M353494 八、新型說明： 【新型所屬之技術領域】 本創作係關於-伽星天線，特糊於—種衛星天線及其角度調 .整機構。 【先前技術】 . 魁天、_侧顧是_魅天線減微_衛纽號，並將 #衛星訊狀紅碟型天線巾的低雜崎頻放大器（Lgw _歸 d_ LNB )。_崎触大器將此針的峨放大至數十 萬倍後再利用振盡電路將高頻衛星訊號轉換至中頻，此中頻訊號為一 個調變訊號，再經視訊轉換器（Set_T〇p—β〇χ，_解調復原音訊 號後’即可輸入電視使用。 由於術星天線需接收衛星發射之微波訊號，而碟型天線是一種高 指向性的衛星触天線，因其接㈣性缺麵天線正巾央對準於遠 籲距離之衛星⑺三萬六千公里），故碟型天線的指向方位需很高的精準 .度。緣是’為提高碟型天線能夠有效接收衛星微波訊號，具有可調整 .仰角及方位角之機構設計為不可或缺之條件。 因此’如何提供-種衛星天線及制度調整機構，藉賴易之機 •構設計既可财且快速聯達成衛星天線之仰肢方㈣的調整，實 為當前重要課題之一。 【新型内容】 5 M353494 有血於上述課題本創作之目的為提供一種衛星天線及其角度調 整機構，藉賴易之機構設計柯精確域速崎時達成衛星天線之 仰角及方位角的調整，以有效提高衛星天線之接收效能。 為達上述目的，依據本創作之—種角度調整機構，用於一衛星天 •，線，角度調整機構包含-基座、一承載單元以及一第一調整單元。承 載早讀基座樞接。第-調整單元具有—第—導桿元件及—第一調敕 疋件。第-導桿元件穿設第-驗元件喊接基纽承鮮元。盆中， ♦調整第-調整元件與第一導桿元件的相對位置，承載單元係相對於基 座以一第一方向轉動。 基座具有-第—座體及—第二座體，第—座體與承鮮元框接， —座體與第—賴連接。角度調整機構更包含—第二機單元，且 2一第二導桿元件及-第二娜元件。第二導桿元件穿設第二調整 =件而連接第-座體及第二座體。其中，調整第二調整元件與第 =件相對位置，第—座體相對於第二座體以—第二方向轉動 載單元係姆於第二座體沿第二方向轉動。 及一 ΓΓ創作之-種衛星天線，包含-碟型天線以 角又I機構。角度調整機構與碟型天線連接，並包含 3载=及單元。第—調整單元具有—第-導桿树及 單_ 雜讀穿設第―鮮元件岭座及承載 :相整第—調整元件與第—導桿元件的相對位置，承載單 兀係相對於基座以一第一方向轉動 承上所述’ _本_之-種魅天線及其角度 調整機構，藉由 6 M353494 第-調整單元連接承載單元及基座及第二調整單元連接基座之第一座 體及第二座體，以分別使承載單元可以第一方向轉動及第二方向轉 動。與習知技術她’本創作之衛星天線及其纽·機構藉由簡易 ‘之機構設計即可精確且快辆時達成衛星天線之仰狀方位角的二維 角度調整，以有效提高衛星天線之接收效能。 【實施方式】 以下將參照相咖式’說明依本創作較佳實施例之—種衛星天線 及其角度調整機構。 請參照圖1A及圖1B所示，本創作較佳實施例之-⑽度調整機 構K) ’制於-魅天線。減縦機構ω個關整—衛星天線 收發訊號所需之仰角及方位角。角度調整機構iq包含—基座n、一 承載料12以及-第-輕單元13。承鱗元12與基座n樞接。 其中基座11具有第-座體lu及—第二座體112。基座Η藉 一座體111與承載單元12樞接，而第：座體m與第-她U連接。 第一調整單元13用以調整衛星天線之仰角，並具有-第-導桿元 件131及—第—調整元件132。第—導桿元件ηι穿設第-調整元件 132而連接基座11之第一座體ηι及承载單元u。 基座u更具有-第一保持元件113與第一座體⑴連接。承載單 』具有-承載4 121及與承载元件a樞接之一第 第一調整私13則分繼—保持元件出及第二鱗元件122 連接。第—調整料13藉由第—保持元件U3及第二保持树122來 7 M353494 保持及支樓承栽元杜] 心件⑵相對於基座11之角度。 第一調整單元J3之第一導桿 藉由螺紋之導程精確調 了為一螺栓或—螺桿，以 -螺帽或-螺紋管。以轉動角又’而第—調整元件出可為 -導桿元件⑶係施辦，第―游單元13之第 明。角度調整機制及^ ―調整元件丨32為-楼帽為例說 稍後敍述。物—刪元13輕―卜柏乃之方法 角度調整機構10更包含 之一第二M H早7" 14 ’肋婦衛星天線 第二導桿元件141穿 $-1兀件M2。 座體112。 一件142而連接第-座體m及第二 二圖：所示’第一座體111或第二座_可具有複數個弧槽分 別設置於第-賴111之—接合㈣或第二助12之—接合面S2, 用以調整第二方向（圖未顯示）。第-座體in或第二座體m對庫該 等弧槽可設置複數個鎖合件，例如為—獅顧栓，肋連接第二座 體111與第二座體112。於本實關中，第二座體112侧如具有四個 弧槽al〜a4 ’且第一座體U1對應該等弧槽ai〜a4設置四個鎖合件 bl〜b4以使鎖合件bl〜b4與弧槽al〜a4可相互滑動或鎖合。另外， 第二調整藉⑷與第二座體⑴_體成型，第二調整元件⑷並穿 設第-座體m之-調整槽cl與第二導桿元件141螺接。其中，第二 導桿元件141儀為一螺检或一螺桿，而第二調整元件142係為一具有 8 M353494 螺紋之板件。 的相1 角度調整機構1G調整第—調整树132與第—導椁元件出 恤置’因第-導桿元件131與第二保持元件122連接，且第二 二轉122與承載元件121樞接，故第一導桿元件⑶τ連 中使承載單元12可相對於基座U以第—方向T1轉動。於本 調二一 ’ t吏衛星可達到理想之收訊角度，角度調整結構!〇可藉由 正調整tl件132與第-導桿元件131的相對位置，使承載單元 相對於基座Π以第-方向T1轉動，可決定承載元件⑵相對於基 座11之一仰角θ。 當角度調整機構10調整第二調整元件142與第二導桿元件⑷ 的相對位置’第-座體nl相對於第二座體112以一第二方向乃轉 動，於本實施例中，藉由第—座體U1以第二方向T2轉動，使承載元 件121相對於第二座體112可調整-方位角（圖未顯示）。 请參照圖2所示’一種衛星天線卜包含一碟型天線ρ以及一角 度調整機構1G。於本實施财，衛星天線丨係制上述肢調整機構 1〇與碟型天線P連接以形成衛星天線。肢赃機構1G包含一基座 U、一承載單元12、一第一調整單元13及一第二調整單元14。因角 度調整機構10之基座11、承載單元12、第一調整單元13及一第二調 整單TL 14，其結構與各元件之連接關係已於上述實施例詳述，於此不 再贅述。衛星天線1更包含—收發模組w及―支料元ls與角度調 整機構10連接。其中，收發模組w更包含一濾波器、一正交模態轉 換器（OMT)、一饋源器（feed h〇m)與一導波管(waveguide)，並藉 9 M353494 由連杯L夾持收發模級w，使連桿L與角度調整機構之承載元 件121鎖固。支樓單元15係與角度調整機構川之第二座體in螺鎖 以完成具有可調整仰角及方位角之衛星天線1。衛星天線1之角度調 整方法及触已於上述實施例詳述，於此不料述。 ”’丁、上所述’依據本創作之—種衛星天線及其肖度調整機構，藉由 第一調整單元連接承鮮元絲座及$二纟驗單元賴基座之第一座 體及第-座體’以分別使承載單元可以第—方向轉動及第二方向轉 動。與習知技術相較，本創作之衛星天線及其角度調整機構藉由簡易 之機構設計即可精確錄賴時達成魅天狀仰歧綠角的二維 角度調整，以有效提高衛星天線之接收效能。 以上所述僅為舉例性，而非為限制性者。任何未脫離本創作之精 神與料，而對其進行之等效修改或變更，均應包含於後附之 利範圍中。 寻 • 【圊式簡單說明】 • 圖1A為本創作之一種角度調整機構之示意圖； • 圖1B為本創作之一種角度調整機構之分解示意圖；以及 ® 2為本_之-種魅天線及其角度罐機構之示意圖。 【主要元件符號說明】 1 .