604 and the L-shaped design of the L-shaped outer casing 610, will make the conventional satellite concentrator 60 quite bulky. When the conventional satellite wave finder 60 is bulky and requires a large number of conventional satellite concentrators 60 to be applied, the dish area of the dish antenna needs to be larger, and thus the price of the dish antenna The more it is 13⁄4. [0009] Therefore, in order to reduce the disk area of the dish to reduce the price of the dish-shaped form number A0101 page 5 / 32 pages M422177 line, how can we develop a smaller satellite wave collector? It is an important topic for the moment. [New Content] [0010] In order to improve the above disadvantages of the prior art, the aim of the present invention is to provide a miniaturized satellite wave concentrator. [0011] In order to achieve the above object of the present invention, the miniaturized satellite wave concentrator of the present invention comprises: a carrier comprising a first side of a carrier and a second side of a carrier, the first side of the carrier and The second surface of the carrier is reversely disposed; a hollow bump is disposed at one end of the first surface of the carrier; a hollow cylindrical neck is disposed at one end of the hollow bump; and an end bump And the other end of the first surface of the carrier is opposite to the hollow bump; at least one front end bump is adjacent to the end of the hollow bump disposed on the first surface of the carrier; a first printed circuit board Provided on the first side of the carrier; a second printed circuit board disposed on the front end bump and the end bump; and at least one flexible wire soldered to the first printed circuit board and the second Between the printed circuit boards, an electrical connection between the first printed circuit board and the second printed circuit board is achieved. [0012] The effect of this creation is to miniaturize the satellite wave collector. [Embodiment] [0013] Please refer to the second figure, which is a three-dimensional exploded view of the miniaturized satellite wave collector of the present invention; and also refers to the third figure, which is the miniaturized satellite wave collection of the creation. An exploded view of the other angle of the device; and please refer to the fourth figure at the same time, which is a perspective view of the miniaturized satellite wave collector of the creation; and also refer to the fifth figure, which is the miniaturization of the creation. A perspective view of another angle of the satellite wave collector. Form No. A0101 Page 6 of 32 [0014] The miniaturized satellite wave collector 7〇 of the present invention comprises a carrier 7〇2, a hollow protrusion 704, a hollow cylindrical neck 7〇6, at least a front end bump (3), an end bump 708, a first printed circuit board 71, a second printed circuit board Π2, and at least one flexible wire 714. [0015] The carrier 702 includes a first side of the carrier 7〇22 and a second surface 7024 of the carrier, the first surface 7022 of the carrier and the second surface 7〇24 of the carrier are arranged in opposite directions. [0016] The hollow protrusion 704 is disposed at one end of the first surface 7022 of the carrier; the hollow cylindrical neck 706 is disposed at one end of the hollow protrusion 704; the front end protrusion 734 is adjacent to the hollow protrusion The block 704 is disposed at one end of the first surface 7022 of the carrier; the end bump 708 is disposed at the other end of the first surface 7022 of the carrier relative to the hollow bump 7〇4. [0017] The first printed circuit board 710 is disposed on the first surface 7022 of the carrier; the second printed circuit board 712 is disposed on the front end bump 734 and the end bump 708; the flexible wire 714 is soldered to Between the first printed circuit board 71 and the second printed circuit board 712 to achieve electrical connection between the first printed circuit board 710 and the second printed circuit board 712 [0018] The satellite collector 7 further includes at least one wire joint 716, a third printed circuit board 718, a protective cover 720, an isolation cover 722, a cylindrical casing 724, a heat sink II 726, and a plurality of The screw 728, a fourth printed circuit board 736, a fifth printed circuit board 738 and a metal plate 740. The flexible wire 714 is soldered between the continuation wire connector 716 and