201141757 六、發明說明： 【發明所屬之技術領域】 本發明係關於一種運輪梦署，姑g 置 雜聚置，特別是—種節能的運輸裝 【先前技術】 因為石油即職竭，有效替代能源又尚未發現 持人類的文明，勢必開發不使用石油作為燃料的交通工具維201141757 VI. Description of the invention: [Technical field to which the invention pertains] The present invention relates to a transportation dream system, which is a kind of energy-saving transportation device. [Prior Art] Because oil is exhausted, an effective alternative Energy has yet to discover a civilization that holds humanity, and it is bound to develop a vehicle that does not use oil as a fuel.
飛艇_絲源幾乎不會_石油，所軸對於現 能性能較好’而且對於環境的破壞也較小。圖 飞為傳、桃艇刚的結構。傳統飛艇刚，例如著名的齊 ，艇设卯㈣，具有環形銘合金骨架11〇和以布料或皮革覆 ^架110而形成的機殼120。在機殼12〇时一些獨立的 j 130及輔助氣囊(未圖示）。在飛行中，輔助氣囊可通過 充氣或放氣來㈣浮力。有多鮮板式尾鰭14㈣於操縱和 保持穩定。兩台發動機(未圖示)懸掛在機殼⑶下面，通過 長驅動軸(未圖示)來驅動安裝在機殼12G兩側的螺旋樂15〇。 另外還有-個客臉160雜在機殼12G下面，以供載客之用。 般而5，队艇充氣一次即可長久使用。氣室bo提供 的浮力使得飛艇前進所需能量降至最低。因為不需額外能量 保持飛艇的升空，且飛行可以進行最短直線移動，節省許多 時間。 ° 然而，因為傳統的飛艇100是以布或皮革材質的機殼12〇 包覆於充填氫氣的氣室130之外侧，而產生安全上的疑慮。 例如興登保號飛船在啟航的第二年，1937年5月6日，在美 國紐澤西洲的Lakehurst Naval Air Station著陸前，因船長的n 3 201141757 操作失誤，導致氣室13G中支撐鋼索_、彈“擊破_ :導致魏_，加上當時訂的靜電職轉 ㈣祕封散花，而進—步·外域氣，產 、因此’若能改良舰結_改善安全上關題，飛艇 以成為環保、安全又有鱗的大眾運輸工具。 【發明内容】 裝置本發明之目的在於提供—種雜、安全又梭率的運輸 點可以從本發明所揭露的技術特 本發明的其他目的和優 徵中得到進一步的了解。 為達上述之-或部份或全部目的或是其他目的，本發明 之一實施例為一種戰裳S。雜灯包括-氣囊、一支^、 一動力機構及-搶體。支架位於氣囊之下方，並且與氣囊相 連，。動力機構連接於支架上。艙體位於支架之下方，並且 口定於支架上，用以容納—承载物。搶體包括—重量調節機 ，’以調節雜、承載物、氣囊及絲之總重力等於氣囊所 供的冷*力。 ^氣囊的位置在地面上丨_公尺以内時，氣囊的大小ν 係以算f V=k*N估計’其中k為介於0.909134至0.982014 門的#數’而N為該運輸裝置及該承載物之總重。 艙體包括一外箱體、一内腔體以及外箱體所容納之一液 ，，内腔體位於外箱體之内部，並懸浮於液體上，而承載物 合納於内腔體之内部，外箱體包括—出水口及一入水口。動 201141757 力機構例如是裝設於支架之二相對側的人造翅膀、螺旋槳、 或是纜繩。 在一實施例中，上述運輸裝置適合行駛於二高架結構體 之間’其中動力機構包括二纜繩及二動力源，每一動力源分 別設置於每一高架結構體上，每一纜繩連接於每一動力源與 支架之間。運輸裝置更包括二安全索，其中每一安全索連接 於二咼架結構體之間。艙體之底部具有二支撐件，二支撐件 分別連接於不同的二安全索，並可於二安全索上滑動。 • 本發明的運輸裝置利用重量調節機構來以調節艙體、承 載物及支架之總重力等於氣囊所提供的浮力，使得運輸裝置 前進所需能量降至最低，提供另一種不同於傳統飛艇的節省 機制。 【實施方式】 有關本發明之前述及其他技術内容、特點與功效，在以 下配合參考圖式之一實施例的詳細說明中，將可清楚的呈 現。以下實施例中所提到的方向用語，例如：上、下、左、 右、前或後等，僅是參考附加圖式的方向。因此，使用的方 向用語是用來說明並非用來限制本發明。 圖2為一種可以替代傳統飛艇的運輸裴置。此運輸裝置 包括一氣囊210、一支架220、一動力機構230及一舰 24〇。支架22〇位於氣囊210之下方，並且與氣囊別相連接， 以支標氣囊210及搶體24G。動力機構23G連接於支架上， 用以提供運輸裝置200於水平方向前進的動力。雜24〇位 於支架220之下方，並且固定於支架22〇上，用以容納人員 或物貧等承載物250。臉體240包括一重量調節機構如，& 5 201141757 調節艙體240、承載物250、氣囊210及支架220之總重力， 使其與氣囊210所提供的浮力在垂直方向上力平衡。 在氣囊210設計方面，氣囊21〇採用比空氣輕的氣體充 填，例如氫、氦等氣體，氣囊21〇的材質以堅韌、不透氣、 質輕、防水、耐用為佳。 依浮力公式’在1大氣壓、25ΐ、地面上1〇〇〇公尺以内， 氣囊210大小的計算如下： 一、 充填氫氣的氣囊大小VH2=〇 9〇9134*N， 二、 充填氦氣的氣囊大小VHe=〇.982014*N， 上式中，N為運輸裝置及其承載物之總重(單位：公斤) VH2及VHe之單位皆為m3。 氣囊210宜以多個小氣囊組成，避免單-氣囊破裂導致 所有氣體漏光的情形。 氣囊210的充氣有二種方式：第-種為在地面設置充氣 站(，圖示)以進行充氣，行進間不充氣，此方式適合氫氣與 氦氣；第二種為配備充氣設備(未圖示)於艙體24〇中，行進 間可以補充氣囊210之氣體。 上述第二種方式的絲設備有二種，—種為鋼瓶，内含 已製備的氫氣&氦氣；另-種為轉製氫設備，只適合氮氣 種類。 在艙體240設計方面，艙體24〇包括一外箱體2料、一 内腔體246以及外箱體所容納之一液體24s。内腔體246位 於外箱體244之内部’並懸浮於液體245上。而承載物25〇 容納於内腔體246之内部。艙體24〇的重量調節機構242設 201141757 於外箱體244上，係包括一出水口 243及一入水口 24卜通 過出水口 243及入水口 241調整液體245的量，使氣囊21〇、 支架220、外箱體244、内腔體246、液體245及承载物25〇 之總重等於氣囊210所提供的總浮力。 如圖2所示’艙體240與氣囊210之間具有一支架22〇， 此支架220係為支撐艙體240的主要結構。 在動力機構230的設計方面，大致可分成三類： 1) .人造翅膀231 :仿鳥類之雙翅裝設在支架22〇之兩相 對側’可收摺或展開，如圖3所示。 2) .螺旋槳232 :如圖4所示，二螺旋槳232分別裝設於 支架220之二相對侧。螺旋槳232可利用人力踩踏驅動、使 用汽油的引擎或使用電力的馬達來驅動。 3) .纜繩233 :如圖5所示，上述運輸裝置2〇〇適合行駛 於二高架結構體501、502之間，其中動力機構23〇包括纜繩 233及動力源234’動力源234例如是馬達與滑輪組之組合。 