M344178 八、新型說明： 【新型所屬之技術領域】 本創作是提供-種遙控飛機馬達固定座組體調整機 構’主要是對la設在遙控飛機其間的動力馬達固定座組體 可依改裝時的馬達大小作上、下方位或角度調整，來配合 螺旋槳轉動時可達到遙控飛機飛行時的平衡設置。 【先前技術】 r 按’目前組設在各式遙控飛機其間作為動力的馬達組 體/使用者通常是直接將馬達組裝在遙控飛機其機身前端 f後端預設方位’該馬達使用的電池則組設在相臨方位， 亥遙控I機其機身—端的馬達組體作帛端貞彳可加設以螺 旋槳，作為使用者在啟動遙控飛機其間組設的遙控器即可 使螺旋槳透過馬達組體的開啟進行高速旋轉，而使遙控飛 機作預設的飛行或旋轉。但對該馳飛機的玩家在須改變 飛機的最大飛行速度時，齡將组設在遙控飛機其間的馬 達予以改裝變更，使得該與原先不-大小的馬達在組裝入 遙控飛機其機相形成重㈣位，使用者間再調整遙控 ，機其機㈣前後平衡重心及馬達角度，以使遙控飛機: 飛行時保财平穩的“飛行’料該機身在進行前後平 ^重心及馬達角度的調整則相當不易’必須靠長期玩遙控 浙機的經驗來作重心的修正。 【新型内容】 ^本創作即是依目前組設在遙控飛機其間的馬達在作改 裝變更時存有的不易調整馬達角度的問題來作一改良，以 5 M344178 期組設在遙控錢其_動力馬軸定隸體可依改裝時 的馬達大小作上、下方位或角度調整，以配合螺旋紫轉動 時可達到遙控飛機飛行時的平衡設置。 —本創作之主要目的，是對遙控飛機其間組設的馬達固 定座組體是將結合以馬達的座體一端形成的凹槽可允許一 支持部件套合其間，在該支持部件其兩旁是配合以其間開 _具有數道間距孔的連結件及透過—螺固元件將兩連結件與 •支持部件預設相應的孔Μ貫穿定位成—體；對該組設^ 支持部件兩旁的連結件另端是可配合一抵靠板體其一侧架 設段的方位對應及透過一螺固元件將兩連結件該端與抵靠 板體其架設段相應的孔予以貫穿定位成-體；另在抵靠板 體其另端δ又置的螺紋孔則藉一螺桿段加以貫穿及使該螺桿 段另端定位在支持部件相應端的孔，依此來對一端結合有 螺旋槳的馬達固定座組體可依改裝時的馬達大小作上、下 方位或角度調整，來配合螺旋槳轉動時可達到遙控飛機飛 鲁行時的平衡設置。 、 本創作之第二目的，是對組設在遙控飛機其間的馬達 -口疋座組體该抵靠板體可依定位所須來加以架設在支 件其上方或下方。 ' 〜本創作之第三目的，是對組設在遙控飛機其間的馬達 固定座組體該結合有馬達的座體可依所須來加以袓 持部件的上方或下方。 、、ϋ在支 本創作之第四目的，是對組設在遙控飛機其間的馬達 固疋座組體該結合在支持部件與抵靠板體之間的兩連結 M344178 件’可依所須來加以架設在支持部件與抵靠板體之間的前 端或後端方位。 本創作之第五目的，是對組設在遙控飛機其間的馬達 固疋座組體該結合在支持部件與抵靠板體之間的兩連結 :’可依所須將其間開具的數道間距孔配合支持部件或抵 靠板體作一方位調整及透過螺固元件加以貫穿定位。 本創作之第六目#，是對組設在遙控飛機其間的馬達 固疋座組體該抵靠板體—側的架設段可依所須來配合支持 部件作朝上或朝下的方位設置。 【實施方式】 ^本創作設計之遙控飛機馬達固定座組體調整機構，參 第二、三圖，是對遙控飛機（1〇)其機身（1〇1)預設段落之間 組設以馬達固定座組體（9)。其中； 馬達固定座組體⑻（參第一、二圖），在其結合 達⑴的座體⑵-端是形成有凹槽（21)以允許—支持部件、 • (3)套合其間，在該支持部件⑶其兩旁是配合以其間開且 有數這間距孔（41)的連結件⑷及透過一螺固元件⑻將兩 連結件⑷與支持部件⑶預設相應的孔⑷、31)予 定位成-體；對該組設在支持部件⑻兩旁的連結件⑷： 端是可配合-抵靠板體（5)其一側架設段⑸）的方位對 及透過-螺固元件⑻將兩連結件⑷該端與抵靠板體^ 其架设段（51)相應的孔⑷、52)予以貫穿定位成—體 在抵靠板體⑸其另端設置的螺紋孔⑽則藉一螺桿段 加以貫穿及使該螺桿段⑺另端定位在支持部件⑶相應端） M344178 的孔（31);同時對突伸出座體（2)其間貫孔（22)的馬達軸心 (11)是可結合一螺旋槳（8)，依此來組成一馬達固定座組體 (9)(如第二圖）。 對該馬達固定座組體（9)在與遙控飛機（1〇)作組裝實 施（參第三、四圖），是將一端結合以螺旋槳（8)的馬達固 定座組體（9)朝遙控飛機（1〇)其機身（101)靠後段落的集風 槽（102)内部予以套合入及加以定位，並使該馬達固定座組 鲁體（9)其間組設的螺旋槳（8)朝後方位架設（如第四圖）: 依此作為啟動遙控飛機（10)其間組設的遙控器即可使螺旋 槳（8)透過馬達固定座組體（9)的開啟進行高速旋轉，而使 遙控飛機（10)作預設的飛行或旋轉。 同時當該遙控飛機在作改裝以改變飛機的飛行速度 時，則會將組設在遙控飛機其間的馬達（1)予以改裝變更， 對使用者為配合改裝該馬達（丨）其大小可與一端的螺旋槳 (8)在轉動時保持有遙控飛機（1〇)飛行時的平衡，則可將馬 ⑩達固定座組體（91)其間該抵靠板體（5) 一側的架設段（51) 依、、且π又重〜所須來配合支持部件（3 )作朝上方位的設置（如 ‘第七圖），或將結合在支持部件⑶與抵靠板體⑸之間的 兩連結件（4)，依組設重心所須將其間開具的數道間距孔 (、4^ =合抵罪板體（5)作一方位調整及透過螺固元件（6)加 二貝牙疋位（如第八圖的調整至中間段落的孔及抵靠板體 ’、一側的架設段作朝下方位設置）；抑將馬達固定座組體 ί93)其間該抵靠板體⑸—侧的架設段⑼依組設重心所 縣配合支持部件⑶作朝上方位的設置（如第九圖）。 8 M344178 另一馬達固定座組體（94)的調整形態是將結合以馬達 (1)的座體（2)依組設重心所須加以組設在支持部件（3)的 下方，及抵靠板體（5)架設在支持部件（3)其上方（如第十 圖）；或將架設在支持部件⑶上方的抵靠板體⑸其一側 的架設段（51)作朝下方位設置（如第十一圖）；抑將支持 部件（3)與架設其上方的抵靠板體⑸之間兩連結件⑷，依 組設所須架設在支持部件⑶與抵靠板體⑸之間的後端方 位，同時對結合在支持部件⑶與抵靠板體（5)其間的兩連 結件（4)則可依組裝重心所須，將其間開具的數道間距孔 支持部件⑶作-方位調整及透過螺固元件⑻加 乂貝牙疋位（如第十二圖）；亦可將架設在支持部件（3)上 ^的抵靠板體（5)其-側的架設段⑸）作朝下方位設置（如 弟十三圖）；依此來對改裝的馬達⑴其大小可依據一端結 =的螺旋紫（8)作上、下方位或角度調整（如第五圖的將抵 罪板體（5)其間貫穿的螺桿段⑺另端結合的支持部件⑻ 予以上、下方位調整出所須的角度），以配合螺旋槳（8)在 轉動時可達到遙控飛機(1〇)飛行時的平衡設置。 、同％對本創作設計的馬達固定座組體（9)亦可配合遙 二氣機？ 〇)組设在其機身（1 〇 1〕的前端容納空間及加以定 7 (如第六圖）’作為遙控飛機（10)其改裝的馬達（1)大小 I依據結合的螺旋槳（8)作上、下方位或角度調整，以達到 k控飛機（10)飛行時的平衡設置。 Λ _*、、、里以上組設在遙控飛機其間的馬達固定座組體在配合 端的螺旋槳作為組設平衡的調整實施是具有如下優點·· M344178 ι·對整體的馬達固定座組體可依改裝時的馬達其大小 作上、下方位或角度調整，來配合螺旋槳轉動時可 達到遙控飛機飛行時的平衡設置。 2 ·該組設在遙控飛機其間的馬達固定座組體其構件可 依組設重心所須作適切的方位及角度調整。 3·遠馬達固定座組體可依遙控飛機組設所須加以结人 在機身其後侧或前側方位，以達到預期的飛行平衡 調整及組設。 M344178 【圖式簡單說明】 =一，_•本創作馬達固定座組體的構件分解圖 第:圖··本創作馬達固定座組體的外觀立體圖 一。·本創作馬達固定座組體與遙控飛機在未組設 的示意圖 第四圖：太名| | 、 乍馬達固定座組體組設入遙控飛機後端 第。