201036869 六、發明說明： 【發明所屬之技術領域】 本發明是有關於一種降落傘，特別是指一種可判定適 當開傘時機，以自動且即時地啟動開傘動作的自動安全啟 動降落傘。 【先前技術】 降落傘是應用空氣阻力原理的—㈣動力減速器，^ 時折疊於包内’並透過-連接元件與—降諸相連接，且方 使用時可展_增加該㈣體的運動阻力，使其減速下降妾 穩定其運動姿態’藉此，能達到使該降落體穩定且安全㈣ 落到地面的目的。 參閱圖1與圖2,現有的-降落傘！具有-個適於背, 在-使用I 10或一物體上的背袋u、一收納在該背袋i 内的增12、一設置在該背袋u上用於開啟該背袋i 使該主傘部12自該背脫出的扣件13，及—與該扣利 π相連接的拉、繩14。當—使用者ig自高空降料，在㈣ 一段預定距離處，需以年勤古斗 而手動方式拉動該拉，繩14以將該扣科 13解開，使該背袋U開啟，進而使該主伞部 ： 由收折狀態展開為傘狀，該主切12展開後就能增大阻力 面’產生減速和穩定使用者1〇 得以安全著陸。 妾勢的作用，讓該使用者Η 然料的降落傘1可於使用時展開以增加下降阻力 進而達到女全著陸的目的 扪仁貫際上仍具有下列缺失： …以手動方式開伞時’則使用者ι〇需有精確的判 201036869 斷力掌握開傘時機才能確保安全著陸，若太快開傘，則該使 用者H)在高空停留的時間較久’容易受氣流吹動而遠離預 定的㈣目標，可能造成該使用者1Q迷失方位，或因降落 地點不佳而危及使用者1G的安全，若太慢開傘，則著地時 的下墜速度無法獲得充份緩衝，易導致該使用者ig在著地 時受傷，此外’在高速下降的過程中，若使用者1〇突然身 體不適或昏迷，則會因錯失開傘時機而造成嚴重的意外’，、因 此’現有手動方式開傘的降落傘i易因使用者1〇的判斷錯 誤而發生危險，而有安全性相對較不足的缺失。 曰 二、以手動拉動該拉繩14解開該扣件13以開啟背代 U ’進而讓主傘部12張開的開傘方式，易因下降過程中; 拉繩Μ被使用者10身上的其他配件纏住，或因該扣件η 與該拉繩14之間的連動機構老舊無法順利作動，導致無去 解開扣件⑴同樣會造成嚴重的意外事件，而使現有降落 傘1具有安全性相對較低的缺失。 【發明内容】 因此，本發明的目的，是在提供一種能夠在適當時機 自動且即時地進行開㈣作，以增加降落傘使用上之安全 性的自動安全啟動降落傘。 王 _於是，本發明自動安全啟動降落伞，包含一降落伞單 疋，及一用以啟動該降落傘單元開傘的控制裝置。 該降落傘單元包括一個適於背負與固定在一降落體上 的收納背袋、—個分別能夠被收藏在該收納背袋内，與自 k收、.内者袋稅出並展開成一傘狀的傘主體、一個設置在，201036869 VI. Description of the Invention: [Technical Field] The present invention relates to a parachute, and more particularly to an automatic safety start-up parachute capable of determining an appropriate opening time to automatically and instantly activate an opening operation. [Prior Art] The parachute is based on the principle of air resistance—(4) the power reducer, which is folded into the bag and connected through the connecting element and the falling element, and can be used to increase the motion resistance of the body. It slows down and stabilizes its motion posture', thereby achieving the purpose of making the landing body stable and safe (4) falling to the ground. See Figure 1 and Figure 2 for the existing - parachute! Having a back pocket u on the use of I 10 or an object, an increase 12 contained in the back pocket i, and a setting on the back pocket u for opening the back pocket i The fastener 13 from which the main umbrella portion 12 is detached, and the pull and rope 14 connected to the buckle π. When the user ig descends from high altitude, at a predetermined distance of (4), the pull is manually pulled by the old and the old, and the rope 14 is unwrapped to open the back pocket U, thereby enabling the back pocket U to be opened. The main umbrella portion is expanded into an umbrella shape from the folded state, and the main cut 12 can be expanded to increase the resistance surface to generate a deceleration and stabilize the user 1 to safely land. The effect of the squatting effect is that the user's parachute 1 can be deployed to increase the resistance to fall and thus reach the full landing of the woman. The cockroaches still have the following deficiencies: ... when manually opening the umbrella The user needs to have an accurate judgment of 201036869. The breaking force can be used to ensure a safe landing. If the umbrella is opened too quickly, the user H) stays at a high altitude for a long time 'easy to be blown by the airflow away from the predetermined one. (4) The target may cause the user to lose position in 1Q, or the safety of the user 1G may be endangered due to poor landing location. If the umbrella is too slow, the falling speed when landing will not be fully buffered, which may lead to the user. Ig was injured when he landed. In addition, in the process of high-speed descent, if the user suddenly becomes unwell or comatose, he or she will be seriously accidentally missed by the opportunity to open the umbrella. The parachute i is dangerous due to a user's judgment error, and there is a lack of safety. Secondly, by pulling the