母一尚架結構體501或502皆設置一組馬達與滑輪組，每一 馬達係提供動力給位於同一高架結構體上的滑輪組。每一纜 繩233連接於動力源234與支架220之間。 除此之外，運輸裝置200更包括二安全索26卜262，其 中每一安全索261或262連接於二高架結構體5〇1、5〇2之 間。艙體240之底部具有二支撐件247、248，二支撐件247、 248分別連接於不同的二安全索261 ' 262，並可於二安全索 26卜262上滑動。 因為圖5所示的動力機構230是利用牽引力，故艙體24〇 201141757 及氣囊210的重量可被大幅的減少。此種運輸裝置2〇〇的兩 條安全索261、262被設置在二高架結構體5〇1、5〇2之間， 用以引導本運輸裝置200，以避免因天候不佳而導致失控。 由於運輸裝置200與承載物250的總重量與氣囊21〇提供的 空氣浮力形成垂直方向的力平衡，依牛頓定律，此種運輸裝 置200的能量損失將可以很小。 為了調節艙體240内的液體245量，可設置儲水槽、水 菜等裝置於每-高架結構體5〇1、502或地面上。運輸裝置 200停留於地面或高架結構體5〇1、5〇2時，儲水槽中的液體 245可通過入水口 241注入艙體測中，相反地，搶體24〇 中的液體245也可以通過出水口 243排至儲水槽中，以達到 調節液體量的目的。附帶一提的是，在入水口 241可設置一 洋球249 ’當水位上升至入水口 241處時，浮球249即可將 入水口 241堵住，以控制液面高度。 以上幾種動力機構230皆可用於可承载丨〜2人的小型運 輸裝置、可承载4〜1G人的中型運輸裝置或可承載3()人以上 的大型運輸裝置。 t H 置較強調其機動性，故其__2 較適。私用人造翅膀或螺旋紫232。而中型運 大型運輸裝置考慮降低《，減錢囊210的大小等因素 並且通常絲進行狀輯無_大 覺 233或風帆等動力機構為佳。 故使· 因為浮力與運輸裝置2〇〇能達到力平衡，理論上，此 =Γ::停留在空間的任何位置，術置的 升、下降或轉f皆視所使用的動力機構23〇 201141757 定，並且可加農方向艇或不裝。 、以3本裝置200時’應配合氣象資料，例如注意風 、、=…空運輸時’適當的高度應在地面上1000公尺 公’娜侧綱大，例如位 吩，將變成位於地面時的2.9倍大，有撐破危 險。 飛行===褒置200後’道路結構變得不需要、The airship _ silk source is almost no _ petroleum, the shaft has better performance for the current performance, and the damage to the environment is also small. Figure fly for the transmission, the structure of the Tao boat. Conventional airships, such as the well-known Qi, the boat set (4), have a ring-shaped alloy skeleton 11〇 and a casing 120 formed by a cloth or leather cover 110. There are separate j 130 and auxiliary airbags (not shown) when the casing 12 is closed. In flight, the auxiliary airbag can be buoyed by inflation or deflation. There are many fresh plate tail fins 14 (four) that are manipulated and stable. Two engines (not shown) are suspended below the casing (3), and a long drive shaft (not shown) is used to drive the screw 15 安装 mounted on both sides of the casing 12G. In addition, there is a guest face 160 mixed under the chassis 12G for passengers. As usual, the team boat can be used for a long time. The buoyancy provided by the chamber bo minimizes the energy required to advance the airship. Because no extra energy is required to keep the airship off, and the flight can be moved in the shortest straight line, saving a lot of time. ° However, since the conventional airship 100 is covered on the outer side of the hydrogen-filled air chamber 130 by a cloth or leather case 12, a safety concern arises. For example, in the second year of the sailing of the Xingdengbao spacecraft, on May 6, 1937, before the landing at Lakehurst Naval Air Station in New Jersey, USA, due to the operation error of the captain's n 3 201141757, the supporting cable in the air chamber 13G was caused. _, the bomb "breaking _: lead to Wei _, plus the electrostatic service (4) secret seals at that time, and advance - step outside the field gas, production, therefore 'if you can improve the knot _ improve safety, airship In order to be an environmentally friendly, safe and scaly mass transit vehicle. SUMMARY OF THE INVENTION The present invention is directed to providing a transport point that is heterogeneous, safe, and