九、發明說明： 【發明所屬之技術領域】 、服2明=氣動卫具有關，詳而言之係指—種氣動工且之 氣缸，其具有大出力與低耗氣量之效果。 八之 【先前技術】 轉而產生觀體秘力源，藉由㈣氣紅之運 =驅域㈣之場猶，隨_紅缸 粉力，惟，氣流於習知渦輪氣缸中流動時，並 氣缸之耗“，二其輸出動力仍屬有限。此外，f知渴輪 矶缸之耗軋1大，較浪費能源。 方再者’渦輪氣缸之渦輪於高速轉動時，由於 生=螺儀效應’故氣缸之轉軸將固糾指 =此個=握住氣動工具時，會感到氣動 作扭動的現象’需要施力將之穩定，故容易使操 【發明内容】 具有的在於提供-種氣動工具之渦輪氣缸，可 具有目的纽麟—魏私狀雕氣缸，其 #友ff 2又—目_於提供'種氣動工具之渦輪氣缸’可 1乳缸之轉動構件於高速運轉時保持平衡，不會產生陀螺儀效 【實施方式】 為使貴審查委員能進-步瞭解本發明之目的、特徵以及 1327949 如第四圖；而筒部(38)與缸室(25)間之間隙係形成一環形空間 ^〇) ’該空間(40)係與流道(30)連通。三個凹入(42)，沿徑向自 筒部(38)周面往内凹設；三導孔(44)，設於筒部(38)前端面，並 往，分別與該三凹入(42)相通。該三導孔(44)前端分別正對於 ，氣孔(32)，如第四圖。因此，當高壓氣體流入缸蓋(24)之進 氣孔(32)後，即流經導流件(35)之導孔(44)而充盈於該 (4〇) ’復自流道(30)流入缸室(25)。將氣體自進氣孔導入缸室之 方式不以本實施例所示者為限。Nine, invention description: [Technical field to which the invention belongs], service 2 Ming = Pneumatic Guard has a shut-off, in other words, refers to a pneumatically-operated cylinder, which has the effect of large output and low air consumption. Eight [previous technology] turned to the source of the secret of the body, by (4) qihongyun = drive domain (four) of the field, with the _ red cylinder powder, but the air flow in the conventional turbine cylinder, and The consumption of the cylinder ", the output power of the two is still limited. In addition, the consumption of the thirst wheel of the rock tank is larger than the waste of energy. The turbine of the turbo cylinder is rotated at high speed due to the raw screw effect. 'Therefore, the rotation axis of the cylinder will be solid-corrected = this one=When the pneumatic tool is held, the phenomenon that the pneumatic action will be twisted' needs to be stabilized by force, so it is easy to make the operation. The turbine cylinder of the tool can have the purpose of the Newlin-Wei private engraving cylinder, and the #友ff 2 again--the _the turbo cylinder that provides the 'pneumatic tool' can be balanced at high speed during the high-speed operation. Gyro effect will not be produced. [Embodiment] In order to enable the review committee to further understand the purpose and features of the present invention and 1327949 as shown in the fourth figure; the gap between the barrel portion (38) and the cylinder chamber (25) is formed. An annular space ^ 〇) 'The space (40) is in communication with the flow channel (30). a recess (42) recessed inwardly from the circumferential surface of the tubular portion (38); a third guide hole (44) disposed on the front end surface of the tubular portion (38) and respectively facing the three recesses ( 42) The front end of the three-way hole (44) is opposite to the air hole (32), as shown in the fourth figure. Therefore, when the high-pressure gas flows into the air inlet hole (32) of the cylinder head (24), it flows through the guide. The guide hole (44) of the flow piece (35) is filled in the (4〇) 're-automatic flow path (30) and flows into the cylinder chamber (25). The manner of introducing gas from the air inlet hole into the cylinder chamber is not in this embodiment. The display is limited.