pull cord 14 manually to unlock the fastener 13 to open the back U' and then opening the main umbrella portion 12, the method of opening the umbrella is easy to fall; the drawstring is worn by the user 10 The other accessories are entangled, or because the interlocking mechanism between the fastener η and the pull cord 14 is old and cannot be smoothly operated, so that the unfastening of the fastener (1) can also cause serious accidents, and the existing parachute 1 is safe. Relatively low loss. SUMMARY OF THE INVENTION Accordingly, it is an object of the present invention to provide an automatic safety start parachute that can automatically and instantly perform an open (four) operation at an appropriate time to increase the safety of use of a parachute. Wang _ Thus, the present invention automatically and safely activates the parachute, including a parachute trailer, and a control device for activating the parachute unit to open the umbrella. The parachute unit comprises a storage bag adapted to be carried and fixed on a falling body, which can be respectively stored in the storage bag, and is taxed and unfolded into an umbrella shape. Umbrella body, one set,
201036869 背袋上並能相互接合與脫離以分別使該收納背袋收合與張 開的開關組合體’及多數條相間隔地連接 與該收納背袋之間的傘繩。 體周緣 該控制裝置包括一個連動該開關組合體自相接合的關 閉狀態轉換為相脫離的開啟狀態的磁控單元'一個控制該 磁控早7L作動的控制單元、一個與該控制單元電連接的中 央處理單元、分別與該中央處理單元電連接以傳送資料至 該中央處理單元的—個加速旋轉定向器、_個全球衛星定 位(GPS)系統單元及一個輸入單元’該加速旋轉定向器是用 以量測該降落體下降過程中在相垂直的—前後方向、一水 平方向及一直立方向上的旋轉速度。 。个知a的有盃效果在於：藉由與該控制裝置之中央處 理T元相連接的加速旋轉定向器與全球衛星定位系統單： 可量測該降落體下降過程中的高度變化與旋轉情形，再配 :以該輸入單元所設定的落地剩餘時間’及該降落體在前 後、水千及直立方向上的旋轉速度之合角速度的上限值， : = 理單元能根據所接收的資料與設定值在預定的 %間點啟動該㈣單元’以透過該控制單元使該磁控單元 作動，帶動該開關組合體由關閉狀態轉換為開啟狀 納背袋被打開，以便於該伞主體能在預定二 該收納^脫出並展開成傘狀，讓該降落體可安 與旋轉速度變化，以即的高度 …入^即時開伞，而具有使用時的穩定性愈 女全性相對較佳的特性與優點。 - 5 201036869 【實施方式】 有關本發明之前述及其他技術内容、特點與功效，在 Γ配合參考圖式之―個較佳實施例的詳細說明中，將可 清楚的呈現。 >閱圖3 ®4與圖5’本發明自動安全啟動降落傘2 Ϊ較W]包含—降落傘單元3,及-肋啟動該降落伞 早元3開傘的控制裝置4。 X降落傘單几3包括—個適於背負與固定在_降落體 '内月衣3 1、—個分別能夠被收藏在該收納背袋31内 :自該收納背袋31脫出並展開成一傘狀的傘主體％、一個 在X #衣3 1上並能相互接合與脫離以分別使該收納背 袋^收合與張開的開關組合體33，及多數條相間隔地連接 在4傘主體32周緣與該收納背袋31之間的伞繩％。 ,★其中’該開關組合體33具有一個設置在該背袋η上 、·第彳# 331、-個能與該第一扣件331相接合與相脫離 以/刀別使《納背袋31收合與張開的第二扣件说、一個 與該第二扣件332相連接且由磁性材質所製成的活動環塊 及個與忒第一扣件332反向地凸設在該活動環塊 333的限位柱334。 該控制裝置4包括一個連動該開關組合體33自相接合 的關閉狀態轉換為相脫離的開啟狀態的磁控單丨4 i、一個 控制该磁控單元41作動的控制單元42、-個與該控制單 一 電連接的中央處理單元43、分別與該中央處理單元. 43電連接以傳送資料至該中央處理單元43的—個加速旋轉 201036869 定向器44、一個全球衛星定位系統單元45、一個輸入單元 46、一個語音播放單元47及一個顯示器48。該加速旋轉定 向器44是用以量測該降落體下降過程中在相垂直的—前後 方向X、一水平方向γ及一直立方向z上的旋轉速度Rh、 RvY、RVz。其中，該直立方向z是與該降落體的下降方向相 平行。此外，在本實施例中，是以飛機跳傘為例說明該自 動安全啟動㈣傘2較时法與功效，且在該實施例中 ’ s亥降落體為一使用者100。 較佳地，該磁控單元41具有一個與該開關組合體33 的活動環塊333相間隔設置的中空管件411，及一纏繞在該 s件411 一外表面且與該控制單元42電連接的磁性線圈 412。該巾空官件411具有一個與該活動環塊⑶相對應設 置且是由磁性材質製成的環緣部413，—與該環緣部413相 連接的管體部414，及-貫穿該環緣部413與該管體部414 用以供該開關組合體33的限位柱334容置活動的通道415 要進行開傘時，是利用該控制單元42啟動該磁控單元41 藉由改變"IL通於s亥磁性線圈4 i 2的電力使該中空管件411 產生磁力並在該環緣部413形成一個吸引該活動環塊333 的磁吸力’使該活動環塊333受磁吸作用靠向該磁控單元 41位移’進而連動該第二扣件332自與該第一扣件如才目 接。的位置移動到與該第-扣件33 1相脫離的位置，藉此 使°玄傘主體32能自張開的背袋31脫出而完成開傘動作 〇 該°°曰播放單元47具有一個與該中央處理單元43電 201036869 連接的語音IC(integ瞻d eireuit，積體電路，_為ic)切 及個與該語音1C471電連接的喇。八472。在該實施例中 該自動安全降落傘2還包含—個適於穿戴在該使用者】⑻ 頭的頭蓋5，且該語音播放單元47的制。八472是設置在 該頭盔5内與該使用者1〇〇耳部相鄰近的位置。但不應以 此限制該，Λ 472的型式，該似472也可以設計為適於 配戴在該使用者100耳部的耳機型式。 當該使用者100利用該自動安全啟動降落傘2進行高 =傘運動時’可先搭乘一飛機101飛行到一預定高度的η 问二處停留，再自預定高度處跳離該飛機101，在落下過程 中，就能利用該控制裝置4感測外界條件並計算落下過程 各時間點的落地剩餘時間與合角速度，並和所設定的時間 下限值與速度上限值比對，以即時進行開傘，而能提供較 安全的保障. 參閱圖5、圖6與圖7，自跳傘的預備動作到安全著陸 ，使用該自動安全啟動降落傘2進行跳傘的詳細步驟可再 進一步說明如下： 0 步驟601是該使用者100在該預定高度的高空處，以 該輸入單元46輸入落地剩餘時間設定值△ τ，及合角速度 設定值R，並設定在落地剩餘時間Δτ，及合角速度r ==R時，立即啟動開傘。其中，配合與該中央處理單元43 電連接的顯示器48，讓該使用者1〇〇在進行輸入時，可清 楚地辨識所輸入的設定值，並能便於快.速完成輪入動作。 其中’在落下過程中’該中央處理單元43可以根據不 201036869 同夺門點4王球衛星定位系統單元45所接收到的座標訊號 計异落下逮度與加速度，進而能夠計算出該使用者100落 地剩餘時間’此外，該中央處理單元43還能根據該加速旋 轉定向器44所量測的該使用1100下降過程中在該前後、 水平、直立方向Χ、Υ、Ζ上的旋轉速度RVX、RVY、RVZ計 算出當時的合角速度ρ其中， Ο 〇 、步驟602為以該全球衛星m统單元45讀取起跳的 初始時間t。