convenient. Other objects of the present invention can be derived from the techniques disclosed herein. Further understanding is provided in the preferred embodiment. In order to achieve the above-mentioned or some or all of the objectives or other purposes, an embodiment of the present invention is a battle skirt S. The lamp includes an airbag, a harness, a power mechanism and - The body is located below the airbag and is connected to the airbag. The power mechanism is connected to the bracket. The cabin is located below the bracket, and the mouth is fixed on the bracket to accommodate the carrier. The grabbing body includes - weight adjustment Machine, 'to adjust the total gravity of the miscellaneous, carrier, airbag and wire is equal to the cold* force provided by the airbag. ^When the position of the airbag is within _meter of the ground, the size of the airbag is calculated as f V=k *N estimates 'where k is the #number between 0.909134 and 0.982014 doors and N is the total weight of the transport unit and the load. The pod includes an outer box, an inner chamber and the outer box a liquid, the inner cavity is located inside the outer casing and suspended on the liquid, and the carrier is integrated inside the inner cavity, and the outer casing includes a water outlet and a water inlet. The movement mechanism 201141757 is for example An artificial wing, a propeller, or a cable mounted on the opposite side of the bracket. In an embodiment, the transport device is adapted to travel between two elevated structures, wherein the power mechanism includes two cables and two power sources, each A power source is respectively disposed on each of the elevated structures, and each cable is connected between each power source and the bracket. The transport device further includes two safety cables, wherein each safety cable is connected between the two truss structures. The bottom of the body has two support members. The support members are respectively connected to different two safety cables and are slidable on the two safety cables. The transport device of the present invention utilizes a weight adjustment mechanism to adjust the total gravity of the cabin, the carrier and the bracket to be equal to the buoyancy provided by the airbag. The energy required to advance the transport device is minimized, and another saving mechanism different from the conventional airship is provided. [Embodiment] The foregoing and other technical contents, features and effects of the present invention are hereinafter described in conjunction with an embodiment of the reference drawings. The detailed description will be clearly presented. The directional terms mentioned in the following embodiments, such as: up, down, left, right, front or back, etc., are only directions referring to the additional schema. Therefore, the use of The directional terminology is used to illustrate that it is not intended to limit the invention. Figure 2 is a transport device that can replace a conventional airship. The transport device includes an air bag 210, a bracket 220, a power mechanism 