衛星天線 10:角度調整機構 10 M353494 II :基座 III :第一座體 112 :第二座體 113:第一保持元件 • 12 :承載單元 ' 121 :承載元件 '122:第二保持元件 φ 13:第一調整單元 131 :第一導桿元件 132 :第一調整元件 14 :第二調整單元 141 :第二導桿元件 142 :第二調整元件 15 :支撐單元 φ al〜a4 :弧槽 bl〜b4:鎖合件 cl :調整槽 L :連桿 P:碟型天線 SI、S2 :接合面 T1 :第一方向 T2 :第二方向 M353494 w:收發模組M353494 VIII, new description: [New technology field] This creation is about - gamma antenna, special paste - a kind of satellite antenna and its angle adjustment. [Prior Art] . Quebec, _ side is _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _ _Saki Toucher magnifies the 峨 of the pin to hundreds of thousands of times and then uses the vibration circuit to convert the high frequency satellite signal to the intermediate frequency. The IF signal is a modulation signal and then the video converter (Set_T〇) After p-β〇χ, _ demodulation and recovery of the audio signal, it can be input to the TV. Since the satellite antenna needs to receive the microwave signal transmitted by the satellite, the dish antenna is a highly directional satellite antenna, because it is connected (4) The antenna of the sexually-deficient antenna is aligned with the satellite of the far-reaching distance (7) 36,000 kilometers), so the pointing orientation of the dish antenna needs to be highly accurate. The edge is designed to be an indispensable condition for improving the dish antenna to effectively receive satellite microwave signals, with adjustable, elevation and azimuth mechanisms. Therefore, 'how to provide a kind of satellite antenna and system adjustment mechanism, and relying on the machine of Yi Yi. The design can not only achieve the adjustment of the satellite antenna's limbs (4), which is one of the current important issues. [New content] 5 M353494 Blood on the above subject The purpose of this creation is to provide a satellite antenna and its angle adjustment mechanism. Effectively improve the receiving performance of satellite antennas. In order to achieve the above object, according to the creation of the angle adjustment mechanism for a satellite sky, the line, the angle adjustment mechanism comprises a base, a carrying unit and a first adjusting unit. The anchor reading base is pivoted. The first adjustment unit has a -th guide member and a first adjustment member. The first-guide member is passed through the first-inspection component. In the basin, ♦ adjusting the relative position of the first adjusting element and the first guiding rod element, the carrying unit is rotated in a first direction with respect to the base. The base has a - a seat body and a second seat body, and the first seat body is framed with the fresh element, and the seat body is connected with the first base. The angle adjustment mechanism further includes a second machine unit, and a second guide member and a second member. The second guide member passes through the second adjustment member to connect the first seat body and the second seat body. Wherein, the second adjusting element is adjusted to the relative position of the second member, and the first seat body rotates relative to the second seat body in the second direction to rotate the carrier unit in the second direction. And the creation of a satellite antenna, including a dish antenna with an angle and an I mechanism. The angle adjustment mechanism is connected to the dish antenna and includes 3 carriers = and units. The first-adjusting unit has a -th guide tree and a single_missing through-the-fresh element ridge and bearing: the relative position of the phase-adjusting element and the first-guide member, and the bearing unit is opposite to the base The seat rotates in a first direction to carry the '_本_'--the antenna antenna and its angle adjustment mechanism, and the 6 M353494 first-adjustment unit connects the carrying unit and the base and the second adjusting unit to the base a body and a second body to respectively rotate the carrying unit in a first direction and in a second direction. With the conventional technology, her satellite antenna and its mechanism can achieve two-dimensional angular adjustment of the satellite antenna's tilting azimuth accurately and quickly when the vehicle is designed to improve the satellite antenna. Receive performance. [Embodiment] Hereinafter, a satellite antenna and an angle adjusting mechanism thereof according to a preferred embodiment of the present invention will be described with reference to a coherent style. Referring to Fig. 1A and Fig. 1B, the - (10 degree adjustment mechanism K) of the preferred embodiment of the present invention is manufactured in a fascinating antenna.