一轉軸(50) ’係藉由二軸承(52)裝設於缸體(2〇)中;後轴承 係固疋於缸身(22)後端，而前轴承則固定於缸蓋(24)。 一前渦輪(60)及一後渦輪(80)，於周面等間隔設有多數呈 U形或新月形之葉片(biade)(62)(82)。。 一逆向輪(70)，其周面亦等間隔設有葉片（72)，其葉片（72) 之葉形恰與滿輪之葉片（62)(82)之形狀相反。該逆向輪(7〇)之質 量等於該二渦輪(60)(80)之質量和為佳。A rotating shaft (50) is mounted in the cylinder (2〇) by two bearings (52); the rear bearing is fixed to the rear end of the cylinder (22), and the front bearing is fixed to the cylinder head (24) . A front turbine (60) and a rear turbine (80) are provided with a plurality of U-shaped or crescent-shaped blades (62) (82) at equal intervals on the circumference. . A counter wheel (70) is provided with blades (72) at equal intervals on its circumferential surface, the blades of which have a blade shape that is exactly opposite to the shape of the blades (62) (82) of the full wheel. The quality of the counter wheel (7 〇) is equal to the mass sum of the two turbines (60) (80).
該三渦輪(60)(70)(80)係裝設於該轉轴(5〇)上，而位於缸室 (25)内’逆向輪(70)係位於該二渦輪(60)(78)之間。渦輪(6〇)(8〇) 係與轉軸(50)固接而同步轉動；該逆向輪(70)之輪孔中係裝設 一單向軸承(75) ’如第四圖所示，而樞接於轉軸(5〇)，藉由該 單向軸承(75)，逆向輪(70)於轉軸上只能單向轉動，且其轉動 方向係與渦輪之方向恰為相反，將於下文說明。 前渦輪(60)之裝設位置係位於流道(3〇)末端，且位於吸氣 口(26)及排氣口(27)(28)之處，如第五圖。 此外，請參閱第四圖’葉片（62)(72)(82)之高度係由前往後 遞增’亦即’前渦輪之葉片之高度最淺，而後渦輪之葉片之高 度最深。本實施例之逆向輪之葉片（72)高度係呈傾斜狀，由前 往後漸增。同樣的，葉片（62)及(82)之高度亦可呈傾斜狀，使 7 1327949 該等葉片呈連續的斜向狀。 一本發明之氣缸係裝設於一氣動工具之殼體内，並 將回壓氣體導引至氣缸之進氣孔㈣，復流入缸室⑽，以驅 動氣紅運轉。The three turbines (60) (70) (80) are mounted on the rotating shaft (5 〇), and the reverse gear (70) is located in the cylinder chamber (25) at the two turbines (60) (78) between. The turbine (6〇) (8〇) is rotated synchronously with the rotating shaft (50); a one-way bearing (75) is mounted in the wheel hole of the reverse wheel (70) as shown in the fourth figure, and The pivot shaft (5〇) is pivoted by the one-way bearing (75), and the reverse wheel (70) can only rotate in one direction on the rotating shaft, and the direction of rotation is opposite to the direction of the turbine, which will be described below. . The front turbine (60) is located at the end of the flow path (3〇) and is located at the suction port (26) and the exhaust port (27) (28), as shown in the fifth figure. In addition, please refer to the fourth figure 'the height of the blade (62) (72) (82) is the lightest from the rearward increment 'that is, the blade of the front turbine is the shallowest, and the blade of the rear turbine is the deepest. The blade (72) of the reverse wheel of this embodiment has a height which is inclined and gradually increases from front to back. Similarly, the height of the blades (62) and (82) may also be inclined so that the blades are continuously inclined in the shape of 7 1327949. A cylinder of the invention is mounted in a housing of a pneumatic tool and directs back pressure gas to the intake port (4) of the cylinder and into the cylinder chamber (10) to drive the gas red operation.