230, and a ship. The bracket 22 is located below the airbag 210 and is connected to the airbag to support the airbag 210 and the grabbing body 24G. The power mechanism 23G is coupled to the bracket to provide power for the transport device 200 to advance in a horizontal direction. The miscellaneous 24 is located below the bracket 220 and is fixed to the bracket 22 to accommodate a load 250 such as a person or a poor person. The face 240 includes a weight adjustment mechanism such as & 5 201141757 to adjust the total weight of the cabin 240, the carrier 250, the airbag 210, and the bracket 220 such that it is in a vertical balance with the buoyancy provided by the airbag 210. In the design of the airbag 210, the airbag 21 is filled with a gas lighter than air, such as hydrogen, helium, etc., and the material of the airbag 21 is preferably tough, airtight, lightweight, waterproof, and durable. According to the buoyancy formula 'at 1 atm, 25 ΐ, 1 metre above the ground, the size of the airbag 210 is calculated as follows: 1. The size of the airbag filled with hydrogen VH2=〇9〇9134*N, 2. The airbag filled with helium Size VHe=〇.982014*N, In the above formula, N is the total weight of the transport device and its load (unit: kg). The units of VH2 and VHe are both m3. The air bag 210 is preferably composed of a plurality of small air cells to avoid a situation in which a single-balloon rupture causes all gases to leak light. There are two ways to inflate the airbag 210: the first type is to set up an inflating station (shown) on the ground for inflation, the air is not inflated during the travel, which is suitable for hydrogen and helium; the second is equipped with an inflatable device (not shown) Shown in the cabin 24, the air between the airbags 210 can be replenished during the travel. There are two kinds of wire devices of the above second mode, namely, a steel cylinder containing the prepared hydrogen & helium gas; and the other type is a hydrogen conversion device, which is only suitable for the nitrogen type. In terms of the design of the cabin 240, the cabin 24 includes an outer casing 2, an inner cavity 246, and a liquid 24s contained in the outer casing. The inner cavity 246 is located inside the outer casing 244 and suspended on the liquid 245. The carrier 25 is housed inside the inner cavity 246. The weight adjustment mechanism 242 of the cabin 24 设 is set on the outer casing 244, which includes a water outlet 243 and a water inlet 24, and the amount of the liquid 245 is adjusted through the water outlet 243 and the water inlet 241 to make the airbag 21 and the bracket. 220. The total weight of the outer casing 244, the inner cavity 246, the liquid 245, and the carrier 25〇 is equal to the total buoyancy provided by the airbag 210. As shown in Fig. 2, there is a bracket 22A between the cabin 240 and the airbag 210, which is the main structure for supporting the cabin 240. In the design of the power mechanism 230, it can be roughly divided into three categories: 1) Artificial wings 231: The double wings of the imitation birds are mounted on the opposite sides of the bracket 22' to be folded or unfolded, as shown in FIG. 2) Propeller 232: As shown in Fig. 4, the two propellers 232 are respectively disposed on opposite sides of the bracket 220. The propeller 232 can be driven by a human pedaling drive, an engine using gasoline, or a motor using electric power. 