方位的側視剖面圖 曰，創作馬達g|定座組體在配合遙控飛機其尾 第丄回·部作角度調整的實施示意圖 '本創作馬達固定座組體組設入遙控飛機前端 — 方位的立體圖 弟七圖：本創作馬達固定座組體的其二組設形態示意 圖 第八圖：本創# I、去π 馬達固定座組體的其三組設形態示意 圖 第九圖：本創作€、去门 Η乍馬達固定座組體的其四組設形態示意 圖 一㈤t創作馬達固定座組體的其五組設形態示意 圖 ★圖士創作馬達固定座組體的其六組設形態示 意圖 第十二圖：夫& ’馬達固定座組體的其七組設形態示 意圖 '本訇作馬達固定座組體的其八組設形態示 M344178 意圖 【主要元件符號說明】 〔本創作〕 (10)遙控飛機 (101)機身 (102)集風槽 (1)馬達 (11)軸心 (2)座體 (21)凹槽 (22)貫孔 (3)支持部件 (31 、 41 、 52)孔 (4)連結件 (5)抵靠板體 (51)架設段 (53)螺紋孔 (6)螺固元件 (8)螺旋槳 (7)螺桿段 (9、91、92、93、94、95、96、97)馬達固定座組體 12M344178 VIII, new description: [New technical field] This creation is to provide a kind of remote control aircraft motor mount assembly adjustment mechanism 'mainly for the power motor mount base set between the remote control aircraft can be modified The motor is sized up and down or angled to match the balance of the RC airplane when the propeller is rotated. [Prior Art] r Press the current motor group/user that is set as the power between various remote control aircrafts. Usually, the motor is directly assembled in the front end of the front end of the fuselage of the remote control aircraft. The group is set in the adjacent orientation, and the motor of the fuselage-end of the Hai remote control machine can be added with a propeller. As a remote controller set up by the user during the start of the remote control aircraft, the propeller can be transmitted through the motor. The opening of the group performs high-speed rotation, and the remote control aircraft makes a preset flight or rotation. However, when the player of the aircraft needs to change the maximum flight speed of the aircraft, the motor that is set in the middle of the remote control aircraft is modified and modified, so that the original non-size motor is formed into a heavy-duty aircraft. (4) Position, adjust the remote control between the users, and adjust the center of gravity and the motor angle before and after the machine (4) to make the remote control aircraft: “Fly” when flying, the fuselage is adjusted before and after the center of gravity and the angle of the motor It is quite difficult to 'have to rely on the experience of long-term remote control of Zhejiang machine to make corrections. 【New content】 ^This creation is based on the fact that the motor currently set in the remote control aircraft is not easy to adjust the motor angle when making modifications. The problem is to make an improvement. The 5 M344178 group is set in the remote control. The Qiang _ power horse shaft can be adjusted according to the size of the motor when the modification is made, and the angle can be adjusted to match the spiral purple rotation. Balance setting during flight. — The main purpose of this creation is that the motor mount assembly that is assembled between the remote control aircraft is formed by the end of the base that is combined with the motor. The recess allows a support member to be nested therebetween, and the support member is provided with a joint between the two sides of the support member and the through-and-screw member. Μ Μ 定位 定位 ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; ; The corresponding hole of the erection section of the plate body is penetrated and positioned into a body; and the threaded hole which is placed at the other end of the plate body δ is penetrated by a screw section and the