TW201529134A - Flying building block assembly - Google Patents
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Abstract
Description
本發明是有關於一種積木組合,特別是指一種飛行積木組合。 The present invention relates to a building block combination, and more particularly to a flying building block combination.
參閱TW366296,揭露一習知積木組合,包含複數積木元件,該等積木元件能以不同角度分別成對地互補相連,依此可照著模型或想像而建構出大型結構。使用者可利用該等積木元件建構出如飛機及人體的結構,且元件間因為成對地互補相連,而有一可動地自由度,可以任意旋轉變形。 Referring to TW 366 296, a conventional building block assembly is disclosed that includes a plurality of building block elements that can be complementarily connected in pairs at different angles, whereby a large structure can be constructed in accordance with a model or imagination. The user can construct the structure such as the airplane and the human body by using the building block components, and the components are mutually connected in pairs, and have a movable degree of freedom, and can be arbitrarily rotated and deformed.
然而,習知的積木組合雖然可任意的組裝變形,完成特定外觀,但因積木的結構設計僅是為了能輕易地構成任何形狀,因此藉以組裝的模型不具有任何功能。所以,使用者儘管使用該等積木組合製成一飛機模型,該飛機模型完全不具有任何飛行的能力。 However, the conventional building block combination can be arbitrarily assembled and deformed to achieve a specific appearance, but since the structural design of the building block is only for easily forming any shape, the assembled model does not have any function. Therefore, even though the user uses these building blocks to make an aircraft model, the aircraft model does not have any flying ability at all.
參閱TWM392687U1,揭露一種習知飛行玩具,主要由發泡保力龍所構成,其包含有一飛機骨架、二補強機身架、一機翼、一扁平尾翼。該飛機骨架之相反二側分別黏貼上該等補強機身架,構成一機身。機翼之中央與該機身上緣黏接,該扁平尾翼黏貼於該機身之尾端底部。因 該飛機玩具是以發泡保力龍材質所構成,具有輕量化之特性,因此在滑行時該機翼能提供足夠的浮升力,而支撐住該飛行玩具,使之飛行。 Referring to TWM392687U1, a conventional flying toy is disclosed, which is mainly composed of a foaming dragon, which comprises an aircraft skeleton, a two-reinforcing fuselage frame, a wing, and a flat tail. The opposite sides of the aircraft skeleton are respectively attached to the reinforcing fuselage frames to form a fuselage. The center of the wing is bonded to the upper edge of the fuselage, and the flat tail is adhered to the bottom end of the fuselage. because The aircraft toy is made of foamed dragon material and has the characteristics of light weight, so that the wing can provide sufficient floating force when sliding, and support the flying toy to fly.
然而,習知的飛行玩具雖具有飛行功能,然其各個元件間皆以固定之方式連接,僅有單一種外觀,使用者無法依據其想像而調整該習知的飛行玩具。亦即,習知的飛行玩具無法供使用者發揮想像而完成其所欲達成的外觀。 However, the conventional flying toy has a flying function, but its components are connected in a fixed manner, and there is only a single appearance, and the user cannot adjust the conventional flying toy according to his imagination. That is, the conventional flying toy cannot provide the user with the imagination to complete the desired appearance.
所以,習知的積木組合雖能供使用者發揮想像,完成所欲的飛機型態,但卻不具有飛行的功能。而習知的飛行玩具雖具有飛行的功能,但使用者無法依據其想像完成所欲達成的外觀。習知的玩具中無法同時滿足任意組合及飛行功能的需要。 Therefore, the conventional building block combination can provide the user with the imagination to complete the desired aircraft type, but does not have the function of flying. While the conventional flying toy has the function of flying, the user cannot complete the desired appearance according to his imagination. Conventional toys cannot meet the needs of any combination and flight function at the same time.
因此,本發明之目的,即在提供一種可任意組裝且具有飛行功能的飛行積木組合。 Accordingly, it is an object of the present invention to provide a flyweight assembly that is arbitrarily assembled and has a flying function.
