經濟部中央標隼局員工消費合作社印製 A7 _B7___ 五、發明説明（'） 發m 本發明係有關一種具有伸縮式加油系統的空中加油箱， 持別是指航空器作飛行中加油之用而结合於現存裝設於 機翼吊架內的一種裝置。 相關枝術說明 飛行中肮空器的加油系統已沿用多年>這類系統通常使 用一種被稱為’捲軸軟管及錐形套系統’。這類糸統說明 於下列的美國專利中：於1963年8月13日授予Morrow的 第3, 100 ,614號專利；於1962年10月30日授予Kirby的第 3,061 ,246號專利；於1986年12月30日授予Newmari的第 4,633 ,376號專利；於1978年6月20日授予Anderson等人 的第4,095,761號專利；於1985年9月11日授予Perrella 的第4,540,144號專利；由Boeing於1954年4月27日提出 的英國專利申請案第740,334號文件。 這些糸統中除Perrella的專利外，接受加油之肮空器 的空中加油探針都是一個自肮空器油箱突出的固定單位 。而Perrella的專利中，說明的是一種利用液壓驅動的 伸縮式的供油探针。這種單位是非常短且縮回裝設於航 空器的機身外殻之內。在這種探計的完全縮回位置上其 供油噴嘴是突出於外殻的。 瑄種習知的糸統中，整個探针或外殼或者其實質部分 不只在供油時而是一直都延伸到氣流內。這會給肮空器 帶來不必要的〇及/或^。此外，這種看得見的單 位立即為不友善的觀測者標示出該肮空器能進行長程作 -3- 本紙張尺度適用中國國家標準（CNS ) A4規格（210X297公釐） (讀先閱讀背面之注意事¾再填寫本頁)Printed by A7 _B7___ of the Consumer Cooperatives of the Central Bureau of Standards of the Ministry of Economic Affairs. 5. Description of the Invention (') The invention relates to an aerial refueling tank with a telescopic refueling system. A device installed in an existing wing hanger. Description of the relevant branch technique The refueling system of the aircraft in flight has been in use for many years > This type of system usually uses what is called a 'reel hose and conical sleeve system'. Such systems are described in the following U.S. patents: Patent No. 3, 100,614 issued to Morrow on August 13, 1963; Patent No. 3,061,246 issued to Kirby on October 30, 1962; and in 1986 Patent No. 4,633,376 issued to Newmari on December 30, 2014; Patent No. 4,095,761 granted to Anderson et al. On June 20, 1978; Patent No. 4,540,144 issued to Perrella on September 11, 1985; issued by Boeing in British Patent Application No. 740,334 filed on April 27, 1954. Except for Perrella's patents in these systems, the aerial refueling probe that accepts the refueling tank is a fixed unit protruding from the tank of the tank. In Perrella's patent, a telescopic oil supply probe using hydraulic drive is described. This unit is very short and retracted inside the fuselage housing of the aircraft. In the fully retracted position of this probe, its oil supply nozzle projects beyond the housing. In this conventional system, the entire probe or housing or its substantial part extends into the airflow not only during oil supply. This will cause unnecessary 0 and / or ^ to the dirty device. In addition, this visible unit immediately marked the unfriendly observer as capable of long-range operations. -3- This paper size applies to the Chinese National Standard (CNS) A4 specification (210X297 mm) (read first read (Notes on the back ¾ then fill out this page)
A7 B7 經濟部中央標隼局員工消費合作社印掣 五、發明説明（ 業而這項資訊會策略地不利於軍事作業。 同時，許多習知的空中加油系統中駕駛員很難在供油 作業期間方便地觀測到供油探針。當然，這使得探針與 加油軟管的接合變得更困難而可能需要另一飛行組員的 輔肋。在只有輩.人駕駛的戰鬥機中，基本上是要求駕駛 員能看到整個探針K利進行探針與加油軟管的接合。 ^明―一總1_ 本發明的系統較之習知的空中加油糸統是有極顯著的 改良，提供了能K適當角度向外作足夠延伸的可伸縮供 油探針使得駕駛員能於供油作業期間迅速看到此探針， 而這個探針能完全縮回油箱機身内使得探針不致對航空 器造成氣體動力學的(¾轉或拉引且在不供油時不致被看 出。 本發明的条統使用許多可伸縮導管構件而在最裡面的 構件的末梢端點上具有供油的噴嘴。利用可能屬電氣或 氣壓式馬達驅動可伸縮構件使之於伸展及縮回位置之間 移動。此種可伸縮構件於其縮回位置上是完全包含在航 空器的供油機身或其他外掛油箱内的。箱内的馬達上則 提供有「乾燥的J隔間K便使馬達和燃油隔離開。 最裡面的導管構件的探針噴嘴於其伸展位置上會作夠 遠的延伸且與航空器夾相對的角度使得駕駛員能從駕駛 艙很容易看到此探針。 利用與固定地黏著於最裡面的導管構件的之螺帽構件 聯合的長形插孔螺釘將馬達的轉動式驅動轉換成線性驅 -4- 本紙張尺度適用中國國家標準（CNS ) A4規格（210 X 297公釐） ----------- (請先閱讀背面之注意事項再填寫本頁)A7 B7 Printed by the Consumer Cooperatives of the Central Bureau of Standards of the Ministry of Economic Affairs 5. Invention Description (This information will be strategically detrimental to military operations. At the same time, it is difficult for pilots in many conventional aerial refueling systems to operate during fueling operations. The fueling probe is easily observed. Of course, this makes the engagement of the probe with the refueling hose more difficult and may require the auxiliary