201017971 九、發明說明： 【發明所屬之技術領域】 本發明是有關於一種調整衛星天線的基座，特 別是指一種可精確微調水平與垂直方位的衛星天線 調整裝置。 【先前技術】 針對衛星天線（碟形天線）的使用，為了達到較 佳的接收角度，一般作法會在衛星天線的盤體與支 撐柱之間，裝設有一組可調整角度的調整座，而此 調整座提供了 X轴方向與γ軸方向之操作調整， 藉由X轴與Y軸的搭配調整，以期達到最佳的接 收角度，使電子設備能獲得清晰無雜質的收訊效果 〇 習知的衛星天線調整座，其角度調整的機構， 一般是利用孔對孔的對位，或是單孔對長條孔的對 位方式，達到固定幅度的調整效果，但是，孔對孔 的對位方式，因波段大而無法獲得精密的微調效果 ;單孔對長條孔的對位方式，單憑使用經驗來調整 幅度，操作不易，且幅度調整後，再鎖上螺絲，才 是最後調整的位置，因此，在調整的過程中，無波 段的長條孔，並無法獲得立即的定位，所以待鎖上 螺栓過程中，已位移的調幅還是容易受影響，進而 失去精確調整的效果。 如上所述，現有以孔位對正的調整結構，不但 5 201017971 操作不易、構件繁複，而且不夠精確，使用上仍不 夠精良，充其量只能歸類於粗調的調整方式，因此 ，有必要再尋求解決之道。 【發明内容】 本發明係提供一種衛星天線調整裝置，藉由齒輪 與齒排的嚅合關係，使衛星天線可依天線支撐桿為基 準，以水平方位與垂直方位作精準無誤的微調效果， 而且操作上相當簡易，且構件簡單。 於是，本發明衛星天線調整裝置，供連接在衛星 天線與一天線支撐桿之間，包含一承盤基座、一支承 座、一連結座、一 X軸微調機構及一 γ軸微調機構 。該承盤基座是結合於該衛星天線的一盤面上。該支 承座是結合於該天線支撐桿上。該連結座是連結在該 承盤基座與該支承座之間。該X轴微調機構是結合於 該支承座與該連結座之間，利用齒輪與齒排的嚅合關 係，連動該承盤基座，使得衛星天線以該天線支撐桿 為基準，產生X軸方向之微幅運動。該Y軸微調機 構是結合於該連結座與該承盤基座之間，利用齒輪與 齒排的嚅合關係，連動該連結座與承盤基座，使得衛 星天線得以該天線支撐桿為基準，產生Y軸方向之微 幅運動。 依照上述本發明之衛星天線調整裝置，其中該承 盤基座包含一底架、一爪固架及一接合架，該爪固架 是結合於衛星天線的盤面上，該底架自該爪固架向外 201017971 延伸，使衛星天線的周緣抵接在底架上，該接合架係 自該爪固架朝向遠離於該衛星天線盤面的方向延伸。 該支承座包含一承盤、一結合架及一套接管，該套接 管是連接在該天線支撐桿上，該承盤是安置於該套接 管上。該連結座包含一底壁與二侧壁。該X轴微調機 構包含相互嚙合的一第一齒輪與一第一齒排，該第一 齒輪是軸固於該支承座的承盤上，該第一齒排是設置 於該連結座之底壁的側壁面上。該γ軸微調機構包含 相互嗡合的一第二齒輪與一第二齒排，該第二齒輪是 軸固於該承盤基座的接合架上，該第二齒排是設置於 該連結座之侧壁的侧壁面上。 依照上述本發明之衛星天線調整裝置，其中該第 一齒排係呈圓弧形，該支承座的承盤具有一圓弧長條 孔，此長條孔的形狀是依據該第一齒排的曲線而設。 依照上述本發明之衛星天線調整裝置，其中該第 二齒排係呈圓弧形，該承盤基座的接合架具有一圓弧 長條孔，該長條孔的形狀是依據該第二齒排的曲線而 設。 依照上述本發明之衛星天線調整裝置，其中該承 盤基座包含一基座主體及多數個耳片，此些耳片是鎖 固於該衛星天線的盤面上，該支承座包含一底壁、二 側壁、一夾凹部及一微調孔，該夾凹部是挾抵於該天 線支撐桿上。該連結座包含一底壁、二侧壁、一内槻 板、一外槻板及一調整孔。該X軸微調機構包含相互 7 201017971 嚅合的一第一齒輪與一第一齒排，該第一齒排是設置 於該連結座之微調孔的孔緣上，該第一齒輪是穿置於 該微調孔且轴固於該支承座之外襯板上。該γ軸微調 機構包含相互嚅合的一第二齒輪與一第二齒排，該第 二齒排是設置於該連結座之調整孔的孔緣上，該第二 齒輪是穿置於該調整孔且轴固於該連結座之内襯板上 〇 依照上述本發明之衛星天線調整裝置，其中該第 一齒排係呈圓弧形，該支承座的側壁具有一圓弧長條 孔，該連結座的外襯板具有一鎖孔，該長條孔是對應 於該鎖孔，並鎖固於該連結座上，此長條孔的形狀是 依據該第一齒排的曲線而設。 依照上述本發明之衛星天線調整裝置，其中該第 二齒排係呈圓弧形，該連結座的侧壁具有一圓弧長條 孔，該連結座的内襯板具有一鎖孔，該長條孔是對應 於該鎖孔，並鎖固於該承盤基座上，且長條孔與鎖孔 的形狀是依據該第二齒排的曲線而設。 因此，本發明利用齒輪配合齒排的嚅合關係，使 X轴（左右侧角）與Y軸（仰角）的方位調整，皆能獲得 精密化的微調效果。此外該調整裝置整體構造簡單， 且操作上方便快速。 【實施方式】 本發明之衛星天線調整裝置具有以下功能：利用 齒輪配合齒排的嚅合關係，以獲得精密化的微調效果 201017971 嚆合的一第一齒輪與一第一齒排，該第一齒排是設置 於該連結座之微調孔的孔緣上，該第一齒輪是穿置於 該微調孔且軸固於該支承座之外襯板上。該Y軸微調 機構包含相互嚅合的一第二齒輪與一第二齒排，該第 二齒排是設置於該連結座之調整孔的孔緣上，該第二 齒輪是穿置於該調整孔且轴固於該連結座之内襯板上 〇 依照上述本發明之衛星天線調整裝置，其中該第 一齒排係呈圓弧形，該支承座的侧壁具有一圓弧長條 孔，該連結座的外襯板具有一鎖孔，該長條孔是對應 於該鎖孔，並鎖固於該連結座上，此長條孔的形狀是 依據該第一齒排的曲線而設。 依照上述本發明之衛星天線調整裝置，其中該第 二齒排係呈圓弧形，該連結座的侧壁具有一圓弧長條 孔，該連結座的内襯板具有一鎖孔，該長條孔是對應 於該鎖孔，並鎖固於該承盤基座上，且長條孔與鎖孔 的形狀是依據該第二齒排的曲線而設。 因此，本發明利用齒輪配合齒排的嚅合關係，使 X轴（左右側角）與Y軸（仰角）的方位調整，皆能獲得 精密化的微調效果。此外該調整裝置整體構造簡單， 且操作上方便快速。 【實施方式】 本發明之衛星天線調整裝置具有以下功能：利用 齒輪配合齒排的嚅合關係，以獲得精密化的微調效果 8 201017971 ，而且此調整裝置之構件簡單、操作容易。 參閱第1圖與第2圖，本發明衛星天線調整裝置 之第一實施例，供連接在一衛星天線100與一天線支 撐桿200之間。該調整裝置300包含一承盤基座10 、一支承座20、一連結座30、一第一齒輪40、一第 一齒排50、一第二齒輪60、一第二齒排70、複數個 螺栓80與複數個螺帽90。 該承盤基座10,供結合於該衛星天線1〇〇的一 盤面110上。該承盤基座10包含一底架11、一爪固 架12及一接合架13。該爪固架12是由螺栓80與螺 帽90鎖固於該衛星天線100的盤面110上。該底架 11自該爪固架12向外延伸，使衛星天線100的周緣 抵接在底架11上。該接合架13係自該爪固架12朝 向遠離於該衛星天線100盤面110的方向延伸。該接 合架13是一门形架體，利用螺栓80與螺帽90鎖固 於該爪固架12的後侧，且該接合架13的兩侧壁各設 有一圓弧長條孔131與一鎖孔132。 該支承座20是結合於該天線支撐桿200上。該 支承座20包含一承盤21及一套接管22。該套接管 22是利用螺栓80與螺帽90鎖固於該天線支撐桿200 上。該承盤21是水平安置於該套接管22上。 該連結座30是連結在該承盤基座10與該支承座 20之間。該連結座30包含一底壁31與二侧壁32。 該等侧壁32皆是一扇形板體。 9 201017971 該第一齒輪40與該第一齒排50構成X軸微調機 構，並且結合於該支承座20與該連結座30之間。該 第一齒輪40是軸固於該支承座20的承盤21上，該 第一齒排50是設置於該連結座30之底壁31的侧端 面上。 參照第1圖、第4圖與第5圖，該第一齒排50 係呈圓弧形，該支承座20的承盤21具有一圓弧長條 孔211，此長條孔211的形狀是依據該第一齒排50的 曲線而設，另外，在該連結座30之底壁31與承盤 21之間穿設有一組螺栓80、螺帽90，且螺栓80正 好在承盤21之長條孔211内。