3) Cable 233: As shown in FIG. 5, the transport device 2 is adapted to travel between two elevated structures 501, 502, wherein the power mechanism 23 includes a cable 233 and a power source 234'. The power source 234 is, for example, a motor. Combined with the pulley block. Each of the mother-and-shoulder structures 501 or 502 is provided with a set of motors and pulley blocks, each of which provides power to a pulley block located on the same elevated structure. Each cable 233 is coupled between the power source 234 and the bracket 220. In addition to this, the transport device 200 further includes two safety cables 26 262, each of which is connected between the two elevated structures 5〇1, 5〇2. The bottom of the cabin 240 has two support members 247, 248. The two support members 247, 248 are respectively connected to different second safety cables 261 ' 262 and are slidable on the two safety cables 26 262. Since the power mechanism 230 shown in FIG. 5 utilizes traction, the weight of the cabin 24〇 201141757 and the airbag 210 can be greatly reduced. Two safety cables 261, 262 of such a transport device 2 are disposed between the two elevated structures 5, 1, 5, 2 to guide the transport device 200 to avoid loss of control due to poor weather. Since the total weight of the transport unit 200 and the carrier 250 and the air buoyancy provided by the air bag 21〇 form a vertical force balance, according to Newton's law, the energy loss of such a transport device 200 can be small. In order to adjust the amount of liquid 245 in the tank 240, a water tank, a water dish, or the like may be provided on each of the elevated structures 5, 1, 502 or the ground. When the transport device 200 stays on the ground or the elevated structure 5〇1, 5〇2, the liquid 245 in the water storage tank can be injected into the cabin through the water inlet 241, and conversely, the liquid 245 in the body 24 can also pass through. The nozzle 243 is discharged into the water storage tank for the purpose of adjusting the amount of liquid. Incidentally, a water ball 249 can be disposed at the water inlet 241. When the water level rises to the water inlet 241, the floating ball 249 can block the water inlet 241 to control the liquid level. The above several power mechanisms 230 can be used for a small transport device capable of carrying 丨~2 people, a medium transport device capable of carrying 4~1G people, or a large transport device capable of carrying more than 3 (persons). t H puts more emphasis on its maneuverability, so its __2 is more suitable. Private artificial wings or spiral violet 232. The medium-sized transport large-scale transport device is considered to reduce the factors such as the size of the money-reducing capsule 210, and it is