other end of the screw section is positioned at the support part. The hole of the end, according to this, the motor fixing seat body which is combined with the propeller at one end can be adjusted according to the size of the motor when the modification is made, and the angle of the motor can be adjusted to achieve the balance setting when the propeller rotates. The second purpose of the present invention is to mount the motor-mouth shackle group disposed between the remote control aircraft. The abutting plate body can be erected above or below the support member according to the positioning. third The purpose is to set the motor mount base set between the remote control aircraft and the motor-incorporated base body to hold the upper or lower part of the component according to the necessity. The two-part M344178 piece that is coupled between the support member and the abutting plate body is disposed between the supporting member and the abutting plate body, and is disposed between the supporting member and the abutting plate body. The front end or the rear end orientation. The fifth purpose of the creation is to connect the two components between the support member and the abutting plate body for the motor-fixing base set between the remote control aircraft: ' The plurality of pitch holes are provided in the middle to cooperate with the supporting member or to abut the plate body for positioning and through the screwing member. The sixth item of the present invention is a motor solid block group set in the remote control aircraft. The erection section of the body against the plate body side may be arranged in an upward or downward direction in accordance with the support member. [Embodiment] ^The remote control aircraft motor mount assembly adjustment mechanism of this design is referred to as the second and third figures, and the motor is set up between the preset passages of the fuselage (1〇1) of the remote control aircraft (1〇). Fixing block body (9). Wherein; the motor mount body (8) (refer to the first and second figures) is formed with a groove (21) at the end (2) end of the joint (1) to allow the support member, and (3) to be nested therebetween, The supporting member (3) is bounded on both sides by a connecting member (4) with a plurality of spaced holes (41) therebetween and a corresponding fixing hole (4), 31 for supporting the connecting member (3) through a screwing member (8). Positioning the body (the body); the connecting member (4) provided on both sides of the supporting member (8): the end is abutting against the plate body (5) on one side of the mounting section (5)) and the through-screwing element (8) The end of the connecting member (4) and the hole (4), 52) corresponding to the erecting portion (51) of the connecting plate body are disposed through the screw hole (10) disposed at the other end of the plate body (5) by a screw segment. Throughout and positioning the other end of the screw segment (7) at the corresponding end of the support member (3), the hole (31) of the M344178; at the same time, the motor shaft (11) of the intervening hole (22) protruding from the base (2) can be combined A propeller (8), thereby forming a motor mount base (9) (as shown in the second figure). The motor mount base (9) is assembled