rib of another flight crew member. In a fighter aircraft with only one generation of human pilots, it is basically required The driver can see the entire probe K to facilitate the connection of the probe and the refueling hose. ^ Ming— 一 总 1_ The system of the present invention has a very significant improvement over the conventional aerial refueling system, which provides the ability K A telescopic fueling probe with sufficient extension outwards at an appropriate angle allows the pilot to quickly see the probe during fueling operations, and the probe can be fully retracted into the fuel tank fuselage so that the probe does not cause gas to the aircraft Dynamic (¾ turn or pull) and not visible when not supplying oil. The system of the present invention uses a number of retractable conduit members and has a nozzle for supplying oil at the distal end of the innermost member. Utilization May be an electric or pneumatic motor that drives the retractable member to move between the extended and retracted positions. This retractable member is fully contained in the aircraft's fuel supply fuselage or other external tank in its retracted position. The motor inside the box is provided with a "dry J compartment K to isolate the motor from the fuel. The probe nozzle of the innermost duct member will extend far enough in its extended position and opposite the aircraft clamp The angle makes it easy for the driver to see the probe from the cockpit. The elongated jack screw combined with the nut member fixedly attached to the innermost duct member converts the motor's rotary drive to a linear drive- 4- This paper size applies to China National Standard (CNS) A4 (210 X 297 mm) ----------- (Please read the precautions on the back before filling this page)
、1T •ο. kl B7 經濟部中央標準局員工消費合作社印製 五、發明説明 ( ) 1 1 動 9 以 便 馬 達 的 轉 動 蓮 動 能 導 致 最 裡 面 的 導 管 的 線 性 蓮 1 1 動 〇 其 他 可 延 伸 的 伸 编 式 導 管 中 可 能 有 一 個 兩 餡 或 更 1 | 多 値 9 是 利 用 第 二 插 孔 螺 釘 或 可 滑 動 的 驅 動 器 而 進 行 相 請 1 | 似 的 線 性 驅 動 以 回 應 馬 達 的 轉 動 式 驅 動 〇 鬩 1 1 讀 1 1 伸 縮 式 導 管 是 利 用 倒 轉 馬 達 致 導 管 作 反 向 的 線 性 蓮 動 背 © 1 I 之 1 而 縮 回 油 箱 内 〇 注 意 1 I 所 以 本 發 明 的 一 値 百 的 是 提 供 一 種 以 探 針 和 加 油 軟 管 ψ 項 1 1 型 式 作 供 油 連 接 的 改 良 式 空 中 供 油 % 統 〇 冉 填 寫 本 裝 本 發 明 的 另 一 掴 百 的 •是 提 供 一 種 利 用 能 兀 全 縮 回 航 空 頁 1 1 器 油 箱 内 之 伸 縮 式 導 管 的 空 中 供 油 条 統 〇 1 1 本 發 明 還 有 一 個 百 的 是 提 供 一 種 能 讓 駕 駛 員 能 從 駕 1 I 駛 艙 很 容 易 看 到 其 供 油 探 針 的 空 中 供 油 条 統 〇 I 1 訂 1 本 發 明 的 其 他 百 的 在 參 照 所 附 leal 圖 示 及 下 述 說 明 之 後 會 變 得 更 明 顯 〇 1 I 画 式 簡 述 1 1 第 1 圖 、 係 探 針 於 伸 展 位 置 的 上 佃 侧 面 簡 ran 圏 〇 1 第 2 圔 \ 偽 具 有 能 展 示 縮 回 油 箱 内 之 探 針 的 切 開 區 段 Q I 的 上 仰 側 面 簡 m 〇 1 1 第 3 圖 俗 具 有 能 展 示 馬 達 驅 動 器 的 上 佃 倒 面 簡 圖 〇 1 | 第 4 圖 % 沿 第 1 画 中 標 示 為 4- 4之平面的截面圖。 1 1 第 5 圖 N 偽 沿 第 4 圓 中 標 示 為 5- 5之平面的截面圖。 1 1 第 6 圈 % 沿 第 1 圖 中 標 示 為 6- 6之平面並能展示二 1 I 階 插 孔 螺 釘 及 桶 形 螺 帽 之 作 業 的 截 面 面 _ 〇 1 1 第 7 圔 Η % 沿 第 6 圖 中 標 示 為 7- 7之平面的截面_。 1 1 第 8 圖 、 係 沿 第 6 圖 中 標 示 為 8_ -8之平面的截面圖β 1 I 第 9 圖 、 偽 沿 部 分 截 面 用 來 -5- 展 示 二 階 插 孔 螺 釘 之 作 業 1 1 1 本紙張尺度適用中國國家標準（CNS ) A4規格（210X297公釐） 經濟部中央標準局貝工消費合作社印家 A7 B7 五、發明説明（4 ) 的h仰圃示。 第9a圖、係展示用來使二階插孔螺訂達成線性蓮動之 T -形柄的透視圖。 第1 0 _、係展示於機翼油箱加滿時用來截斷燃油不再 潦向油箱並將多餘的燃油轉移到另一油箱之截止閥的簡 略圖7K。 第1 1圖、係沿部分截面用來展示截止閥反轉送閥的上 仰側而簡圖。 第1 2 a - 1 2 C圖、係用來展示能讓駕駛員能看到的探針 位置。 第1 3園、係展示用來伸展及縮回伸縮式導管之替代機 制在導管接近縮回位置時的簡略圖示。 第1 4 _、係展示第1 3圖中替代機制在導管接近伸展位 置時的簡略願示。 發明的詳细說明 較钽置 「第1實施例] 第1圖和第2圖所展示的分別是本發明在伸展和縮回 位置上的系統。固定式導管30是固定地裝設於收納馬達 1 2之隔間1 4的外壁上。裝設於油箱1 6底壁上的隔間1 4屬 流密式使得馬達能與箱內的燃油隔開並因而保持乾燥。 油箱16可以是一個裝設於肮空器機翼17底下旳吊架。如 第2圖所示於縮回位置上，中間導管18伸入外側的固定 式導管30内而内側導管27則伸入中間導管18内。內側導 -6 - 本紙張尺度適用中國國家樣準（CNS ) A4規格（210X297公嫠） --------裝------訂--^------- (請先閲讀背面之注意事項再填寫本頁) 經濟部中央標隼局員工消費合作社印製 A7 __B7五、發明説明（：） 管在末梢端點上具有供油的探针噴嘴28M便和軟管结合 而將燃油灌進油箱16內。 參照第1丽為了方便駕駛員於供油期間的観測。對特 定的航空器而言探針28必須從吊架向外延伸一個適當的 水平距雛「Η」、一個適當的鉛直距離「V」、Μ及一個 適當的角度「A」。