時的全球衛星定位座標（χο, Υ0,^。 步驟603是根據該初始時間t。時的全球衛星定位座標 (X: 4 Z。，t〇)定位初始位置高度，在本實施例巾，初始位 ^度為ZG ’並將該高度值及起跳時的該原始位置座標儲 存至該中央處理單元43。 步驟_是將該㈣傘單元3的收納f袋31背負至該 使用者100背部並固定好’使該自動安全啟動降落伞2與 ^使转1〇〇形成穩固連接的狀態，裝備確認並檢查完成 <接著，遺使用者100就能自該初始位置高度處跳離 飛機101。 A步驟605是在該使用者100落下過程中，該全球衛星 疋位系統單元45及該加速旋轉定向器44即日㈣測各個不 :時間點時的全球衛星定位座標（^，^，及該使用刮降 洛體）1〇〇在該前後、水平、直立方向χ、γ、ζ上的加速度 〜、aY、az ’及旋轉角速度Κνχ、、^。 步驟606是將該全球衛星定位系統單元45及該加速旋 轉定向器44所_到的數值傳送_中央處理單元43進 9 201036869 仃處理運算’並分別算出當時的落地前剩餘時間△t與合角 速度m 步驟607是該中央處理單元43將所計算出的落地剩餘 時間At值與合角速度r分別與步驟6〇1所輸入的設定值相 比較，以判斷是否要啟動開傘。若比較結果顯示當時的落 地剩餘時間△ t大於△ τ，則會再進行步驟6〇8，並將當時所 β十异出的合角速度Γ與步驟601所輪入的合角速度設定值R 相比較，若Γ也小於R，就再回到步驟605繼續量測不同時 間點的位置座標與旋轉角速度，及在步驟606計算落地前 剩餘時間△ t與合角速度Γ。例如，當該使用者⑽落下到 门X Ζ!時’ s玄中央處理單元43計算出的落地剩餘時間△卜 △ h A ti大於△ T，且合角速度Γι小於R，則該控制裝置4 將不啟動開傘，使該使用者1〇〇仍然背負該自動安全啟動 降洛傘2快速地向下落。當該使用者⑽落下到高度&時 右"玄中央處理單元43計算出的落地剩餘時間△ t= △ h， 且“小於等於步驟6〇1所設定的Δτ時，則進行步驟_ ’該中央處理單^ 43會立刻送出啟動指令至該控制單元42 ，再透過該控制單元42啟動該磁控單元41，以連動該第 二扣件332與該第-扣# 331相分離，並使該收納背袋η 的開口打開’使該傘主體32自該收納背袋31脫出及自動 張開成傘狀’進而完成開傘動作，這時就能藉由該伞主體 32展開後所增大的面積，配合空氣作用形成阻力，讓該使 用者100的下降速度減慢’及其下降姿勢獲得穩定，最炊 達到安全著地的目的。此外，若所算出的落地剩餘時間△二 10 201036869201036869 The back pockets are engageable and disengageable to connect the storage bag to the open switch assembly and the plurality of strips, respectively, to the parachute between the back pockets. The peripheral control device includes a magnetic control unit that interlocks the closed state of the switch assembly from the closed state of the switch assembly to the open state of the phase release. A control unit that controls the magnetron to operate 7L early, and is electrically connected to the control unit. a central processing unit, an acceleration rotary orienter electrically connected to the central processing unit to transmit the data to the central processing unit, a global satellite positioning (GPS) system unit, and an input unit 'the accelerated rotation orienter is used The rotation speed in the vertical direction - the front-rear direction, the horizontal direction, and the constant cubic direction during the falling of the falling body is measured. . The effect of knowing a cup is that the acceleration rotation director and the global satellite positioning system are connected to the central processing T element of the control device: the height change and the rotation situation during the falling of the drop body can be measured, Re-equipment: the remaining time of the landing time set by the input unit and the upper limit of the angular velocity of the falling body in the front, back, water and straight cube directions, : = The unit can be based on the received data and settings The value activates the (four) unit at a predetermined % point to actuate the magnetic control unit through the control unit, and the switch assembly is turned from the closed state to the open-type back pocket to be opened, so that the umbrella body can be scheduled. Secondly, the storage unit is pulled out and unfolded into an umbrella shape, so that the falling body can be changed and the rotation speed is changed, that is, the height is...immediately open, and the stability of the use is relatively better. And advantages. - 5 201036869 [Embodiment] The foregoing and other technical features, features and advantages of the present invention will be apparent from the detailed description of the preferred embodiments. > Read Fig. 3®4 and Fig. 5' The automatic safe start parachute 2 本 of the present invention contains the parachute unit 3, and the rib starts the control device 4 of the parachute early 3 open umbrella. The X parachute single 3 includes a suit which is suitable for carrying and fixing in the falling body, and can be stored in the storage bag 31 