利用第一齒輪40與第 一齒排50的嚅合關係，以間接連動該承盤基座10， 使得衛星天線100以該天線支撐桿200為基準，產生 X軸方向之微幅運動，如第4圖箭頭X所示，假想線 所示的衛星天線100可向左樞轉或向右樞轉，進而達 到X軸方向之微調效果，待調整好後再以螺栓80及 螺帽90將連結座30與支承座20鎖固即完成。 該第二齒輪60與該第二齒排70構成Y軸微調機 構，並且結合於該承盤基座10與該連結座30之間。 該第二齒輪60是轴固於該承盤基座10的接合架13 上，該第二齒排70是設置於該連結座30之扇形侧壁 的端面上。 續配合參照第3圖，該第二齒排70係呈圓弧形 ，該第二齒排70的曲線是依據該承盤基座10之接合 201017971 板13的長條孔131形狀而設，另外，在接合架13與 連結座30之侧壁32間穿設有一組螺栓80、螺帽90 ，且螺栓80位在接合架13之長條孔131内。利用第 二齒輪60與第二齒排70的嚅合關係，以連動該連結 座30與承盤基座10，使得衛星天線100得以該天線 支撐桿200為基準，產生Y軸方向之微幅運動，如第 3圖箭頭Y所示，假想線所示的衛星天線100可向上 樞轉或向下樞轉，進而達到Y軸方向之微調效果，待 調整好後再以螺栓80及螺帽90將連結座30與承盤 基座10鎖固即完成。 據上可知，本發明的衛星天線調整裝置，齒輪、 齒排結合長條孔施以同步位移的作法，不但使衛星天 線100保有左右偏移調整與上下仰角之調整，更藉由 齒輪嚅合的關係，讓調幅更加微細精準，而達到精密 化的微調使用效果，此外，此調整裝置300的構造精 簡，操作容易，有助於安裝作業。 參閱第6圖，本發明衛星天線調整裝置之第二實 施例，供連接在一衛星天線100與一天線支撐桿200 之間，該調整裝置400包含一承盤基座500、一支承 座600、一連結座700、一第一齒輪40、一第一齒排 50、一第二齒輪60、一第二齒排70、複數個螺栓80 與複數個螺帽90。 續參閱第7圖與第8圖，該承盤基座500包含一 基座主體510及多數個耳片520。此些耳片520是鎖 11 201017971 固於該衛星天線100的盤面110上。 該支承座600包含一底壁610、二侧壁620、一 夾凹部630以及一設於其中一個侧壁620上的微調孔 640。該夾凹部630是辅以一夾片650與螺栓80、螺 帽90挾抵於該天線支撐桿200上。 該連結座700包含一底壁710、二侧壁720、一 内襯板730、一外襯板740及一設於其中一個侧壁 720上的調整孔750。 該第一齒輪40與第一齒排50組成X軸微調機構 ，該第一齒排50是設置於該支承座600之微調孔 640的孔緣上，該第一齒輪40是穿置於該微調孔640 且軸固於該連結座700之外襯板740上。且該第一齒 排50係呈圓弧形，該支承座600的側壁620具有一 圓弧長條孔621，該連結座700的外襯板740具有一 鎖孔741，該長條孔621是對應於該鎖孔741，並利 用螺栓80與螺帽90鎖固於該連結座700上，此長條 孔621的形狀是依據該第一齒排50的曲線而設。 該第二齒輪60與第二齒排70組成Y軸微調機構 ，該第二齒排70是設置於該連結座700之調整孔 750的孔緣上，該第二齒輪60是穿置於該調整孔750 且軸固於該連結座700之内襯板730上。該第二齒排 70係呈圓弧形，該連結座700的侧壁720具有一圓 弧長條孔721，該連結座700的内襯板730具有一鎖 孔731，該長條孔721是對應於該鎖孔731，並利用 12 201017971 螺栓80、螺帽90將連結座700鎖固於該承盤基座 500上，且長條孔721與鎖孔731的形狀是依據該第 二齒排70的曲線而設。201017971 IX. Description of the Invention: [Technical Field] The present invention relates to a susceptor for adjusting a satellite antenna, and more particularly to a satellite antenna adjusting device capable of accurately fine-tuning horizontal and vertical orientations. [Prior Art] For the use of a satellite antenna (dish antenna), in order to achieve a better receiving angle, it is common practice to install a set of angle-adjustable adjustment seats between the disk body and the support column of the satellite antenna. The adjustment seat provides operational adjustment of the X-axis direction and the γ-axis direction, and is adjusted by the X-axis and the Y-axis to achieve an optimal reception angle, so that the electronic device can obtain a clear and impurity-free reception effect. The satellite antenna adjustment seat, the angle adjustment mechanism, generally uses the hole to the hole alignment, or the single hole to the long hole alignment mode, to achieve a fixed amplitude adjustment effect, but the hole to hole alignment In the way, due to the large band, it is impossible to obtain precise fine-tuning effect; the alignment method of single hole to long hole is adjusted by the experience alone, the operation is not easy, and after the amplitude is adjusted, the screw is locked, which is the final adjustment. Position, therefore, in the process of adjustment, there is no long hole in the band, and the immediate positioning cannot be obtained, so the amplitude modulation of the displacement is still easily affected during the process of locking the bolt. The effect of the loss of precise adjustment. As mentioned above, the existing adjustment structure with the hole alignment is not only 5 201017971, the operation is not easy, the components are complicated, and it is not accurate enough, and the