每一個安裝都必須Μ實驗決定出最 佳的參數。對F-16戰機而言，這些參數已經決定如下： Η = 8 4 英十、A = 1 0 ° 、而 V = 3 4 英寸。 規在參照第3圖到第9a_中所展示的是用來在伸展與 縮回位置之間驅動該裝置的驅動機制。 如第3圖所示，將可能是電氣或液壓式的驅動馬達12 支撐於流密式或.「乾燥」而裝設於油箱1 6底壁上的隔間 14內部。馬達的驅動機軸是利用螺拴10固定地黏著於有 螺紋的機軸或插孔螺钉11 a上。插孔螺釘11 a實質上是沿 整個長度攻上螺紋如第4圖和第5圖中可Μ看得最清楚 ，依螺紋结合桶形螺帽構件15而固定地黏著於基礎延伸 導管18上。利用桶形螺帽配件對基礎延伸導管18的轉動 摩擦阻抗防止這個配件發生轉動，因此Κ插孔螺钉1 1 a 的轉動而線性驅動該延伸導管18。 如第6圖所示，形成第二插孔螺訂的管狀機軸lib呈 外部崗心的套在插孔螺钉11a上。對第一插孔螺釘而言， 第二插孔螺釘的外壁也是實質上沿整個長度攻有螺紋。 第二插孔螺釘依螺紋結合固定地黏著於內側延伸導管2.7 上的桶形螺帽25。從第9圖和第9a圖中可K看得最清楚 ~ 7 - (讀先閱讀背面之注意事項再填寫本頁) .裝-, 1T • ο. Kl B7 Printed by the Consumer Cooperative of the Central Standards Bureau of the Ministry of Economic Affairs. 5. Description of the invention () 1 1 Motion 9 so that the kinetic energy of the rotation of the motor results in the linear lotus of the innermost catheter 1 1 Motion 〇 Other extendable extensions There may be a two-filler or more in the braided catheter | Multi 値 9 is the use of a second jack screw or a slidable drive for 1 phase 1 | Similar linear drive in response to the rotary drive of the motor 0 阋 1 1 read 1 1 The telescopic catheter is a linear linear moving back that uses an inverted motor to cause the catheter to reverse. 1 1 of 1 is retracted into the fuel tank. 0 Note 1 I Therefore, a hundred of the present invention is to provide a probe and refueling soft Pipe ψ Item 1 1 Improved aerial fuel supply for fuel supply connection% System 0 Ran fill in this package Another hundred of the invention is to provide a benefit The aerial fuel supply system with retractable duct in the fuel tank of the aviation page can be fully retracted. The invention also provides a method for the driver to easily see from the 1 I cockpit. The air fuel supply system to its fueling probe. 0I 1 Order 1 The other hundred of the present invention will become more apparent after referring to the attached leal diagram and the following description. 0 1 Brief description of the picture 1 1 1 picture, the upper side of the probe with the probe in the extended position, Jan ran 〇〇1 2 圔 \ pseudo-up side with a cut section QI that can show the probe retracted in the fuel tank, Jan m 〇1 1 3 There is a simplified top view showing the top and bottom of the motor driver. 〇1 | Figure 4% Sectional view along the plane labeled 4-4 in the first picture. 1 1 Fig. 5 N Pseudo-section view along the plane marked 5-5 in the 4th circle. 1 1 6th circle% Along the plane marked 6- 6 in the first figure and showing the operation of the 2 1-stage jack screw and barrel nut _ 〇1 1 7th 圔 Η% along the 6th The cross section of the plane marked 7-7 in the figure. 1 1 Fig. 8 is a cross-sectional view along the plane labeled 8_ -8 in Fig. 6 β 1 I Fig. 9 is a cross-section of a pseudo-pronged section used to show the work of a second-order jack screw 1 1 1 This paper The scale is applicable to the Chinese National Standard (CNS) A4 specification (210X297 mm). The Ajia B7, a consumer printing cooperative of the Central Standards Bureau of the Ministry of Economic Affairs, A7 B7. 5. The description of the invention (4). Fig. 9a is a perspective view showing a T-shaped handle for making the second-order jack screw to achieve linear motion. The 10th, _, is shown in Figure 7K of a simple stop valve used to cut off the fuel when the wing fuel tank is full. It is no longer facing the fuel tank and transferring excess fuel to another fuel tank. Figure 11 is a simplified diagram showing the upward side of the shut-off valve to the reverse feed valve along a partial section. Figures 1 2 a-1 2 C are used to show the position of the probe that can be seen by the driver. Section 13 shows a schematic diagram of an alternative mechanism for extending and retracting a telescopic catheter as the catheter approaches the retracted position. Figure 1 4 _ shows a brief wish of the alternative mechanism in Figure 13 when the catheter is close to the extended position. Detailed description of the invention "First embodiment" Figures 1 and 2 show the system of the present invention in the extended and retracted positions, compared to tantalum. The fixed catheter 30 is fixedly installed in the storage motor. 