縦 縦 关 — — 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星 卫星The angle adjustment mechanism iq includes a base n, a carrier 12 and a -th-light unit 13. The scale element 12 is pivotally connected to the base n. The base 11 has a first seat body lu and a second seat body 112. The base 枢 is pivotally connected to the carrying unit 12 by the body 111, and the first body m is connected to the first-side U. The first adjusting unit 13 is configured to adjust the elevation angle of the satellite antenna, and has a -th guide member 131 and a first adjusting member 132. The first guide member ηι is passed through the first adjusting member 132 to connect the first body ηι of the base 11 and the carrying unit u. The base u further has a first holding element 113 connected to the first base body (1). The carrier unit has a carrier 4121 and is pivotally connected to the carrier member a. The first adjustment component 13 is connected to the second scale component 122. The first adjusting material 13 is held by the first holding member U3 and the second holding tree 122, and the angle of the core member (2) relative to the base 11 is maintained. The first guide rod of the first adjusting unit J3 is precisely adjusted by a lead of a thread to a bolt or a screw, a nut or a threaded tube. The rotation angle can be 'and the first adjustment element can be - the guide element (3) is applied, and the first - navigation unit 13 is specified. The angle adjustment mechanism and the adjustment element 丨32 are - the floor cap as an example, which will be described later. The method of deleting the element 13 is light--Bobner. The angle adjustment mechanism 10 further includes one of the second MH early 7"14' 14-ribbed satellite antenna. The second guide member 141 is worn by the $-1 element M2. Seat 112. One piece 142 is connected to the first seat body m and the second two figure: the first seat body 111 or the second seat _ can have a plurality of arc grooves respectively arranged on the first lag 111 - joint (four) or second aid 12 - the joint surface S2, used to adjust the second direction (not shown). The first seat body or the second seat body m may be provided with a plurality of lock members for the arc grooves, for example, a lion bolt, and the rib connects the second seat body 111 and the second seat body 112. In the present embodiment, the second body 112 side has four arc slots a1 to a4' and the first body U1 is provided with four locking members bl~b4 corresponding to the arc slots ai~a4 to make the locking member bl ~b4 and arc slots al~a4 can slide or lock each other. Further, the second adjustment is formed by the second body (1) and the second body (1), and the second adjusting member (4) is provided with the adjusting portion c1 of the first body m to be screwed to the second guiding member 141. The second guiding member 141 is a screw or a screw, and the second adjusting member 142 is a plate having 8 M353494 threads. The phase 1 adjustment mechanism 1G adjusts the first adjustment tree 132 and the first guide member to enter the shirt, because the first guide member 131 is connected to the second holding member 122, and the second two rotation 122 is pivotally connected to the carrier member 121. Therefore, the first guide member (3) τ is connected to enable the carrier unit 12 to rotate in the first direction T1 with respect to the base U. In the present invention, the satellite can achieve an ideal receiving angle, the angle adjusting structure can be adjusted by the relative