respectively: it is released from the storage bag 31 and expanded into an umbrella. The umbrella main body %, one switch body 33 which can be engaged and disengaged on the X #衣 3 1 to respectively fold and retract the storage back pocket, and the plurality of strips are connected to each other at 4 umbrella bodies 32% of the rope between the circumference and the storage bag 31. , wherein the switch assembly 33 has one disposed on the back pocket η, and the third member 331 can be engaged with the first fastener member 331 and disengaged from the knife to make the "back bag 31" The folded and unfolded second fasteners are said, and a movable ring block connected to the second fastening member 332 and made of a magnetic material is protruded in the opposite direction from the first fastening member 332. A limit post 334 of the ring block 333. The control device 4 includes a magnetron unit 4i that interlocks the closed state of the switch assembly 33 from the engaged state to the disengaged open state, a control unit 42 that controls the operation of the magnetron unit 41, and a control unit A central processing unit 43 for controlling a single electrical connection, an acceleration rotation 201036869 that is electrically connected to the central processing unit 43 to transmit data to the central processing unit 43, an orientation unit 44, a global satellite positioning system unit 45, and an input unit 46. A voice playback unit 47 and a display 48. The acceleration rotary director 44 is for measuring the rotational speeds Rh, RvY, and RVz in the vertical direction - the front-back direction X, the horizontal direction γ, and the upright direction z during the falling of the falling body. Wherein, the upright direction z is parallel to the descending direction of the falling body. In addition, in the present embodiment, the automatic safe start (four) umbrella 2 time method and effect are described by taking an airplane skydiving as an example, and in this embodiment, the s hai landing body is a user 100. Preferably, the magnetron unit 41 has a hollow tube member 411 spaced apart from the movable ring block 333 of the switch assembly 33, and an outer surface of the s member 411 and electrically connected to the control unit 42. Magnetic coil 412. The towel 411 has a rim portion 413 disposed corresponding to the movable ring block (3) and made of a magnetic material, a body portion 414 connected to the rim portion 413, and a through-loop When the edge portion 413 and the tube body portion 414 are used for the opening portion 334 of the switch assembly 33 to accommodate the movable passage 415 for opening the umbrella, the control unit 42 is used to activate the magnetic control unit 41 by changing the " The power of the IL magnetic coil 4 i 2 causes the hollow tubular member 411 to generate a magnetic force and forms a magnetic attraction force attracting the movable ring block 333 at the rim portion 413 to cause the movable ring block 333 to be magnetically attracted. Displacement to the magnetic control unit 41 to further interlock the second fastener 332 from the first fastener. The position is moved to a position disengaged from the first fastening member 33 1 , whereby the parabolic umbrella main body 32 can be disengaged from the opened back pocket 31 to complete the opening operation, and the playback unit 47 has a The voice IC (integret, e, ic) connected to the central processing unit 43 is connected to the voice 1C471. Eight 472. In this embodiment, the automatic safety parachute 2 further includes a head cover 5 adapted to be worn on the user's (8) head, and the voice playback unit 47 is manufactured. Eight 472 is disposed in the helmet 5 at a position adjacent