12 on the outer wall of compartment 14. The compartment 14 installed on the bottom wall of the fuel tank 16 is fluid-tight so that the motor can be separated from the fuel in the tank and thus kept dry. The fuel tank 16 can be a container The hanger is located under the airfoil wing 17. In the retracted position as shown in Fig. 2, the intermediate duct 18 extends into the outer fixed duct 30 and the inner duct 27 extends into the middle duct 18. The inner guide -6-This paper size is applicable to China National Standard (CNS) A4 (210X297 cm) -------- installation ------ order-^ ------- (please first Read the notes on the back and fill in this page) Printed by A7 __B7, Employee Consumer Cooperative of the Central Bureau of Standards of the Ministry of Economy Fill the fuel into the fuel tank 16. Refer to Dili for the convenience of the pilot during fueling. Probe 28 is necessary for certain aircraft Extending outwardly from the hanger level from a proper child "Η", a suitable vertical distance "V", [mu] and a suitable angle "A." For each installation, M experiments must determine the best parameters. For F-16 fighters, these parameters have been determined as follows: Η = 8 4 inches, A = 1 0 °, and V = 3 4 inches. The gauge shown in reference to Figures 3 to 9a_ is the drive mechanism used to drive the device between the extended and retracted positions. As shown in Fig. 3, the drive motor 12 which may be an electric or hydraulic type is supported inside the compartment 14 on the bottom wall of the fuel tank 16 by being fluid-tight or "dry". The drive shaft of the motor is fixedly attached to the threaded shaft or the socket screw 11a by a bolt 10. The socket screw 11a is substantially the best seen when tapping the thread along the entire length, as shown in Figs. 4 and 5, and is fixedly adhered to the base extension tube 18 by screwing in combination with the barrel nut member 15. The frictional resistance of the barrel extension nut to the base extension tube 18 is prevented by the frictional resistance. Therefore, the rotation of the K socket screw 1 1 a linearly drives the extension tube 18. As shown in Fig. 6, the tubular shaft lib forming the second jack screw is sleeved on the jack screw 11a with an external core. For the first socket screw, the outer wall of the second socket screw is also threaded along substantially the entire length. The second socket screw is fixedly adhered to the barrel nut 25 on the inner extension duct 2.7 by screwing. K can be seen most clearly from Figures 9 and 9a ~ 7-(Read the precautions on the back before filling this page).
、1T 4 本紙張尺度適用中國國家標準（CNS ) Α4ϋ格（210X29*7公釐） 經濟部中央標準局員工消費合作社印繁 A7 B7 五、發明説明u ) ,T -形驅動柄29是Μ T的頂部固定地黏著於第二插孔螺 钉lib的内壁上。第一（內側）插孔螺釘11a具有沿其縱軸 延伸的凹槽11c而其上依可滑動方式騎有此T的底下部 分。因此，插孔螺钉1 1 a的轉動會轉移到插孔螺釘11 b上 而插孔螺釘Ub會沿插孔螺钉11a滑動因而同時為插孔螺 钉11 b提供了線性及轉動式的運動。 如上文所指出的，第二插孔螺钉lib依螺紋結合固定 地黏著於内側延伸導管27上的桶形螺帽25。導管27在末 梢端點上具有供油的探針噴嘴28。因此，插孔螺钉lib 的轉動運動線性驅動了導管27。截止構件32(參見第6圖 和第8圖）從導管1 8的內壁延伸出來K限制內側導管2 7 相對於中間導管的向前運動。 因此，内側導管構件27及中間導管構件18是依互為相 對於固定式導管30的方式而線性驅動到一個延伸位置上 。瑄些導管構件是利用倒轉馬達的轉動而驅動到油箱內 的縮回位置上。 攸闢低速加油穩定度之肮空器供油系統的分布必需能 同時將燃油分配到內部和外部的油箱中。這是藉氣壓方 式達成的且於使用空中加油箱時是不會實施的。於加油 期間，如同Μ傳統的裝設於機翼的油箱一般是將燃油轉 移到所有的內部油箱內。不過，為了提供朝相對另一機 翼上外部油箱（吊架）的燃油流，可能在肮空器的供油糸 統內安裝一個止逆閥38(參見第10圖和第11圖）。