use is still not good enough. At best, it can only be classified into the coarse adjustment mode. Therefore, it is necessary to Seek a solution. SUMMARY OF THE INVENTION The present invention provides a satellite antenna adjusting device. By combining the gears and the tooth rows, the satellite antenna can be accurately adjusted according to the antenna support bar as a reference, and the horizontal and vertical directions are accurately adjusted. It is quite simple to operate and has a simple structure. Therefore, the satellite antenna adjusting device of the present invention is connected between the satellite antenna and an antenna support rod, and includes a retainer base, a support base, a joint base, an X-axis fine adjustment mechanism and a γ-axis fine adjustment mechanism. The susceptor base is coupled to a face of the satellite antenna. The support is coupled to the antenna support bar. The joint is coupled between the base of the retainer and the support. The X-axis fine adjustment mechanism is coupled between the support base and the coupling seat, and the coupling base is interlocked by the coupling relationship between the gear and the tooth row, so that the satellite antenna generates the X-axis direction based on the antenna support rod. The slight movement. The Y-axis fine-tuning mechanism is coupled between the connecting seat and the susceptor base, and uses the coupling relationship between the gear and the tooth row to interlock the connecting seat and the susceptor base, so that the satellite antenna can be referenced by the antenna supporting rod , produces a slight movement in the Y-axis direction. According to the satellite antenna adjusting device of the present invention, the retainer base includes a chassis, a claw fixing frame and a binding frame, and the claw fixing frame is coupled to the disk surface of the satellite antenna, and the chassis is fixed from the claw The frame extends outwardly to 201017971 such that the periphery of the satellite antenna abuts the chassis, the adapter extending from the claw holder in a direction away from the disk surface of the satellite antenna. The support base comprises a retaining plate, a binding frame and a set of connecting tubes. The connecting socket is connected to the antenna supporting rod, and the retaining plate is disposed on the socket. The joint comprises a bottom wall and two side walls. The X-axis fine adjustment mechanism includes a first gear and a first tooth row that are meshed with each other, and the first gear is fixed to a retainer of the support seat, and the first tooth row is disposed on a bottom wall of the joint On the side wall. The γ-axis fine adjustment mechanism includes a second gear and a second tooth row that are coupled to each other, the second gear is fixed to the joint frame of the retainer base, and the second tooth row is disposed on the joint The side wall of the side wall. According to the satellite antenna adjusting device of the present invention, the first tooth row has a circular arc shape, and the retainer of the support base has a circular arc hole, and the shape of the long hole is according to the first tooth row. Set the curve. According to the satellite antenna adjusting device of the present invention, the second tooth row has a circular arc shape, and the engaging frame of the retainer base has an arc-shaped