the second printed circuit board 712 to achieve the cable connector 716 and the second printed circuit board form number A0101. Page 7 of 32 [0019 An electrical connection between the M422177 712; the third printed circuit board 718 is disposed on the second surface 7024 of the carrier, and the flexible wire 714 is soldered to the third printed circuit board 718 and the second printed circuit board 712 The electrical connection between the first printed circuit board 718 and the second printed circuit board 712 is achieved. The protective cover 720 is disposed on the third printed circuit board 718; the isolating cover 722 is disposed Between the first printed circuit board 710 and the second printed circuit board 712; the fourth printed circuit board 736 is screwed to the side of the carrier 702; the fifth printed circuit board 738 and the second printed circuit board The 712 and the fourth printed circuit board 736 are soldered; the metal block 740 is used for soldering and fixing the second printed circuit board 712, the fifth printed circuit board 738, and the fourth printed circuit board 736. [0020] The heat dissipation fin 726 covers one end of the cylindrical casing 724, and the hollow cylindrical neck portion 706 covers the other end of the cylindrical casing 724; the cylindrical casing 724 covers the carrier body 〇2 The hollow bump 704, the front end bump 734, the end bump 708, the first printed circuit board 710, the second printed circuit board 712, the flexible wire 714, the third printed circuit board 718, the protection The cover 720, the fourth printed circuit board 736, the fifth printed circuit board 738, the metal plate 740, the isolation cover 722, and the screws 728 ° [0021] The miniaturized satellite wave concentrator 70 of the present invention Further comprising at least one aperture housing 730 and at least one spacer 732. [0022] The cylindrical casing 724 includes at least one opening 7242; the cable joint 716 passes through the opening 7242, and the opening shell 730 and the gasket 732 are fixed to the surface of the cylindrical casing 724. . [0023] In addition, the carrier 702 includes at least one carrier screw hole 7026; the front form number A0101, page 8 of 32 [0024] The end bump 734 includes at least one front end bump screw hole? 342. The end bump 708 includes at least one end bump screw hole 7082. The first printed circuit board 7iG includes at least a first brush circuit board screw hole 7102. The screw 728 carries the first printed circuit board 71 (4) (4) through the first printed circuit board screw (10) and the carrier screw hole 7〇26. The first side of the body is 7022. [0025] The isolation cover 722 includes at least a separate cover screw hole? 222. The screw 728 is screwed to the first printed circuit board 71 by the isolation cover screw hole 7222, the first printed circuit board screw hole 71 02 and the carrier screw hole 7026. The second printed circuit board 712 includes at least one second printed circuit board screw hole 7122. The screw 728 passes the second printed circuit board screw hole 7122 and the front end bump screw hole 7342 to the second printed circuit board. The second printed circuit board 712 is screwed to the end bump 708 through the second printed circuit board screw hole 7122 and the end bump screw hole 7082. [0027] The third printed circuit board 718 includes at least a third printed circuit board screw hole 7182. The screw 728 passes the third printed circuit board screw hole 7182 and the carrier screw hole 7026 to the third printed circuit board 718. Screwed on the second surface of the carrier 7024 » [0028] The protective cover 720 includes at least one protective cover screw hole 7202, the screw 728 passes through the protective cover screw hole 7202, the third printed circuit board screw hole 7182 And the carrier screw hole 7 〇 26 screwes the protective cover 720 to the third printed circuit board 718. Form No. 1010101 Page 9 of 32 M422177 [0029] The fourth printed circuit board 736 includes at least a fourth printed circuit board screw hole 7362, the screw 728 passing the fourth printed circuit board screw hole 7362 Four printed circuit boards 736 are screwed to the sides of the carrier 702. [0030] The metal plate 740 includes at least one metal plate screw hole 7402, the screw 7 2 8 passes the metal plate screw hole 7 4 0 2, the front end bump screw hole 7342 and the end bump screw hole 7082 A plate 