to the user's ear. However, the type of Λ 472 should not be limited thereby, and the 472 can also be designed to fit the earphone type of the user's 100 ear. When the user 100 uses the automatic safe start of the parachute 2 to perform high=umbrella movement, 'the aircraft 101 can be first taken to a predetermined height of the η request two stop, and then the aircraft 101 is jumped from the predetermined height, and is dropped. During the process, the control device 4 can be used to sense the external conditions and calculate the remaining time and the combined angle of the landing time at each time point, and compare with the set time lower limit value and the speed upper limit value to instantly open Umbrella, but can provide a more secure protection. Referring to Figure 5, Figure 6 and Figure 7, from the preparatory action of the skydiving to the safe landing, the detailed steps of using the automatic safe start of the parachute 2 for skydiving can be further explained as follows: 0 Step 601 When the user 100 is at the height of the predetermined height, the input unit 46 inputs the landing residual time set value Δ τ and the combined angular velocity set value R, and sets the remaining time Δτ and the combined angular velocity r==R. , immediately start the umbrella. The display 48 electrically connected to the central processing unit 43 allows the user 1 to clearly recognize the input set value when inputting, and to facilitate the fast-speed completion of the round-in operation. The central processing unit 43 can calculate the user's 100 according to the coordinate signal received by the camera signal system unit 45 that is not in the 201036869 and the king ball satellite positioning system unit 45. The remaining time of landing 'In addition, the central processing unit 43 can also measure the rotational speeds RVX, RVY in the front, rear, horizontal, and upright directions Χ, Υ, Ζ during the use of the 1100 descent measured according to the accelerated rotary orienter 44. RVZ calculates the combined angular velocity ρ at that time, Ο 〇, step 602 is to read the initial time t of the start of the jump with the global satellite unit 45. Global satellite positioning coordinates (χο, Υ0, ^. Step 603 is to locate the initial position height according to the global satellite positioning coordinates (X: 4 Z., t〇) at the initial time t. In this embodiment, the initial The position is ZG′ and the height value and the original position coordinate at the time of the jump are stored to the central processing unit 43. Step _ is to carry the storage bag f of the (4) umbrella unit 3 to the back of the user 100 and fix it It is good to make the automatic safe start of the parachute 2 and ^ to make a stable connection state, the equipment confirmation and the inspection is completed. Then, the user 100 can jump off the aircraft 101 from the initial position height. 605 is a global satellite positioning coordinate (^, ^, and the use of the wiper drop) when the user 100 is in the process of dropping the global satellite clamp system unit 45 and the acceleration rotary orienter 44 Loose acceleration of 〇〇, aY, az ' and rotational angular velocity Κνχ, ^ in the front, back, horizontal, upright directions χ, γ, ζ. Step 606 is the global satellite positioning system unit 45 and the acceleration Rotary director 44 _ The numerical value transmission _ central processing unit 43 proceeds to 9 201036869 仃 processing operation 'and calculates the current remaining time before landing Δt and the combined angular velocity m respectively. Step 607 is that the central processing unit 43 combines the calculated remaining time At value of landing time. The angular velocity r is compared