elongated hole, and the elongated hole has a shape according to the second tooth. Set the curve of the row. According to the satellite antenna adjusting device of the present invention, the susceptor base includes a base body and a plurality of ears, the ears are locked on the disk surface of the satellite antenna, and the support base includes a bottom wall. Two side walls, a clip recess and a fine adjustment hole, the clip recess is abutting on the antenna support rod. The connecting seat comprises a bottom wall, two side walls, an inner raft, an outer raft and an adjusting hole. The X-axis fine adjustment mechanism includes a first gear and a first tooth row which are coupled to each other, and the first tooth row is disposed on a hole of the fine adjustment hole of the joint, and the first gear is placed on the hole The fine adjustment hole is axially fixed to the outer liner of the support. The γ-axis fine adjustment mechanism includes a second gear and a second tooth row that are coupled to each other, and the second tooth row is disposed on a hole edge of the adjusting hole of the joint seat, and the second gear is placed on the adjustment The hole and the shaft are fixed on the inner liner of the joint. According to the satellite antenna adjusting device of the present invention, the first tooth row has a circular arc shape, and the side wall of the support has a circular arc hole. The outer lining of the connecting seat has a locking hole corresponding to the locking hole and is locked on the connecting seat. The shape of the elongated hole is set according to the curve of the first tooth row. According to the satellite antenna adjusting device of the present invention, the second tooth row has a circular arc shape, and the side wall of the connecting seat has an arc-shaped elongated hole, and the inner lining plate of the connecting seat has a locking hole, the length The strip hole corresponds to the lock hole and is locked to the retainer base, and the shape of the long hole and the lock hole is set according to the curve of the second tooth row. Therefore, the present invention can obtain a precise fine adjustment effect by adjusting the orientation of the X-axis (left and right side angles) and the Y-axis (elevation angle) by using the coupling relationship of the gears and the tooth rows. In addition, the adjustment device has a simple overall structure and is convenient and quick to operate. [Embodiment] The satellite antenna adjusting device of the present invention has the following functions: using a coupling relationship of a gear and a tooth row to obtain a precision fine adjustment effect 201017971, a first gear and a first tooth row, the first The tooth row is disposed on a hole edge of the fine adjustment hole of the joint seat, and the first gear is disposed on the fine adjustment hole and the shaft is fixed on the outer plate of the support seat. The Y-axis fine adjustment mechanism includes a second gear and a second tooth row that are coupled to each other, and the second tooth row is disposed on a hole edge of the adjustment hole of the joint seat, and the second gear is placed on the adjustment The hole and the shaft are fixed on the inner liner of the joint. According to the satellite antenna adjusting device of the present invention, the first tooth row has a circular arc shape, and the side wall of the