740 is screwed to the front end bump 734 and the end bump 708. [0031] The material of the carrier 7〇2 is metal; the material of the hollow bump m is metal; the material of the hollow cylindrical neck 706 is metal; the material of the front bump 734 is metal; The material of the end bump 708 is metal; the first printed circuit board 710 is provided with a plurality of electronic components (not shown); the second printed circuit board 712 is provided with a plurality of electronic 'zero companions (not shown) The flexible wire 714 can be, for example, an RF cable; the third printed circuit board 718 is provided with a plurality of electronic components (not shown), and the protective cover 720 is made of metal; the material of the isolation cover 722 The material of the cylindrical casing 724 is metal; the material of the heat dissipation fin 726 is metal. [032] The small plasticized satellite wave concentrator 70 of the present invention further comprises a medium structure 30 of a satellite concentrator, which is disposed at one end of the hollow cylindrical neck 706, and the medium structure 30 of the satellite concentrator It is used to make the satellite signal transmit well into the satellite wave collector, as detailed below. C〇〇33] Please refer to the ninth figure, which is a three-dimensional schematic diagram of an application embodiment of the media structure of the satellite wave collector of the present invention. Please refer to the tenth figure, which is a schematic cross-sectional view of an application embodiment of the media structure of the satellite wave collector of the present invention. Form No. A0101 Page 10 / Total 32 Pages [0034] [0037] [0039] [0039] [0039] [0039] This is the media structure of the satellite wave collector of the present creation. A schematic diagram of the appearance of one embodiment (the waveguide body and the waveguide cover are combined with 刖)' and please refer to the seventh figure at the same time. The body and the wave guide cover are combined before; and please refer to the eighth figure at the same time, which is the access wave collector of the present invention; a schematic cross-sectional view of one embodiment of the enamel structure (the guided wave body and the wave guide cover are combined) ). The dielectric structure 30 of the satellite concentrator includes a waveguide body 1 〇 and a waveguide cover 20. The waveguide body 10 includes a body structure 1〇2, a first protrusion 1〇4, a second protrusion 106, a waveguide protrusion 108, a first annular groove 112, and a second ring. The groove 114 and an annular latch portion 116. The first stud 104 extends from one end of the body structure 丨〇2; the second stud 106 extends from the other end of the body structure 1〇2 in opposite directions from the first stud 1〇4. The first protrusion 104 defines a first opening 1042. The body structure 1〇2 extends the guiding protrusion 1〇8 in the direction of the first opening 1042. The second protrusion 106 defines a second opening 1 〇 62; the second opening 1062 is opposite to the first opening 1042; the body structure 1 〇 2 opens a waveguide channel in the direction of the second opening 1 〇 62 110. The waveguide channel 11 is connected to the second opening 1 062 from narrow to wide. The first annular groove 112 is disposed on a surface between the first protrusion 104 and the body structure 102; the second annular groove 114 is disposed on the second protrusion 106 and the body structure 10 2 The surface of the annular latching portion 116 is provided with the form number A0101, page 11 / 32 pages, M422177, placed on the surface of the body structure 102. [0040] In a specific embodiment, the body structure 102 is a cylinder The first protrusions 104 are a cylinder; the second protrusions 1〇6 are a cylinder, and the protrusions 1〇8 are a cone whose apex can be connected with the first opening 1042. Sheaving is either lower than the first opening 1 〇 42 or higher than the first opening 1042; the first opening 1 〇 42 is a circle; the second opening 1062 is a circle. The above-mentioned component parts of the present invention are not limited to the above-mentioned circular cylinder, cone or circle, and may be achieved by a truncated cone body, a square shape, an elliptical shape or the like. [0041] In a specific embodiment, the waveguide channel no is divided into three equal parts from the narrow to the wide front and the