如第11 圃所示，此一止逆閥38是一種具有兩段式螺旋管操作的 -8 - 本紙張又度適用中國國家標準（CNS ) Α4規格（210Χ297公釐〉 ---------0^------、玎------Q (請先閱讀背面之注意事項再填寫本頁) A7 B7 五、發明説明（7 ) 習知三通閥。這取代了通常的單通閥而容許透過習用的 空中加油儲槽而加油到外部油箱內。兩段式三通閥同時 允許透過空中加油箱和空中加油儲槽進行加油作業。 如第10圖所示，於供油系統内提供了一個截止閥19。 這個閥在加油期間是打開的Μ便將由探針取得的燃油轉 移到所有的内部和外部油箱中。當加油箱16加滿時，油 箱的準位感測器會關閉截止閥19使得燃油不再灌進油箱 16而轉移到其他的內部和外部油箱中。另外，當所有的 內部和外部油箱都加滿且終止加油時，截止閥19會打開 Κ便允許探針内側的任何剩餘燃油灌進油箱16內。 現在參照第12a圖到第12c圖中的簡圖，是用來展示將 探針放在能方便駕駛員作觀測的位置上。如上文所指出 的，參照第1圖所示探針的放置決定了這項结果。必須 作這樣的放置以便面朝加油機的駕駛員能觀測到探針。 這是依實驗為每一種型式的肮空器決定其條件。如第12a 圖和第12b圔所示的這些參數係鼷於F-16戰機的，其中所 展示的角度是駕駛員自駕駛艙的觀測角。 現在參照第13圖和第14圖，係根據本發明探針之替代 實施例的簡略圖示。 經濟部中央標隼局員工消費合作社印製 (請先閱讀背面之注意事項再填寫本頁) [第2實施例] 如同第1實施例是利用馬達將瑄種探針從縮回位置驅 動到伸展位置，其中是利用结合了至少固定於導管之一 的螺帽的插孔螺釘而使馬達的轉動轉換成線性蓮動。此 實施例與第1實施例的不同配置是用來驅動中間導管的 -9- 本紙張尺度適用中國國家標隼（CNS ) A4規格（210X297公釐） 經濟部中央標準局員工消費合作社印掣 A7 B7 五、發明説明（/ ) 驅動機制Μ及第一和第二插孔螺訂之間的驅動器。這裡 會用相同的標碼Κ標示出第2實施例中與第1實腌例相 同的零件。第13圖所展示的探針是幾乎落在完全縮回的 位置上而第14隱所展示的探針是落在伸展的位置上。 插孔螺釘11a是固定地黏著於可能是電氣或水壓式的 馬達1 2驅動機軸上。插孔螺訂11 a實質上是沿整個長度 攻有螺紋。圓形環40是固定地黏著於插孔螺釘11a的末 梢端點上，這個環的表面上有嚙合或狗牙41。插孔螺訂 11 b是空心狀且呈外部同心地套在插孔螺釘11 a上。位於 插孔螺钉lib —端的套頭部分44在其內側表面上具有螺 紋43可與其外側表面上攻有螺紋的插孔螺釘11a结合。 插孔螺钉lib的末梢端點是利用滑動軸承46支撐於内側 導管27的內壁上。套頭部分44是利用球體軸承48支撐於 圓形環50上。插孔螺訂lib的圓形終端板58上有嚙合或 狗牙79。於圓形環50及滑動軸承配件內提供燃油孔Μ便 允許燃油通過其間。 其上固定地黏著有圓形環52的內側導管27上攻有螺紋 部分5 3是可以和插孔螺钉1 1 b外側表面上的螺紋結合。 中間導管18有一個鍵槽57是圼縱軸走向而沿其內壁通過 ，而內側導管27外壁上的圓形環60在防止内側導管轉動 下装配並騎乘其上。固定式外側導管30上也有類Μ於此 的鍵槽62,而中間導管18的環形構件64則騎乘其上Μ防 止中間導管轉動。滑動軸承70及燃油封口 72是提供於外 御導管30與中間導管18之間以及中間導管18與内侧導管27之間， -1 0 _ 本紙張尺度適用中國國家標準（CNS ) Α4規格（210X297公釐） ---0^-- (請先閲讀背面之注意事項再填寫本頁) 、va d. A7 B7 經濟部中央標準局員工消費合作社印掣 五、發明説明 (、 ) 1 1 這 軸 承 及 封 □ 是 在 從 外 側 及 中 間 導 管 延 伸出 來的圓形 1 1 1 環 74內 側 表 面 上 〇 於 內 側 導 管 27 中 所 有 的 環及 軸承配件 1 內 提 供 開 □ 以 確 保 燃 油 通 過 其 中 〇 請 1 先 1 根 據 本 發 明 第 2 實 施 例 之 裝 置 操 作 如 下 :在 完全縮回 閲 讀 1 的 位 置 上 (第1 3圖所示係沿伸展方向自完全縮回位置移 背 1 之 1 出 少 許 距 離 )， 插孔螺釘1 1 a 上 的 狗 牙 59 a結合相對插孔 兔· ! I 螺 訂 lib上的狗牙59b而 有 效 地 將 兩 個 插 孔 螺釘 鎖在一起 事 項 再 1 ▲ 〇 導 管 27上 攻 有 螺 紋 部 分 53 是 可 Μ 和 插 孔 螺釘 11 b外側 填 寫 本 m 裝 表 面 上 的 螺 紋 结 合 〇 這 兩 個 插 孔 螺 訂 會 與 導管 27—起轉 頁 1 1 動 ♦ 而 導 管 27 的 驅 動 是 透 過 和 插 孔 螺 訂 11 b外側表面螺 1 1 紋 結 合 的 攻 有 母 螺 紋 部 53而 達 成 的 〇 如 上 所述 ,內側導 1 1 管 27 因 環 形 構 件 60嚙 合 於 鍵 槽 57 內 而 不 致 轉動 。所Μ , 1 訂 內 側 導 管 27 會 受 到 線 性 驅 動 〇 當 內 側 導 管 27延 伸得夠遠 1 時 ♦ 環 形 構 件 60 畲 與 相 對 的 環 74 a结合 >中間導管1 8是 1 I 透 過 球 體 軸 承 48 而 連 接 到 插 孔 螺 訂 lib 上， 此軸承在利 1 1 用 鐽 槽 57防 止 中 間 導 管 18 轉 動 下 允 許 插 孔 螺钉 lib轉動 | 0 中 間 導 管 18會 向 外 延 伸 直 到 其 tea 環 形 構 件 64與 外側導管 30 的 相 對 的 rtax 環 74b毗連於如第14圖所示探針呈完全伸展 1 I 的 一 涸 點 上 〇 1 探 針 是 利 用 逆 轉 馬 達 的 轉 動 方 向 而 縮 回 。這 會導致內 1 I 側 插 扎 螺 釘 11 a沿相反方向轉動 3因摩擦力防止了外側 1 1 插 孔 螺 釘 lib的轉動而導致外側插孔螺釘行縮回的線性 1 1 運 動 〇 外 側 插 孔 螺 訂 隨 著 其 縮 回 運 SL, 動 而 將 上鎖 的中間導 1 I 管 向 後 驅 動 〇 一 Μ 外 側 插 孔 螺 钉 1 1 b完全縮回， 内側及 1 1 -1 1 - 1 1 1 1 本紙張尺度適用中國國家標準（CNS〉A4規格（210X297公嫠） A7 B7 五、發明説明（、。） 外側插孔螺訂上的嚙合齒會依連结嚙合的方式一起受到 驅動。這導致外側插孔螺钉lib的轉動進而驅動内側導管 攻有螺紋部分53。內側導管因為將其圓形環60鎖在凹槽 57内而不致轉動反倒線性地向內移動直到抵達完全縮回 的位置上為止。 雖然本發明完全是參照所附圖表上的例子而作的描述 ，不過應該了解本發明並不局限於此而僅受限於下列所 附專利申請範圍。 (請先閲讀背面之注意事項再填寫本頁) 經濟部中央標準局負工消費合作社印家 -12- 本紙張尺度適用中國國家標準（CNS ) A4規格U10X297公釐） A7 B7 五、發明説明（w ) 符號參考說明 I 0 ...螺栓 II a ...插孔螺訂 1 1 b ...機铀 1 1 c ...凹槽 1 2 ...馬達 1 4 ...隔間 1 5 , 2 5 ...桶形螺帽 16 ...油箱 17.. .機翼 18.27.30.. .導管 1 9 ...截止閥 .探針（唄嘴） .驅動柄 28 29 32 38 截止構 止逆閥 件 ----- (請先閱讀背面之注意事項再填寫本頁) 裝. 、\-° 經濟部中央標率局貝工消費合作社印製 40,50,52,6 0，64,74 ...圓形環 41，593,5913，179...嚙合（或狗牙 4 3 ...螺紋 44 ...套頭部分 46,70...滑動軸承 48 ...球體_軸承 5 3 ...攻有螺紋部分 57,62 ...鐽槽 58 ...圓形終端板 7 2 ...