support has a circular arc hole. The outer lining of the connecting seat has a locking hole corresponding to the locking hole and is locked on the connecting seat. The shape of the elongated hole is set according to the curve of the first tooth row. According to the satellite antenna adjusting device of the present invention, the second tooth row has a circular arc shape, and the side wall of the connecting seat has an arc-shaped elongated hole, and the inner lining plate of the connecting seat has a locking hole, the length The strip hole corresponds to the lock hole and is locked to the retainer base, and the shape of the long hole and the lock hole is set according to the curve of the second tooth row. Therefore, the present invention can obtain a precise fine adjustment effect by adjusting the orientation of the X-axis (left and right side angles) and the Y-axis (elevation angle) by using the coupling relationship of the gears and the tooth rows. In addition, the adjustment device has a simple overall structure and is convenient and quick to operate. [Embodiment] The satellite antenna adjusting device of the present invention has the following functions: the gearing is matched with the tooth row to obtain a precise fine adjustment effect 8 201017971, and the adjusting device has simple components and easy operation. Referring to Figures 1 and 2, a first embodiment of the satellite antenna adjustment apparatus of the present invention is coupled between a satellite antenna 100 and an antenna support rod 200. The adjusting device 300 includes a retainer base 10, a support base 20, a connecting base 30, a first gear 40, a first tooth row 50, a second gear 60, a second tooth row 70, and a plurality of Bolt 80 and a plurality of nuts 90. The retainer base 10 is coupled to a disk surface 110 of the satellite antenna 1A. The retainer base 10 includes a chassis 11, a claw holder 12 and an engaging frame 13. The claw holder 12 is locked to the disk surface 110 of the satellite antenna 100 by a bolt 80 and a nut 90. The chassis 11 extends outwardly from the claw holder 12 such that the periphery of the satellite antenna 100 abuts against the chassis 11. The joint frame 13 extends from the claw holder 12 in a direction away from the disk surface 110 of the satellite antenna 100. The joint frame 13 is a gantry frame, and is fastened to the rear side of the claw frame 12 by bolts 80 and a nut 90. The two side walls of the joint frame 13 are respectively provided with a circular arc hole 131 and a Keyhole 132. The support base 20 is coupled to the antenna support bar 200. The support base 20 includes a retainer 21 and a set of nozzles 22. The socket 22 is locked to the antenna support rod 200 by bolts 80 and nuts 90. The retainer 21 is horizontally disposed on the ferrule 22. The joint 30 is coupled between the retainer base 10 and the support base 20. The joint 30 includes a bottom wall 31 and two side walls 32. The side walls 32 are all a sector plate. 