position of the t-piece 132 and the first-guide member 131, so that the carrying unit is opposite to the base. Rotation of the first direction T1 determines the elevation angle θ of the carrier element (2) relative to the base 11. When the angle adjusting mechanism 10 adjusts the relative position of the second adjusting member 142 and the second guiding member (4), the first seat body n1 is rotated in a second direction relative to the second seat body 112, in this embodiment, by The first body U1 is rotated in the second direction T2 to adjust the azimuth angle of the carrier member 121 relative to the second body 112 (not shown). Referring to Fig. 2, a satellite dish includes a dish antenna ρ and an angle adjusting mechanism 1G. In the present implementation, the satellite antenna system is connected to the dish antenna P to form a satellite antenna. The limb mechanism 1G includes a base U, a carrying unit 12, a first adjusting unit 13, and a second adjusting unit 14. The connection between the structure of the pedestal 11 of the angle adjusting mechanism 10, the carrying unit 12, the first adjusting unit 13, and the second adjusting unit TL 14 is described in detail in the above embodiments, and will not be further described herein. The satellite antenna 1 further includes a transceiver module w and a support element ls connected to the angle adjustment mechanism 10. The transceiver module w further includes a filter, an orthogonal mode converter (OMT), a feed (feed h〇m) and a waveguide, and the 9 M353494 is connected by a cup L. The transceiving mold stage w is clamped to lock the connecting rod L and the bearing element 121 of the angle adjusting mechanism. The branch unit 15 is connected to the second body of the angle adjusting mechanism and is screwed to complete the satellite antenna 1 having an adjustable elevation angle and azimuth angle. The angle adjustment method and the touch of the satellite antenna 1 have been described in detail in the above embodiments, and are not described herein. "Ding, the above description" according to the creation of the satellite antenna and its slant adjustment mechanism, the first adjustment unit is connected to the first element of the base plate and the second base of the base The first seat body is configured to respectively rotate the carrying unit in the first direction and in the second direction. Compared with the prior art, the satellite antenna and the angle adjusting mechanism thereof can be accurately recorded by a simple mechanism design. The two-dimensional angle adjustment of the enchanting green angle is achieved to effectively improve the receiving performance of the satellite antenna. The above description is only exemplary, not limiting. Anything does not deviate from the spirit and spirit of the creation, but Equivalent modifications or changes made to it shall be included in the scope of the attached. 寻 • [Simple description] • Figure 1A is a schematic diagram of an angle adjustment mechanism of the creation; • Figure 1B is a kind of creation Schematic diagram of the angle adjustment mechanism; and ® 2 is a schematic diagram of the antenna antenna and its angle can. [Main component symbol description] 1. Satellite antenna 10: Angle adjustment mechanism 10 M353494 II: Base III: Body 112: second seat 113: first retaining element • 12: carrying unit '121: carrying element '122: second holding element φ 13: first adjusting unit 131: first guiding element 132: first adjustment Element 14: second adjustment unit 141: second guide element 142: second adjustment element 15: support unit φ al~a4: arc groove bl~b4: lock piece cl: adjustment groove L: link P: dish type Antennas SI, S2: joint surface T1: first direction T2: second direction M353494 w: transceiver module