燃油封口 13 本紙張尺度適用中國國家標準（CNS ) A4規格（21〇Χ：297公釐）、 1T 4 This paper size applies to Chinese National Standards (CNS) Α4210 格 (210X29 * 7mm) Employees' Cooperatives of the Central Standards Bureau of the Ministry of Economic Affairs Consumer Cooperatives A7 B7 V. Description of the invention u), T-shaped drive handle 29 is Μ T The top is fixedly adhered to the inner wall of the second jack screw lib. The first (inside) jack screw 11a has a groove 11c extending along its longitudinal axis and the bottom portion of the T is slidably mounted thereon. Therefore, the rotation of the jack screw 11a is transferred to the jack screw 11b and the jack screw Ub slides along the jack screw 11a, thereby providing a linear and rotary motion for the jack screw 11b. As indicated above, the second socket screw lib is fixedly adhered to the barrel nut 25 on the inside extension duct 27 by a screw connection. The conduit 27 has an oil-supplying probe nozzle 28 at the tip end. Therefore, the rotational movement of the jack screw lib drives the catheter 27 linearly. A cut-off member 32 (see FIGS. 6 and 8) extends from the inner wall of the catheter 18 to restrict forward movement of the inner catheter 2 7 relative to the middle catheter. Therefore, the inner duct member 27 and the middle duct member 18 are linearly driven to an extended position in a manner relative to the fixed duct 30. Some of the duct members are driven to the retracted position in the fuel tank by the rotation of the reversing motor. The distribution of the fuel supply system for low-speed refueling systems must be capable of distributing fuel to both internal and external tanks. This is achieved by air pressure and is not implemented when using aerial refueling tanks. During refueling, M's traditional wing-mounted fuel tanks typically transfer fuel to all internal fuel tanks. However, in order to provide fuel flow to an external tank (pylon) opposite the other wing, it may be possible to install a check valve 38 in the fuel supply system of the submersible (see Figures 10 and 11). As shown in the 11th garden, this non-return valve 38 is a -8 with a two-stage spiral tube operation. This paper is again applicable to the Chinese National Standard (CNS) A4 specification (210 × 297 mm> ------ --- 0 ^ ------, 玎 ------ Q (Please read the notes on the back before filling this page) A7 B7 V. Description of the invention (7) Know the three-way valve. This replaces A common one-way valve allows refueling to an external tank through a conventional aerial refueling tank. A two-stage three-way valve allows refueling operations through both the aerial refueling tank and the aerial refueling tank. As shown in Figure 10, A shut-off valve 19 is provided in the fuel supply system. This valve is open during refueling and transfers the fuel obtained by the probe to all internal and external fuel tanks. When the fuel tank 16 is full, the fuel tank level The sensor will close the shut-off valve 19 so that the fuel is no longer filled into the fuel tank 16 and transferred to other internal and external tanks. In addition, the shut-off valve 19 will open when all the internal and external tanks are full and the refueling is terminated This allows any remaining fuel inside the probe to be poured into the fuel tank 16. Now refer to The diagrams in Figures 12a to 12c are used to show that the probe is placed at a position that is convenient for the driver to observe. As pointed out above, referring to Figure 1, the placement of the probe determines this. As a result, it must be placed so that the driver facing the tanker can observe the probe. This is determined experimentally for each type of dirty tank. These parameters are shown in Figure 12a and 12b 圔For F-16 fighters, the angle shown is the angle of observation from the cockpit of the pilot. Reference is now made to Figures 13 and 14, which are schematic illustrations of alternative embodiments of the probe according to the present invention. Economy Printed by the Ministry