middle section is a hollow cylinder, and the hollow cylinder of the middle section is larger than the hollow cylinder of the front section. Diameter, the end of the hollow circular table; however, the waveguide channel 110 of the present invention is not limited to the above, and may be divided into two equal parts or more than three equal parts from narrow to wide 'or even a à eight shape And each segment is not limited to the hollow cylindrical table as described above, and also: ' : · · It can be a combination of hollow cone, hollow cylinder and 圆 round table, etc. [0042] The waveguide cover 20 may be a hollow cylinder or a hollow circular platform for covering the waveguide body 10; the satellite wave collector is disposed outdoors, and it is inevitable that rainwater may remain on the medium structure to affect the reception of electromagnetic waves, or Unexpected external force causes damage to the dielectric structure; and the waveguide cover 2 covers the waveguide body 10 to provide both waterproofing and protection of the waveguide body 10. [0043] The waveguide cover 20 includes a cover top surface 202, a cover opening 204, at least a rib 206, a bump 208 and an annular abutment 210. Form No. A0101 Page 12 of 32 M422177 [0044] The cover opening 204 is opened relative to the top surface 202 of the cover; the rib 206 The inner wall of the waveguide cover 20 surrounds the cover opening 204, so that the medium structure 30 of the satellite wave collector and the satellite wave collector 40 are combined to produce a fastening effect; the bump 208 is disposed on the guided wave. The inner wall of the outer cover 20 is adjacent to the outer cover opening 204; the annular abutting portion 210 is disposed on the inner wall of the outer wave guide cover 20 for blocking the annular latch portion 116. [0045] In a specific embodiment The wave body 10 is made of a non-metallic material (such as plastic, glass, acrylic, etc., so that the satellite signal can be refracted and transmitted into the satellite wave collector); the waveguide cover 20 is made of a non-metal material (such as plastic). , glass, acrylic, etc., so that the satellite signal can be refracted into the satellite wave collector. The top surface 202 of the cover is transparent, thereby increasing the internal identification of the medium structure. [〇〇46] The satellite wave collector The medium structure 30 is set in the satellite set The front end of the device is such that the satellite signal (electromagnetic wave) can be refracted into the metal structure of the neck of the LNB, and then through the two receiving pins of the LNB carrier hollow bumps to enter the circuit of the LNB; the satellite concentrator The special structure of the dielectric structure 30 will make the electromagnetic wave refraction transmission effect excellent, so the satellite wave collector can receive a good satellite signal for subsequent signal amplification and frequency reduction. [0047] The creation / 丨, 开< i. The satellite wave collector is used to optimize the traditional satellite wave collector to achieve optimized multi-feed application; the J-shaped satellite wave collector of this creation will be a traditional printed circuit board. Divided into several printing mines by function! ^ 1 Grid 're-use RF cable to achieve electrical connection with each other* Use D Ε» cable flexibility to achieve miniaturization; and some output wheeled connections The traditional method is to directly solder on the printed circuit form No. A0101 page 13 / 32 pages M422177 board 'This creation is also connected by RF cable, so the position of the output input connector can be placed with the appearance appropriate Set; appearance of the Original Tubular employed, would create the most efficient use of space, in order to reduce the overall volume. In summary, when Zhiben_ has industrial miscellaneous, reliance and progress, and the structure of this creation has not been seen in similar products and public use, it fully meets the requirements of new special shots, and applies for patent law. . BRIEF DESCRIPTION OF THE DRAWINGS [0049] The first figure is a cross-sectional transparent view of a conventional satellite wave collector. The three figures of the circle are the three-dimensional exploded view of the miniaturized satellite set (4). [0051] The third figure is a perspective exploded view of another angle of the miniaturized satellite wave collector. Just the fourth item is the perspective of the small-scale reading star S of the creation. [0053] The fifth figure is a perspective view of another angle of the miniaturized satellite wave collector. [0054] The sixth figure is a schematic diagram of an implementation of one of the dielectric structures of the satellite wave collector of the present invention (before the waveguide body and the waveguide cover are combined).