with the remote control aircraft (1〇) (refer to the third and fourth figures), and the motor mount base (9) with one end combined with the propeller (8) is directed to the remote control. The aircraft (1) is fitted and positioned inside the wind collecting groove (102) of the rear fuselage (101), and the propeller (8) is arranged in the motor fixing seat group (9). Erecting in the rearward direction (as shown in the fourth figure): As a remote controller set up between the remote control aircraft (10), the propeller (8) can be rotated at high speed through the opening of the motor mount base (9). The remote control aircraft (10) makes a preset flight or rotation. At the same time, when the remote control aircraft is being modified to change the flight speed of the aircraft, the motor (1) set in the remote control aircraft will be modified and modified, and the size of the motor (丨) can be modified with the user. The propeller (8) maintains the balance of the remote control aircraft (1〇) during flight, and the horse 10 can reach the mounting section of the fixed seat body (91) on the side of the plate body (5) (51) ) depends on , and π is heavy ~ must be matched with the support member (3) for upward orientation (such as 'seventh diagram), or two links between the support member (3) and the abutment plate (5) Piece (4), according to the set center of gravity, the number of pitch holes (4^ = the sin board (5) to be adjusted in one direction and the snail element (6) plus the second shell position ( As shown in the eighth figure, the hole is adjusted to the middle section and the erection section of the one side, and the erection section of one side is disposed downwardly; the motor mount base ί93) is abutted against the plate body (5) - the side erection section (9) Set the upward support position (such as the ninth figure) according to the support unit (3) of the center of gravity. 8 M344178 The other motor mount base (94) is adjusted in such a way that the base body (2) combined with the motor (1) is assembled under the support member (3) according to the center of gravity of the assembly, and abuts The plate body (5) is erected above the supporting member (3) (as shown in the tenth figure); or the erecting section (51) of one side of the supporting plate member (5) which is erected above the supporting member (3) is disposed downward ( As shown in the eleventh figure; the two connecting members (4) between the supporting member (3) and the abutting plate body (5) above it are arranged to be erected between the supporting member (3) and the abutting plate body (5). The rear end orientation, at the same time, the two connecting members (4) combined between the supporting member (3) and the abutting plate body (5) can be adjusted according to the assembly center of gravity, and the plurality of pitch hole supporting members (3) which are opened therebetween are adjusted for azimuth And twisting the beak position through the screwing element (8) (as shown in the twelfth figure); or erecting the support member (3) against the plate body (5) on its side (the erection section (5)) The lower position setting (such as the 13th figure); accordingly, the modified motor (1) can be made up and down according to the spiral purple (8) of one end = Or angle adjustment (such as the support member (8) at the other end of the screw segment (7) that penetrates the plate body (5) in the fifth figure to adjust the upper and lower directions to adjust the required angle) to match the propeller (8) when rotating It can reach the balance setting when the remote control aircraft (1〇) is flying. The same motor design of the motor mount base (9) can also be combined with the remote two air machine? 