usually better to use the power mechanism such as the 233 or the sail. Therefore, because the buoyancy and the transport device can achieve the balance of force, in theory, this = Γ:: stay in any position in the space, the rise, fall or turn of the operation depends on the power mechanism used 23〇201141757 It can be used as a farmer or not. When using 3 sets of equipment, 200 hours should be matched with meteorological data, such as paying attention to wind, and ... when transporting in an empty space, the appropriate height should be 1000 meters on the ground, and the side should be large. It is 2.9 times larger and has a danger of breaking through. Flight === After setting 200, the road structure becomes unnecessary,
❹太盘^ 題可峨解決，所以可免除建造道路 =之、，破壞、節省能源與低噪音、使運輸 並可 對於 增加運輪效率、維護容易、製造成本低、 貌，趨向與大自然結合的生活方式，因此， 大眾運輸n她好的選擇。 限定===為本發明之實施例而已，當不能以此 明說明内六麟^’即大凡依本發明申請專利範圍及發 利涵蓋之的等效變化與修飾，皆仍屬本發明專 不須達成本發明所揭露之 1專她圍 要部分和Μ 的或優點或特點。此外，摘 資I刀和^|僅疋用來輔助 制本發明之權利範圍。 J又件搜寸之用並非用來限 【圖式簡單說明】 圖1為傳統飛艇之結構示意圖。 圖2為本發明之運輪«置側剖面示意圖。 意圖。為本發狄實施例的運輸裝置之動力機構俯視示 201141757 圖4為本發明之一實施例的運輸裝置之動力機構俯視示 意圖。 圖5為本發明之一實施例的運輸裝置之動力機構側視示 意圖。 【主要元件符號說明】 傳統飛艇100 骨架110 機殼120 氣室130 平板式尾鰭140 螺旋槳150 客艙160 運輸裝置200 氣囊210 支架220 動力機構230 人造翅膀231 螺旋槳232 纜繩233 動力源234 艙體240 入水口 241 201141757 重量調節機構242 出水口 243 外箱體244 液體245 内腔體246 支撐件247、248 浮球249 • 承載物250 安全索261、262 高架結構體501、502❹太盘^ Problem can be solved, so it can be exempted from building roads, destroying, saving energy and low noise, making transportation and adding efficiency to the transport wheel, easy maintenance, low manufacturing cost, appearance, and trend to integrate with nature. The lifestyle, therefore, the mass transit n her good choice. LIMITATION ================================================================================================= It is necessary to achieve the features or advantages or features of the invention disclosed herein. In addition, the incorporation of I and K| is only used to assist the scope of the invention. The use of J is not limited to the use of [simplified description] Figure 1 is a schematic diagram of the structure of a traditional airship. Figure 2 is a schematic cross-sectional view of the transport wheel of the present invention. intention. A top view of the power mechanism of the transport apparatus of the present embodiment is shown in the drawings. Fig. 4 is a plan view showing the power mechanism of the transport apparatus according to an embodiment of the present invention. Figure 5 is a side elevational view of the power mechanism of the transport apparatus in accordance with one embodiment of the present invention. [Main component symbol description] Traditional airship 100 skeleton 110 casing 120 gas chamber 130 flat fin fin 140 propeller 150 cabin 160 transport device 200 airbag 210 bracket 220 power mechanism 230 artificial wings 231 propeller 232 cable 233 power source 234 cabin 240 water inlet 241 201141757 Weight adjustment mechanism 242 Water outlet 243 Outer housing 244 Liquid 245 Inner chamber 246 Supports 247, 248 Float 249 • Carrier 250 Safety cables 261, 262 Elevated structures 501, 502
1111