of Standards and Labor Administration's Consumer Cooperative (please read the precautions on the back before filling out this page) [Second Embodiment] As in the first embodiment, the probe is driven from the retracted position to the extended position by a motor Among them, the rotation of the motor is converted into a linear motion by using a jack screw combining at least one nut fixed to one of the catheters. The different configuration of this embodiment from the first embodiment is to drive the -9 of the intermediate catheter. -This paper size applies to China National Standard (CNS) A4 specification (210X297 mm) A7 B7 printed by the Consumer Cooperatives of the Central Standards Bureau of the Ministry of Economic Affairs 5. Description of the invention (/) The drive mechanism M and the drive between the first and second jacks. Here, the same code K is used to mark the same parts in the second embodiment as in the first solid picking example. The probe shown in Figure 13 is almost in the fully retracted position and the probe shown in Figure 14 is shown. The probe is in the extended position. The jack screw 11a is fixedly attached to the drive shaft of the motor 12 which may be electric or hydraulic. The jack screw 11a is threaded along substantially the entire length. The circular ring 40 is fixedly adhered to the distal end of the jack screw 11a, and the surface of this ring has a meshing or dog tooth 41. The socket screw 11b is hollow and is concentrically sleeved on the socket screw 11a. The ferrule portion 44 at the end of the jack screw lib has a thread 43 on its inner surface to be combined with a jack screw 11a tapped on its outer surface. The distal end of the jack screw lib is supported on the inner wall of the inner duct 27 by a sliding bearing 46. The ferrule portion 44 is supported on the circular ring 50 by a ball bearing 48. The circular terminal plate 58 of the jack screw lib has a meshing or dog tooth 79 on it. A fuel hole M is provided in the circular ring 50 and the sliding bearing fitting to allow fuel to pass therethrough. A threaded portion 5 3 is tapped on the inner duct 27 to which the circular ring 52 is fixedly adhered, and can be combined with the screw on the outer surface of the jack screw 1 1 b. The intermediate duct 18 has a keyway 57 which runs along the longitudinal axis of the diaphragm and passes along its inner wall, while a circular ring 60 on the outer wall of the inner duct 27 is assembled and rides on to prevent the inner duct from rotating. The fixed outer tube 30 also has key grooves 62 similar thereto, and the ring member 64 of the middle tube 18 rides on it to prevent the middle tube from rotating. The sliding bearing 70 and the fuel seal 72 are provided between the outer duct 30 and the middle duct 18 and between the middle duct 18 and the inner duct 27. -1 0 _ This paper size applies to China National Standard (CNS) A4 specification (210X297) (%) --- 0 ^-(Please read the precautions on the back before filling out this page), va d. A7 B7 Printed by the Consumers' Cooperatives of the Central Standards Bureau of the Ministry of Economic Affairs 5. Description of the invention (,) 1 1 This bearing and The seal □ is provided on the inside surface of the circular 1 1 1 ring 74 extending from the outer and middle ducts. □ Provides openings in all the rings and bearing fittings 1 in the inner duct 27 to ensure that the fuel passes through it. The operation of the device according to the second embodiment of the present invention is as follows: at the fully retracted reading position 1 (shown in Figure 13 is a slight distance from the fully retracted position 1 in the direction of extension in the direction of extension), the jack screw 1 1 a dog teeth on a 59a combined with a relative jack rabbit! I screw dog teeth 59b on lib Effectively lock the two socket screws together. 