with the set value input in step 6〇1 to determine whether to open the umbrella. If the comparison result shows that the remaining landing time Δt is greater than Δτ, then step 6〇8 will be performed, and At that time, the combined angular velocity β of the β-derivative is compared with the combined angular velocity R of the step 601. If the Γ is also smaller than R, the process returns to step 605 to continue measuring the position coordinates and the rotational angular velocity at different time points. And calculating the remaining time Δt and the angle of intersection Γ before landing. In step 606, for example, when the user (10) drops to the door X Ζ!, the remaining time Δ Δ h A ti calculated by the sth central processing unit 43 is greater than ΔT, and the angular velocity Γι is less than R, the control device 4 will not activate the opening of the umbrella, so that the user 1〇〇 still bears the automatic safety start to lower the falling umbrella 2 quickly. (10) Falling to the height & right right " Xuan central processing unit 43 calculates the remaining landing time Δ t = Δ h, and "less than or equal to Δτ set in step 6〇1, then proceed to step _ 'the central processing order ^ 43 will immediately send a start command to the control unit 42, and then activate the magnetic control unit 41 through the control unit 42 to interlock the second fastener 332 with the first buckle 331, and the storage bag The opening of η is opened to "open the umbrella body 32 from the storage bag 31 and automatically open into an umbrella shape" to complete the opening operation. At this time, the enlarged area of the umbrella body 32 can be combined with the air effect. The resistance is formed, the user's 100's descending speed is slowed down, and the falling posture is stabilized, and finally the goal of safe landing is achieved. In addition, if the calculated remaining time of landing △ 2 10 201036869
二且△ η大於△ τ時，則會進行步驟6〇8，並將當時所 汁^出的合角速度r與步驟001的R相比，若！·大於等於R 人則進#步驟該中央處理單元Μ同樣會送出啟動指 7到該控制單I 42，進而啟動開傘動作，達到安全著地的 目的。When Δ η is larger than Δ τ, step 6 〇 8 is performed, and the angle r of the juice at the time is compared with the R of step 001, if! · If the R is greater than or equal to the number of steps, the central processing unit will send the start finger 7 to the control unit I 42, and then start the opening operation to achieve the purpose of safe landing.
^值得說明的是，當該中央處理單元43判斷結果是要進 仃開：並送出啟動指令時’可同時啟動該語音播放單元〇 的叩曰IC471 ’再利用該語音IC471啟動該喇叭472播放聲 音及進行著地前倒數計時，由於該伽、472是設置在該使 用者10G所戴的頊& 5内鄰近其耳部的位置，藉此，該使 用者10G %預先清楚地獲知著地前的剩餘時間，以預作心 理準備’而能更穩定地完成著地動作。 在該較佳實施例中，雖然是以飛機跳傘說明該自動安 全啟動降洛傘2的使用方式，但不應以限制該降落傘2的 用途謂洛傘2也能供高山跳傘等其他_的跳傘運動 使用，或者也能用作救生傘、投物傘、飛機阻力傘、航彈 傘、傘兵傘和回收傘等，都能藉由與該降落傘單元3相連 接的控制裝置4’配合開始時所輸入的限制條件，及落下過 程中所接收到的各項資料進行運算與判斷，進而在適當時 機自動啟動開傘動作’讓與該降落傘2相連接的人或好 夠安全且無損傷地著陸。 b 歸納上述，本發明自動安全啟動降落伞2，可獲致下述 的功效及優點，故能達到本發明的目的： ^ - '藉由與該控制裝置4之中央處理單元Ο相連接的 11 201036869 加速旋轉定向器44與全球衛星定位系統單元45，能夠在兮 使用者（降落體）100下降過程中即時量測其高度、位置變化 與旋轉情形，再配合以該輸入單元46所設定的落地剩餘時 間與該降落體在前後、水平及直立方向χ、γ、ζ上的旋轉 速度RVx、RVY、RVz之合角速度的上限值，使該中央處理單 元43能客觀地根據所接收的資料與所設定的限制條件在預 定的時間點啟動該控制單元42，以透過該控制單元42使爷 磁控單元41作動，並帶動該第二扣件332脫離該第一扣件 Ml，進而使該收納背袋31被打開，便於該傘主體32能即 時地自該收納背袋31脫出並展開成傘狀’讓該降落體2可 安全而穩定地著陸，藉此，能減少人為誤判造成開伞時機 不佳而引發意外的危險，且即使該使用者1〇〇在落下過程 中發生身體不適或意識昏迷等情形時，仍能透過該控制震 置4進行判斷以在著地前的適當時機啟動開伞，讓該使用 =100仍能安全抵達地面，使本發明具有能輔助提升使用 時的穩定性與安全性的特性與優點。 相較以手動方式拉動一拉繩14(見圖1)的現有開傘 式與結構，本發明利用該磁控單元41連動該第二扣件 繩第一扣件331達到開伞的效果，能有效避免因拉 处透μ、他配件纏繞導致無法順利開傘的情形發生，除了 :由；=制裝置4量測與計算較佳的開傘時機外，還能 藉由该磁控單开& 傘動作- 該第二扣件332的結構設計，使開 全性相對較高的優點。 