於是,本發明飛行積木組合,包含一骨架單元,及一機翼單元。該骨架單元包括一幹骨積木、一翼骨積木、一連接積木,及二翼接積木。該連接積木具有一沿直線方向延伸並供該幹骨積木可移除地插設的第一插孔,及一中心與該第一插孔相交的第二插孔。該第二插孔為沿與該第一插孔垂直的方向配置,並供該翼骨積木可移除地插設。該等翼接積木分別被該翼骨積木的二相反端部可移除地插設,且具有一結合組。 Thus, the flying block combination of the present invention comprises a skeleton unit and a wing unit. The skeleton unit comprises a dry bone building block, a wing bone building block, a connecting building block, and a two wing connecting block. The connecting block has a first insertion hole extending in a straight line direction for removably inserting the dry bone building block, and a second insertion hole at a center intersecting the first insertion hole. The second insertion hole is disposed in a direction perpendicular to the first insertion hole, and is removably inserted into the stalk building block. The winged blocks are removably inserted by opposite ends of the slat building block and have a combined set.
該機翼單元包括一翼片。該翼片具有位於兩相反端部的二卡合組,每一卡合組可供每一結合組可移除地卡固。該翼片能於滑翔時提供一浮升力,並藉該等翼接積木帶動該骨架單元,支持該飛行積木組合飛行。 The wing unit includes a flap. The flap has two snap-fit sets at opposite ends, each snap-fit group being removably securable for each bond set. The airfoil can provide a floating force when gliding, and the wing unit is used to drive the skeleton unit to support the flight building combination flight.
本發明之功效,在於提供不同的積木,讓使用者可以任意的拼湊組合,而完成所欲達成的外觀,且藉由可任意組裝的該翼片,使用者可藉此調整機翼單元的大小及位置,使之於滑翔時能提供足夠的浮升力使飛行積木組合飛行。 The effect of the invention is to provide different building blocks, so that the user can arbitrarily piece together the combination to complete the desired appearance, and by the arbitrarily assembled flap, the user can adjust the size of the wing unit. And the position, so that when gliding, it can provide enough floating force to fly the flying blocks.
1‧‧‧骨架單元 1‧‧‧ skeleton unit
11‧‧‧幹骨積木 11‧‧‧Bone bone building blocks
12‧‧‧翼骨積木 12‧‧‧Spetal building blocks
12’‧‧‧翼骨積木 12’‧‧·Wingbone blocks
12”‧‧‧翼骨積木 12"‧‧‧Spine bone blocks
13‧‧‧連接積木 13‧‧‧Connecting blocks
13I‧‧‧十字連接積木 13I‧‧‧cross connecting blocks
13I’‧‧‧十字連接積木 13I’‧‧‧cross connecting blocks
13I”‧‧‧十字連接積木 13I”‧‧‧cross connecting blocks
13II‧‧‧傾翼連接積木 13II‧‧‧wing connecting blocks
13III‧‧‧正交連接積木 13III‧‧‧Orthogonal connecting blocks
131‧‧‧第一插孔 131‧‧‧First jack
132‧‧‧第二插孔 132‧‧‧second jack
133‧‧‧第三插孔 133‧‧‧ third jack
14‧‧‧翼接積木 14‧‧‧ wing-connected blocks
141‧‧‧本體部 141‧‧ ‧ Body Department
142‧‧‧翼骨插孔 142‧‧‧wing bone jack
143‧‧‧結合組 143‧‧‧Combination group
144‧‧‧肋條 144‧‧‧ Ribs
145‧‧‧鏤空區 145‧‧‧The open space
146‧‧‧凸塊 146‧‧‧Bumps
147‧‧‧頭段 147‧‧‧ head
148‧‧‧身段 148‧‧‧ body
149‧‧‧卡合空間 149‧‧‧Clock space
15‧‧‧翼接積木 15‧‧‧ wing connected blocks