9 201017971 The first gear 40 and the first tooth row 50 constitute an X-axis fine adjustment mechanism and are coupled between the support base 20 and the coupling seat 30. The first gear 40 is fixed to the retainer 21 of the support base 20, and the first tooth row 50 is disposed on the side end surface of the bottom wall 31 of the joint base 30. Referring to FIG. 1 , FIG. 4 and FIG. 5 , the first tooth row 50 has a circular arc shape, and the retainer 21 of the support base 20 has a circular arc hole 211 , and the shape of the elongated hole 211 is According to the curve of the first tooth row 50, a set of bolts 80 and nuts 90 are disposed between the bottom wall 31 of the joint seat 30 and the retainer 21, and the bolts 80 are exactly at the length of the retainer 21 Inside the strip hole 211. Using the coupling relationship between the first gear 40 and the first tooth row 50, the tray base 10 is indirectly linked, so that the satellite antenna 100 generates a slight movement in the X-axis direction based on the antenna support rod 200, such as 4, as indicated by the arrow X, the satellite antenna 100 shown by the imaginary line can be pivoted to the left or pivoted to the right to achieve the fine adjustment effect in the X-axis direction. After being adjusted, the joints are bolted 80 and the nut 90. 30 is completed by locking the support base 20. The second gear 60 and the second tooth row 70 constitute a Y-axis fine adjustment mechanism and are coupled between the retainer base 10 and the coupling base 30. The second gear 60 is fixed to the joint frame 13 of the retainer base 10, and the second tooth row 70 is disposed on the end surface of the sector side wall of the joint base 30. Referring to FIG. 3, the second tooth row 70 has a circular arc shape, and the curve of the second tooth row 70 is formed according to the shape of the long hole 131 of the 201017971 plate 13 of the retainer base 10, and A set of bolts 80 and nuts 90 are disposed between the joint frame 13 and the side wall 32 of the joint seat 30, and the bolts 80 are positioned in the long holes 131 of the joint frame 13. The coupling relationship between the second gear 60 and the second tooth row 70 is used to interlock the connecting base 30 and the retainer base 10, so that the satellite antenna 100 can be used as the reference of the antenna support rod 200 to generate a slight movement in the Y-axis direction. As shown by the arrow Y in FIG. 3, the satellite antenna 100 shown by the imaginary line can be pivoted upward or downward, thereby achieving the fine adjustment effect in the Y-axis direction, and after being adjusted, the bolt 80 and the nut 90 will be used. The connection of the joint 30 and the retainer base 10 is completed. It can be seen that, in the satellite antenna adjusting device of the present invention, the gear and the tooth row are combined with the long hole to apply the synchronous displacement, so that the satellite antenna 100 not only has the left and right offset adjustment and the adjustment of the up and down elevation angle, but also is matched by the gear. The relationship makes the amplitude modulation more precise and precise, and achieves the fine-tuning use effect. In addition, the adjustment device 300 has a simple structure and easy operation, and is helpful for installation work. Referring to FIG. 6, a second embodiment of the satellite antenna adjusting device of the present invention is connected between a satellite antenna 100 and an antenna support rod 200. The adjusting device 400 includes a retainer base 500, a support base 600, and A joint 700, a first gear 40, a first tooth row 50, a second gear 60, a second tooth row 70, a plurality of bolts 80 and a plurality of nuts 90. Referring to Figures 7 and 