〃有便用上女 12 201036869 冑”圖4 ’值得-提的是，除了能湘該控制裝 置自動執行開傘動作外，該自動安全啟動降落伞2還包It is worth noting that when the central processing unit 43 determines that the result is to be opened: and sends a start command, 'the IC 471 of the voice playback unit can be activated at the same time'. The voice IC 471 is used to activate the speaker 472 to play the sound. And performing the ground countdown, since the gamma and 472 are disposed in the 顼& 5 worn by the user 10G adjacent to the ear, whereby the user 10G% knows the ground in advance The remaining time, in preparation for psychological preparation, can complete the ground movement more stably. In the preferred embodiment, although the automatic safe start of the use of the parachute 2 is described by means of an airplane parachute, the use of the parachute 2 should not be restricted. The Umbrella 2 can also be used for parachuting such as alpine skydiving. Used for sports, or can also be used as a life umbrella, a parachute umbrella, an aircraft resistance umbrella, a parachute umbrella, a paratrooper umbrella, a recycling umbrella, etc., which can be matched by the control device 4' connected to the parachute unit 3 at the beginning. The input restriction conditions and the data received during the drop process are calculated and judged, and the opening operation is automatically started at an appropriate timing to allow the person connected to the parachute 2 to land safely and without damage. b In summary, the present invention automatically and safely activates the parachute 2, which achieves the following efficiencies and advantages, so that the object of the invention can be achieved: ^ - 'Accelerated by 11 201036869 connected to the central processing unit of the control device 4 The rotary orienter 44 and the global satellite positioning system unit 45 can instantly measure the height, position change and rotation of the user (drop body) 100 during the descending process, and cooperate with the remaining time set by the input unit 46. The upper limit value of the angular velocity of the rotational speeds RVx, RVY, and RVz of the descending body in the front, rear, horizontal, and vertical directions χ, γ, and ,, so that the central processing unit 43 can objectively set the data according to the received data. The control unit 42 is activated by the control unit 42 to activate the second magnet 332, and the second fastener 332 is disengaged from the first fastener M1, thereby making the storage bag 31 is opened, so that the umbrella main body 32 can be immediately released from the storage back pocket 31 and unfolded into an umbrella shape, so that the landing body 2 can be safely and stably landed, thereby reducing artificial Judging the risk of accidents caused by poor timing of opening the umbrella, and even if the user is in a situation of physical discomfort or coma during the fall, the control can be judged by the shock 4 to be in front of the ground. The appropriate time to start the opening of the umbrella, so that the use of =100 can still safely reach the ground, so that the present invention has the characteristics and advantages that can help improve the stability and safety in use. Compared with the existing open umbrella type and structure for manually pulling a pull cord 14 (see FIG. 1), the present invention utilizes the magnetic control unit 41 to interlock the second fastener rope first fastener 331 to achieve the effect of opening the umbrella. Effectively avoid the situation that the umbrella can not be opened smoothly due to the penetration of μ, and the winding of his accessories, except: by: = device 4 measuring and calculating the better opening time, can also be opened by the magnetic control Umbrella action - The structural design of the second fastener 332 gives the advantage of relatively high opening. 〃 用 用 12 12 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010 2010