151‧‧‧本體部 151‧‧‧ Body Department
152‧‧‧翼骨插孔 152‧‧‧wing bone jack
153‧‧‧結合組 153‧‧‧Combination group
154‧‧‧凸塊 154‧‧‧Bumps
155‧‧‧卡片 155‧‧‧ card
156‧‧‧頭段 156‧‧‧ head
157‧‧‧身段 157‧‧‧1
158‧‧‧卡合空間 158‧‧‧Clock space
16‧‧‧翼接積木 16‧‧‧ wing-connected blocks
160‧‧‧容置空間 160‧‧‧ accommodating space
161‧‧‧本體部 161‧‧‧ Body Department
162‧‧‧翼骨插孔 162‧‧‧wing bone jack
163‧‧‧結合組 163‧‧‧Combination group
164‧‧‧凸塊 164‧‧‧Bumps
165‧‧‧夾片 165‧‧‧ Clips
166‧‧‧卡槽 166‧‧‧ card slot
167‧‧‧連接區 167‧‧‧Connected area
168‧‧‧穿孔 168‧‧‧Perforation
169‧‧‧卡固區 169‧‧‧Kalgu District
2‧‧‧機翼單元 2‧‧‧wing unit
21‧‧‧翼片 21‧‧‧ wing
211‧‧‧卡合組 211‧‧‧Card Group
212‧‧‧穿孔 212‧‧‧Perforation
3‧‧‧重力單元 3‧‧‧Gravity unit
31‧‧‧長方形積木 31‧‧‧ Rectangular blocks
32‧‧‧方形積木 32‧‧‧Square blocks
33‧‧‧弧形積木 33‧‧‧Arc-shaped blocks
4‧‧‧尾翼 4‧‧‧tail
41‧‧‧尾翼插孔 41‧‧‧Tail Hub
本發明之其他的特徵及功效,將於參照圖式的實施方式中清楚地呈現,其中:圖1是一立體分解圖,說明本發明飛行積木組合之一較佳實施例的元件;圖2是一局部放大分解圖,說明本較佳實施例的一翼接積木的第一實施態樣與二翼片的連接方式;圖3是一立體圖,說明本較佳實施例的第一較佳實施例,為一傳統型的飛機組合;圖4是一立體圖,說明本較佳實施例的第二較佳實施例,為一傾翼型的飛機組合;圖5是一立體圖,說明本較佳實施例的第三較佳實施例,為一展翼型的飛機組合;圖6是一立體圖,說明本較佳實施例的第四較佳實施例,為一多翼型的飛機組合; 圖7是一立體圖,說明本較佳實施例的第五較佳實施例,為一疊翼型的飛機組合;圖8是一立體圖,說明本較佳實施例的第六較佳實施例,為一折翼型的飛機組合;圖9是一立體圖,說明本較佳實施例的該翼接積木的第二實施態樣;及圖10是一立體圖,說明本較佳實施例的該翼接積木的第三實施態樣。 Other features and advantages of the present invention will be apparent from the embodiments of the present invention. FIG. 1 is an exploded perspective view of the components of a preferred embodiment of the flying block combination of the present invention; FIG. 3 is a perspective view showing a first preferred embodiment of the preferred embodiment, showing a first embodiment of the preferred embodiment of the preferred embodiment of the present invention; FIG. 4 is a perspective view showing a second preferred embodiment of the preferred embodiment, which is a tilt-wing type aircraft combination; FIG. 5 is a perspective view illustrating the preferred embodiment of the present invention. The third preferred embodiment is a wing-type aircraft combination; FIG. 6 is a perspective view showing a fourth preferred embodiment of the preferred embodiment, which is a multi-wing type aircraft combination; Figure 7 is a perspective view showing a fifth preferred embodiment of the preferred embodiment, which is a stack of aircraft combinations; Figure 8 is a perspective view showing a sixth preferred embodiment of the preferred embodiment, FIG. 9 is a perspective view showing a second embodiment of the winged building block of the preferred embodiment; and FIG. 10 is a perspective view showing the winged building block of the preferred embodiment. The third embodiment.