1 ▲ 〇 The threaded part 53 on the guide tube 27 is available and the socket screw 11 b is filled with the thread on the mounting surface. The two socket screws are combined. The reservation will be performed with the catheter 27—from page 1 to 1. The drive of the catheter 27 is achieved by tapping the female screw 53 with the screw 11 1 on the outside surface of the jack screw, as described above. The guide 1 1 tube 27 is prevented from rotating because the ring member 60 is engaged in the key groove 57. Therefore, the inner tube 27 will be linearly driven. When the inner tube 27 extends far enough 1, the ring member 60 结合 is combined with the opposite ring 74 a > the middle tube 1 8 is 1 I connected through the ball bearing 48 To the jack screw lib, this bearing allows the jack screw lib to rotate with the groove 57 to prevent the middle tube 18 from turning | 0 The middle tube 18 will extend outward until its tea ring member 64 and the outer tube 30 The opposite rtax ring 74b is adjacent to a point where the probe is fully extended 1 I as shown in Fig. 14. The probe is retracted by reversing the direction of rotation of the motor. This will cause the inner 1 I side insert screw 11 a to rotate in the opposite direction. 3 The linear movement of the outer jack screw retracted due to the frictional force preventing the rotation of the outer 1 1 jack screw lib 1 1 The outer jack screw binding As it retracts the SL, it moves the locked middle guide 1 I tube backwards. The outer side socket screw 1 1 b is fully retracted. The inside and 1 1 -1 1-1 1 1 1 paper size Applicable to Chinese national standard (CNS> A4 specification (210X297 male)) A7 B7 V. Description of the invention (, ...) The engaging teeth on the outer jack screw will be driven together in a manner of joint engagement. This results in the outer jack screw The rotation of lib further drives the inner catheter to tap the threaded portion 53. The inner catheter, due to its circular ring 60 locked in the groove 57, does not rotate but moves linearly inward until it reaches the fully retracted position. Although the present invention The description is made entirely with reference to the examples on the attached drawings, but it should be understood that the present invention is not limited to this but is limited only by the scope of the following attached patent applications (Please read the notes on the back before filling out this page) Yin Jia, Consumer Work Cooperative of the Central Bureau of Standards, Ministry of Economic Affairs -12- This paper size applies to Chinese National Standard (CNS) A4 specification U10X297 mm) A7 B7 V. Description of the invention (W) Symbol reference description I 0 ... bolt II a ... jack screw 1 1 b ... machine uranium 1 1 c ... groove 1 2 ... motor 1 4 ... compartment 1 5, 2 5 ... barrel nut 16 ... fuel tank 17.. Wing 18.27.30... Conduit 1 9 ... shut-off valve. Probe (pout). Drive handle 28 29 32 38 Cut-off check valve ----- (Please read the precautions on the back before filling this page). 、 \-° Printed by the Bayer Consumer Cooperative of the Central Standards Bureau of the Ministry of Economic Affairs 40,50,52,6 0,64,74 ... round ring 41,593,5913,179 ... engage (or dog teeth 4 3 ... thread 44 ... sleeve part 46,70 ... slide bearing 48 ... Sphere_Bearing 5 3 ... Threaded portion 57,62 ... Slotted groove 58 ... Circular terminal plate 7 2 ... Fuel seal 13 This paper size is applicable to China National Standard (CNS) A4 specification (21 〇Χ: 297 mm)