含:個與該«組切33相連接用於執行手划傘的手控 單兀6 ’該手控單元6包括—條穿設於該中空管件411的通 k化且與該開關組合體33的限位柱334相連接的拉繩。 及固接在該拉繩61 -末端的拉環62，當不透過該控制 執行自動開傘時，該使用者_仍可藉由拉動該拉 由該拉繩61直接牵引該限位柱334與該活動環塊 移進而連動該第二扣件332脫離該第一扣件如， 藉此，同樣能完成開傘動作。 处、准以上所述者’僅為本發明之較佳實施例而已，當不 :、此限疋本發明實施之範圍’即大凡依本發明申請專利 ^ 發月"兒明内容所作之簡單的等效變化與修飾，皆仍 屬本發明專利涵蓋之範圍内。 【圖式簡單說明】 1 nV γ-— 不思圖，說明現有的一降落傘； 圖 2 是—-^ —不％、圖，說明一使用者背負已開啟的該降落 傘往下降的情形； 圖 3 是·— 一九 ^ — 不思圖，說明本發明自動安全啟動降落傘— 車乂仏實施例的-開關組合體呈關閉狀態的情形； 圖4疋—不意圖，說明該較佳實施例的開關組合體呈 開啟狀態的情形. 圖5是—一在/阳 不意圖’說明一使用者使用該實施例進行飛 機跳傘的情形； 13 201036869 圖6是一方塊圖，說明該較佳實施例的一降落傘單元 的開關組合體受一控制裝置連動的情形；及 圖7是一流程圖，說明該較佳實施例的一接收處理模 組接收及處理各項參數資料的情形。And comprising: a manual control unit 6 for connecting the group of cuts 33 for performing a hand-drawn umbrella; the manual control unit 6 includes a through-knitted through the hollow tubular member 411 and associated with the switch assembly 33 The limit post 334 is connected to the drawstring. And a pull ring 62 fixed to the end of the pull cord 61. When the automatic opening of the umbrella is not performed through the control, the user can still directly pull the limit post 334 by the pull cord 61 by pulling the pull. The movable ring block moves to interlock the second fastener 332 from the first fastener, for example, thereby completing the opening operation. The above description is only for the preferred embodiment of the present invention, and if not, the scope of the present invention is limited to that of the present invention. Equivalent variations and modifications are still within the scope of the invention. [Simple description of the diagram] 1 nV γ-- does not think about the existing parachute; Figure 2 is --- ^ - not %, the figure shows a user carrying the opened parachute down; Figure 3 Yes - - 九 ^ - I don't think about the situation, the automatic safe start of the parachute of the present invention - the shackle embodiment - the switch assembly is in a closed state; Figure 4 - not intended to illustrate the switch of the preferred embodiment FIG. 5 is a diagram showing a case where a user uses the embodiment to perform skydiving; 13 201036869 FIG. 6 is a block diagram illustrating a preferred embodiment of the present invention. The switch assembly of the parachute unit is interlocked by a control device; and FIG. 7 is a flow chart illustrating the case where a receiving processing module of the preferred embodiment receives and processes various parameter data.
14 20103686914 201036869
【主要元件符號說明】 2 ..........降落傘 3 ..........降落傘單元 31 .........收納背袋 32 .........傘主體 33 .........開關組合體 331 .......第一扣件 332 .......第二扣件 333 .......活動環塊 334 .......限位柱 34 .........傘繩 4 ..........控制裝置 41.........磁控單元 411 .......中空管件 412 .......磁性線圈 413 .......環緣部 414……管體部 415.......通道 42 .........控制單元 43 .........中央處理單元 44 .........加速旋轉定向器 45 .........全球衛星定位 系統單元 46 .........輸入單元 47 .........語音播放單元[Main component symbol description] 2 ..........Parachute 3 ..........Parachute unit 31 .... Storage bag 32 ..... .... umbrella body 33 .... switch assembly 331 .... first fastener 332 .... second fastener 333 ... Activity ring block 334 .... limit column 34 ... ... umbrella rope 4 ..... control device 41 ......... Magnetic control unit 411 . . . hollow tube 412 . . . magnetic coil 413 . . . rim portion 414 ... tube body portion 415....... channel 42 .........control unit 43 .... central processing unit 44 ... ... acceleration rotary orienter 45 ... ... global satellite Positioning system unit 46 .... input unit 47 ......... voice playback unit
471 .......語音1C 472 .......°刺〇八 48 .........顯示器 5 ..........頭盔 6 ..........手控單元 61 .........拉繩 62 .........拉環 100 .......使用者 101 .......飛機 15471 .......Voice 1C 472 .......° Hedgehog Eight 48 ......... Display 5 .......... Helmet 6 .... ... manual control unit 61 ......... pull cord 62 ... ... pull ring 100 ... ... user 101 ... .Aircraft 15