闺 *b ® is the construction of the satellite wave concentrator - a schematic cross-sectional view of the embodiment (before the waveguide body and the waveguide cover are combined). [0056] The eighth figure is a schematic cross-sectional view of an embodiment of the dielectric structure of the satellite wave collector of the present invention (after the waveguide body and the waveguide cover are combined). [0057] The ninth drawing is a perspective view showing an appearance of an application embodiment of the medium structure of the satellite wave collector of the present invention. Form No. A0101 Page 14 of 32 M422177
[0058] 第十圖為本創作之衛星集波器之介質結構之一應用實施 例剖視示意圖。 【主要元件符號說明】 [0059] 習知衛星集波器60 [0060] 主骨架602 [0061] L型骨架604 [0062] 第一印電路板606 [0063] 第二印刷電路板608 [0064] L型外殼610 [0065] 小型化之衛星集波器70 [0066] 承載體702 [0067] 承載體第一面7022 [0068] 承載體第二面7024 [0069] 承載體螺絲孔7026 [0070] 空心凸塊7 0 4 [0071] 空心筒狀頸部706 [0072] 末端凸塊7 0 8 [0073] 末端凸塊螺絲孔7 0 8 2 [0074] 第一印刷電路板710 [0075] 第一印刷電路板螺絲孔71 0 2 表單编號A0101 第15頁/共32頁 M422177 [0076] 第二印刷電路板712 [0077] 第二印刷電路板螺絲孔7122 [0078] 可撓導線714 [0079] 纜線接頭716 [0080] 第三印刷電路板718 [0081] 第三印刷電路板螺絲孔7182 [0082] 保護蓋體720 [0083] 保護蓋體螺絲孔7202 [0084] 隔離蓋體722 [0085] 隔離蓋體螺絲孔7222 [0086] 筒狀外殼724 [0087] 開孔7242 [0088] 散熱鰭片726 [0089] 螺絲728 [0090] 開孔殼體730 [0091] 墊片732 [0092] 前端凸塊734 [0093] 前端凸塊螺絲孔7342 [0094] 第四印刷電路板736 [0095] 第四印刷電路板螺絲孔7362 表單編號A0101 第16頁/共32頁 M422.177 [0096] 第五印刷電路板738 [0097] 金屬板塊740 [0098] 金屬板塊螺絲孔7402 [0099] 衛星集波器之介質結構30 [0100] 導波本體10 [0101] 本體結構102 [0102] 第一凸柱104 [0103] 第一開口 1042 [0104] 第二凸柱 106 [0105] 第二開口 1062 [0106] 導波凸體108 [0107] 導波通道110 [0108] 第一環狀溝槽112 [0109] 第二環狀溝槽114 [0110] 環狀卡掣部116 [0111] 導波外罩20 [0112] 外罩頂面202 [0113] 外罩開口 204 [0114] 凸肋條20 6 [0115] 凸塊2 08 第17頁/共32頁 表單編號A0101 M422177 [0116] 環狀抵掣部210 表單編號A0101 第18頁/共32頁[0058] FIG. 10 is a schematic cross-sectional view showing an application embodiment of a dielectric structure of the satellite wave collector of the present invention. [Main Component Symbol Description] [0059] The conventional skeleton 602 [0060] The main skeleton 602 [0061] The L-shaped bobbin 604 [0062] The first printed circuit board 606 [0063] The second printed circuit board 608 [0064] L-shaped housing 610 [0065] Miniaturized satellite wave concentrator 70 [0066] carrier body first surface 7022 [0068] carrier body second surface 7024 [0069] carrier body screw hole 7026 [0070] Hollow Bumps 7 0 4 [0071] Hollow Cylindrical Neck 706 [0072] End Bumps 7 0 8 [0073] End Bump Screw Holes 7 0 8 2 [0074] First Printed Circuit Board 710 [0075] Printed Circuit Board Screw Holes 71 0 2 Form No. A0101 Page 15 / Total 32 Pages M422177 [0076] Second Printed Circuit Board 712 [0077] Second Printed Circuit Board Screw Holes 7122 [0078] Flexible Wire 714 [0079] Cable Connector 716 [0080] Third Printed Circuit Board 718 [0081] Third Printed Circuit Board Screw Hole 7182 [0082] Protective Cover 720 [0083] Protective Cover Screw Hole 7202 [0084] Isolation Cover 722 [0085] Isolation cover screw hole 7222 [0086] cylindrical housing 724 [0087] opening 7242 [0088] heat dissipation fin 726 [0089] screw 728 [0090] opening Body 730 [0091] Gasket 732 [0092] Front End Bump 734 [0093] Front End Bump Screw Hole 7342 [0094] Fourth Printed Circuit Board 736 [0095] Fourth Printed Circuit Board Screw Hole 7362 Form No. A0101 Page 16 / Total 32 pages M422.177 [0096] Fifth printed circuit board 738 [0097] Metal plate screw hole 7402 [0099] Medium structure of satellite wave collector 30 [0100] Guide wave body 10 [0101 The body structure 102 [0102] The first protrusion 104 [0103] The first opening 1042 [0104] The second protrusion 106 [0105] The second opening 1062 [0106] The guided wave convex body 108 [0107] The guided wave channel 110 [ 0108] First annular groove 112 [0109] Second annular groove 114 [0110] Annular casing portion 116 [0111] Guide wave outer cover 20 [0112] Cover top surface 202 [0113] Cover opening 204 [0114 ] rib 20 6 [0115] Bump 2 08 Page 17 of 32 Form No. A0101 M422177 [0116] Annular abutment 210 Form No. A0101 Page 18 of 32