8, the tray base 500 includes a base body 510 and a plurality of ears 520. These ears 520 are secured to the disk surface 110 of the satellite antenna 100 by a lock 11 201017971. The support base 600 includes a bottom wall 610, two side walls 620, a recessed portion 630, and a fine adjustment hole 640 disposed on one of the side walls 620. The clip recess 630 is attached to the antenna support rod 200 by a clip 650 and a bolt 80 and a nut 90. The joint 700 includes a bottom wall 710, two side walls 720, an inner liner 730, an outer liner 740, and an adjustment hole 750 disposed on one of the side walls 720. The first gear 40 and the first tooth row 50 form an X-axis fine adjustment mechanism, and the first tooth row 50 is disposed on a hole edge of the fine adjustment hole 640 of the support base 600. The first gear 40 is placed on the fine adjustment. The hole 640 is axially fixed to the outer liner 740 of the joint 700. The first tooth row 50 has a circular arc shape, and the side wall 620 of the support base 600 has a circular arc hole 621. The outer liner 740 of the joint base 700 has a locking hole 741, and the long hole 621 is Corresponding to the lock hole 741, the bolt 80 and the nut 90 are locked to the joint base 700. The shape of the long hole 621 is set according to the curve of the first tooth row 50. The second gear 60 and the second tooth row 70 form a Y-axis fine adjustment mechanism. The second tooth row 70 is disposed on the edge of the adjustment hole 750 of the joint 700. The second gear 60 is placed on the adjustment. The hole 750 is fixed to the inner liner 730 of the joint 700. The second tooth row 70 has a circular arc shape, and the side wall 720 of the joint 700 has a circular arc hole 721. The inner liner 730 of the joint 700 has a lock hole 731, and the long hole 721 is Corresponding to the lock hole 731, and using the 12 201017971 bolt 80 and the nut 90 to lock the joint 700 to the retainer base 500, and the shape of the elongated hole 721 and the lock hole 731 is based on the second tooth row. The curve of 70 is set.
如上所述，第二實施例的衛星天線調整裝置，其 X轴與Y軸方位的調整方式，同樣是利用齒輪與齒排 結合長條孔作同步調整，致使衛星天線1〇〇獲得水平 與垂直方位的微調作用，以期達到精準化的微調效果 ，惟此實施例不同的地方，只是將齒輪、齒排運用於 長條寬板形的調整裝置400，其它功用皆與上述實施 例相同，此不再贅述。 值得一提的是，前述兩實施例中，利用第一齒輪 、齒排組與第二齒輪、齒排組分別達到χ軸與γ轴 的微調目的，係為本發明最佳實施例，此外，由於該 連結座與支承座皆設有兩個側壁，因此，在前述兩^ 壁上設置兩組第一齒輪、齒排組與兩組第二齒輪、齒 排組，亦可達到預期的功效，此不再贅述。 如第5圖所示，另可在該承盤基座1〇上設置^ 複數個刻度線，此些刻度線係為χ軸方向之 戶 的參考標#。 很以上所述者，僅為本發明 木 -^ ^ ---双1主貫施例iii ，每不能以此限定本發明實施之範圍，即大凡依功 明申請專利範圍及發明說明内容所作之簡單的等免 化與修飾，皆仍屬本發明專利涵蓋之範圍内。 13 201017971 【圖式簡單說明】 第1圖係為本發明衛星天線調整裝置之第一實施例的立體 圖。 第2圖係為該第一實施例之衛星天線調整裝置的另一立體 圖。 第3圖係為一組合側視圖，是顯示調整裝置組裝於衛星天 線與天線支撐桿的使用狀態。 第4圖係為一組合後視圖’是顯示調整裝置組裝於衛星天 ❹ 線與天線支撐桿的使用狀態。 第5圖係為第4圖中的局部放大圖。 第6圖係為本發明衛星天線調整裝置之第二實施例的組合 側視圖。 第7圖係為第6圖中的一局部放大圖。 第8圖係為該第二實施例之衛星天線調整裝置的組合俯視 圖。As described above, in the satellite antenna adjusting device of the second embodiment, the adjustment of the X-axis and the Y-axis azimuth is also performed by using the gear and the tooth row in combination with the long hole for synchronous adjustment, so that the satellite antenna 1 is horizontally and vertically. The fine-tuning of the azimuth is in order to achieve a precise fine-tuning effect. However, in this embodiment, the gears and the teeth are only used for the strip-shaped adjustment device 400, and other functions are the same as those of the above embodiment. Let me repeat. It is to be noted