〇) Set the front end accommodation space of its fuselage (1 〇 1) and set it 7 (as shown in the sixth figure) as the remote control aircraft (10) its modified motor (1) size I according to the combined propeller (8) Adjust the upper and lower azimuth or angle to achieve the balance setting of the k-controlled aircraft (10) during flight. Λ _*, ,, and above, the propellers of the motor mount base set at the mating end are set up The balance adjustment implementation has the following advantages: · M344178 ι· The overall motor mount base can be adjusted according to the size of the motor when it is modified, to match the rotation of the propeller to achieve the flight of the remote control aircraft. Balance setting 2 · The motor fixing seat set of the group is set in the remote control aircraft. The components can be adjusted according to the set center of gravity. 3. The far motor fixed seat can be set according to the remote control aircraft. It must be knotted on the rear side or front side of the fuselage to achieve the desired flight balance adjustment and assembly. M344178 [Simple diagram of the diagram] = one, _ • The exploded view of the assembly of the motor mount base: Figure ·The stereoscopic view of the appearance of the motor mount base of the present invention. · The schematic diagram of the motor mount base and the remote control aircraft in the unassembled figure. The fourth picture: Tai Ming | | , 乍 Motor mount set is set into the remote control plane The side view of the rear end. The side view of the azimuth, the creation of the motor g|station group in the coordination with the remote control aircraft, the end of the head and the angle adjustment of the implementation of the schematic diagram of the creation of the motor mount block group into the remote control aircraft The front end - the azimuth of the stereoscopic figure seven: the second set of the shape of the motor mount base of the creation of the eighth figure: Ben Chuang # I, go to the π motor mount block body of the three sets of configuration diagram ninth: The creation of the four sets of the gantry motor mounts is shown in the form of a set of five (5) t-created motor mounts. The five sets of forms of the motor mounts Schematic diagram of the twelfth figure: Fu & 'The schematic diagram of the seven sets of the motor mount base'. The eight sets of the shape of the motor mount base are shown as M344178. [Main component symbol description] Creation] (10) Remote control aircraft (101) fuselage (102) wind collecting trough (1) motor (11) shaft center (2) seat body (21) groove (22) through hole (3) support member (31, 41, 52) Hole (4) Connecting piece (5) Abutting plate body (51) Erection section (53) Threaded hole (6) Screwing element (8) Propeller (7) Screw section (9, 91, 92, 93 , 94, 95, 96, 97) motor mount base 12