5月參閲第四圖，高壓氣體流入缸室(25)時，係衝擊於前渦 輪(6〇)之葉片（62)，由於葉片之葉形之緣故，前渦輪將產生第 八圖所不之F方向之轉動，接著氣流復流向逆向輪(7〇)，並衝 擊於逆向輪之葉片（72)，使得逆向輪產生s方向；氣流接著流 向後渦輪(80)並衝擊其葉片（82)，後渦輪同樣以F方向轉動。 因此’該一渴輪(6〇)(8〇)及轉軸(5〇)係同向轉動；而逆向輪(7〇) 則反向轉動；前述之單向轴承(75)係確保逆向輪只能以s方向 轉動，使逆向輪與渴輪始终為不同的轉向。氣流於該三者 (60)(70)(80)間係連續的流動，最後，氣體復自排氣孔(34)排出 氣紅。In May, referring to the fourth figure, when the high-pressure gas flows into the cylinder chamber (25), it hits the blade (62) of the front turbine (6〇). Due to the blade shape of the blade, the front turbine will produce the eighth figure. The rotation in the F direction, followed by the reflow of the airflow to the reverse wheel (7〇), and impact on the blade (72) of the reverse wheel, so that the reverse wheel produces the s direction; the air flow then flows to the rear turbine (80) and impacts its blade (82) The rear turbine also rotates in the F direction. Therefore, the 'thirsty wheel (6〇) (8〇) and the rotating shaft (5〇) rotate in the same direction; the reverse wheel (7〇) rotates in the opposite direction; the aforementioned one-way bearing (75) ensures the reverse wheel only It can rotate in the s direction, so that the reverse wheel and the thirsty wheel always have different steering. The gas flow continuously flows between the three (60) (70) (80), and finally, the gas recirculates from the vent (34) to exhaust the gas red.
向壓氣體衝擊則滿輪(60)之葉片（62)促使前渦輪轉動後， 復經由葉片（62)之導引，流向逆向輪(7〇)而衝擊其葉片(72)，並 使逆向輪反向轉動。因葉片（62)與葉片（72)之葉形為反向，氣 流係形成一反向壓力衝擊於葉片（72)。同時，葉片（72)之容積 較渦輪(60)之葉片（62)之容積大，故氣流之壓力能有效的膨脹 推動逆向輪(70)，使其快速轉動。 接著，氣流復自逆向輪(70)流向後渦輪(80)，同樣的，該 二者(70)(80)亦為反向之轉動、葉片(72)與(82)之葉形相反，^ 及葉片（82)之容積大於葉片（72)之容積，故氣流以一反壓衝擊 後渦輪之葉片（82)，且氣體得以膨脹而推動葉片（82)，使得後 渦輪(80)具有相當的轉動動能。後渦輪之動能將回饋於同步轉 動之前渦輪(60)，增進氣缸整體之輸出動力。 復請參閱第五圖，缸體(20)於前渦輪(60)之位置，以流道 8 1327949 (30)為起點，沿著前難轉動方向依序具有_辅祕氣口⑽ 及二辅助排氣口(27)(28)，流道(3〇)係位於吸氣口(26)及第二排 氣口(28)間。於前渦輪(6〇)轉動之初，由於氣體未完全膨脹， f因轉速快，於吸氣口(26)之處將有外界的氣體被吸入缸室。 當轉動至排氣口(27)(28)時，因氣體已有所膨脹，而有些許氣 體自排氣口排出缸體。在前渦輪(60)之運轉行程中，於初始位 置(A)及終了位置(B)間係具有壓力差，此—壓力差係使前滿輪 易於產生轉動扭力。 缸體設置該等開口(26)(27)(28)時，氣缸即非密閉之空間， 可促^氣體流動之順暢性，因而降低渦輪於缸體内轉動時之阻 力，尚壓氣體之能量即不會損耗於對抗阻力，更有效率地驅動 氣缸。 又，外界氣體自吸氣口(26)補充入氣缸(1〇)時，係被氣把 所利用，故可減低氣缸對於高壓氣體之需求量，從而降低高壓 氣體之耗氣量。 一於軋缸作動時’該二渦輪_(8〇)及逆向輪(7〇)係相反方向 的兩速轉動，則渴輪轉動時施於轉軸之陀螺儀效應與逆向輪施 予轉軸之陀螺儀效應恰為反向硫消，達到平衡，該氣紅即不 會產生扭轉現象，保持穩定，可避免操作人員之疲累。 除了缸體之外，本發明之氣缸並無定子，而均為轉子(即 渦，與逆向輪），有別於習知氣缸。該反向轉動之逆向輪可增 進氣流之動能，提高氣缸之動力，且可防止氣動工具產生扭轉 現象。而喊π赫氣π使氣缸有效的發㈣動扭力，並 高壓氣體之耗氣量。 可理解的是，本發明不以裝設二個渦輪及一個逆向輪為 限，例如，可裝設三個渦輪及二個位於其間之逆向輪。 综上所述，本發明係為同類物品之首創，並具進步性功 9After the impingement of the gas, the blade (62) of the full wheel (60) causes the front turbine to rotate, and then passes through the guide of the blade (62), flows to the reverse wheel (7〇) and impacts the blade (72), and makes the reverse wheel Reverse rotation. Due to the opposite of the blade shape of the blade (62) and the blade (72), the airflow creates a reverse pressure impact on the blade (72). At the same time, the volume of the vane (72) is larger than the volume of the vane (62) of the turbine (60), so that the pressure of the airflow can effectively expand to push the reverse wheel (70) to rotate rapidly. Then, the airflow reverts from the reverse wheel (70) to the rear turbine (80). Similarly, the two (70) (80) are also opposite rotations, and the blades (72) and (82) are opposite in shape, ^ And the volume of the blade (82) is larger than the volume of the blade (72), so the airflow impacts the blade (82) of the turbine after a back pressure, and the gas expands to push the blade (82), so that the rear turbine (80) has an equivalent Turn the kinetic energy. The kinetic energy of the rear turbine will be fed back to the turbine (60) before the synchronous rotation, increasing the overall output power of the cylinder. Referring to the fifth figure, the cylinder (20) is located at the position of the front turbine (60), starting from the flow passage 8 1327949 (30), and has a _ auxiliary secret port (10) and two auxiliary rows along the front difficult rotation direction. The port (27) (28) and the flow path (3〇) are located between the intake port (26) and the second exhaust port (28). At the beginning of the rotation of the front turbine (6〇), due to the incomplete expansion of the gas, f is fast because of the high speed, and outside air will be drawn into the cylinder chamber at the suction port (26). When it is rotated to the exhaust port (27) (28), the gas has already expanded, and some gas is discharged from the exhaust port. During the running stroke of the front turbine (60), there is a pressure difference between the initial position (A) and the final position (B), which causes the front full wheel to be prone to rotational torque. When the cylinders are provided with the openings (26) (27) (28), the cylinder is a non-closed space, which can promote the smooth flow of the gas, thereby reducing the resistance of the turbine when rotating in the cylinder, and the energy of the gas. That is, it will not be worn out against resistance and drive the cylinder more efficiently. Further, when the outside air is replenished into the cylinder (1〇) from the intake port (26), it is used by the gas cylinder, so that the demand for the high pressure gas by the cylinder can be reduced, thereby reducing the gas consumption of the high pressure gas. When the cylinder is actuated, the two turbines (8 〇) and the reverse wheel (7 〇) are two-speed rotation in the opposite direction, and the gyro effect applied to the shaft when the thirsty wheel rotates and the gyro of the reverse wheel are applied to the shaft. The instrument effect is just the reverse sulfur elimination, reaching the balance, the gas red will not produce the torsion phenomenon, maintain stability, and avoid the fatigue of the operator. In addition to the cylinder, the cylinder of the present invention has no stator, but is a rotor (i.e., vortex, and reverse wheel), which is different from conventional cylinders. The counter-rotating reverse wheel increases the kinetic energy of the airflow, increases the power of the cylinder, and prevents the torsion of the pneumatic tool. And shouting π Hz π to make the cylinder effective (four) dynamic torque, and the gas consumption of high pressure gas. It will be understood that the present invention is not limited to the installation of two turbines and one counter-wheel, for example, three turbines and two counter-wheels disposed therebetween. In summary, the present invention is the first of its kind and has progressive merits 9