that, in the foregoing two embodiments, the fine adjustment of the first axis, the tooth row group, the second gear, and the tooth row group respectively to achieve the χ axis and the γ axis is a preferred embodiment of the present invention. Since the connecting seat and the supporting base are provided with two side walls, two sets of first gears, a tooth row group and two sets of second gears and tooth row groups are disposed on the two walls, and the expected effect can also be achieved. This will not be repeated here. As shown in Fig. 5, a plurality of tick marks may be provided on the susceptor base 1 ,, and these tick marks are reference numerals # of the user in the χ axis direction. In view of the above, only the wood-^^--double 1 main embodiment iii of the present invention can not be used to limit the scope of the practice of the present invention, that is, the scope of the patent application and the description of the invention. Simple exemptions and modifications are still within the scope of the invention. 13 201017971 A brief description of the drawings Fig. 1 is a perspective view showing a first embodiment of the satellite antenna adjusting device of the present invention. Fig. 2 is another perspective view of the satellite antenna adjusting device of the first embodiment. Fig. 3 is a combined side view showing the state in which the adjustment device is assembled to the satellite antenna and the antenna support rod. Fig. 4 is a combined rear view' showing the state in which the display adjustment device is assembled to the satellite antenna line and the antenna support bar. Fig. 5 is a partial enlarged view of Fig. 4. Figure 6 is a combined side view of a second embodiment of the satellite antenna adjusting device of the present invention. Fig. 7 is a partially enlarged view of Fig. 6. Fig. 8 is a combined plan view of the satellite antenna adjusting device of the second embodiment.
14 20101797114 201017971
【主要元件符號說明】 100… ••衛星天線 90·.... …螺帽 110 ... ••盤面 400". …調整裝置 200 ... ••天線支撐桿 500·.· …承盤基座 300… ••調整裝置 510... …基座主體 10..... ••承盤基座 520··· …耳片 11 ."· …底架 600". …支承座 12 ••爪固架 610... …底壁 13 .… …接合架 620". …側壁 131 ·· …長條孔 621… …長條孔 132 ·· …鎖孔 630·.. …夾凹部 20.... …支承座 640". …微調孔 21 •… …承盤 650". …夾片 211 ·. …長條孔 700". …連結座 22···· …套接管 710·.. …底壁 30.... …連結座 720". …侧壁 31 .... …底壁 721… …長條孔 32···· …側壁 730·" …内襯板 40.... …第一齒輪 731… …鎖孔 50·". …第一齒排 740... …外襯板 60··.· …第二齒輪 741… …鎖孔 70.·.. …第二齒排 750... …調整孔 80··.. …螺栓 15[Description of main component symbols] 100... ••Satellite antenna 90·.... Nut 110 ... ••Disc 400"....Adjustment device 200 ...••Antenna support bar 500·.·... Base 300... ••Adjustment device 510...Base body 10...••Retainer base 520····ear piece 11 ."·...Base frame 600". Support base 12 ••Claw frame 610... bottom wall 13 .... ...joint frame 620"....side wall 131 ··long hole 621...long hole 132 ··...lock hole 630·.....clip recess 20 .... ... support 640 ". ... fine-tuning hole 21 • ... retaining plate 650 ". ... clip 211 ·. ... long hole 700 ". ... joint seat 22 ···· ... socket 710 ·.. ... bottom wall 30.......joint seat 720"....side wall 31 .......bottom wall 721...long hole 32····...side wall 730·"...liner 40... ...the first gear 731...the keyhole 50·"....the first tooth row 740...the outer lining plate 60··....the second gear 741...the keyhole 70.....the second Tooth row 750... adjustment hole 80··.. ... bolt 15