在本發明被詳細描述之前,應當注意在以下的說明內容中,類似的元件是以相同的編號來表示。 Before the present invention is described in detail, it should be noted that in the following description, similar elements are denoted by the same reference numerals.
需先注意的是,圖1為說明本發明飛行積木組合中所使用的各個元件。為了方便說明各較佳實施例的原件結構,每一較佳實施例皆會參考圖1所列之元件。 It is to be noted that Figure 1 is intended to illustrate the various components used in the flying block combination of the present invention. In order to facilitate the description of the original structure of the preferred embodiment, each of the preferred embodiments will refer to the elements listed in FIG.
參閱圖1至圖3,為本發明之第一較佳實施例,為一傳統型的飛機組合。其為使用一個幹骨積木11、二個翼骨積木12、一個十字連接積木13I、四個翼接積木14、二片翼片21、一個重力單元3,及二片尾翼4所構成。其材質為碳纖維或者塑膠等輕質材料。 Referring to Figures 1 through 3, a first preferred embodiment of the present invention is a conventional aircraft combination. It consists of using one dry bone building block 11, two wing bone building blocks 12, one cross connecting building block 13I, four wing connecting blocks 14, two flaps 21, one gravity unit 3, and two tail fins 4. It is made of lightweight materials such as carbon fiber or plastic.
該幹骨積木11為沿直線延伸的方柱形。每一翼骨積木12得與該幹骨積木11的形狀相同,亦得為不同的形狀,理應不以本較佳實施例所揭露的內容為限制。 The dry bone block 11 is a square column shape extending in a straight line. Each of the splanchnic blocks 12 has the same shape as the dry bone building block 11, and has a different shape, and should not be limited by the contents disclosed in the preferred embodiment.
該十字連接積木13I為本發明連接積木13之第 一種實施態樣,具有沿直線方向延伸的一第一插孔131及一第二插孔132。該該第二插孔132與第一插孔131相互垂直,且該第二插孔132的中心與該第一插孔131相交。 The cross-connected building block 13I is the first connecting block 13 of the present invention An embodiment has a first insertion hole 131 and a second insertion hole 132 extending in a straight line direction. The second insertion hole 132 and the first insertion hole 131 are perpendicular to each other, and the center of the second insertion hole 132 intersects with the first insertion hole 131.
每一翼接積木14具有一本體部141、三個形成於該本體部141上的翼骨插孔142,及二結合組143。該本體部141外周緣略呈眼形,且具有複數連接外周緣及內周緣的肋條144。該等肋條144與該本體部141外周緣相配合界定出複數鏤空區145。每一翼骨插孔142的形狀為十字形,為供每一翼骨積木12插設。 Each wing block 14 has a body portion 141, three wing hole sockets 142 formed on the body portion 141, and a second coupling group 143. The outer peripheral edge of the body portion 141 is slightly eye-shaped and has a plurality of ribs 144 connecting the outer peripheral edge and the inner peripheral edge. The ribs 144 cooperate with the outer periphery of the body portion 141 to define a plurality of hollowed out regions 145. Each wing bone hub 142 is shaped like a cross for each of the wing bone blocks 12 to be inserted.
該等結合組143分別設於該本體部的二個側緣,且每一結合組143具有三個凸扣146。該結合組143亦可僅為一。該結合組143亦可僅包含一或二個凸扣146,又或者為四個以上的凸扣146。 The bonding groups 143 are respectively disposed on the two side edges of the body portion, and each bonding group 143 has three buckles 146. The bonding group 143 may also be only one. The bonding group 143 may also include only one or two buckles 146 or four or more knobs 146.
每一凸扣146具有一頭段147,及一連接該頭段147與該本體部141的身段148。該頭段147與該身段148及本體部141的外周緣相配合界定出一卡合空間149。值得一提的是,該本體部141的外周緣可形成複數個與該等凸扣146相配合的凹槽,使該等凸扣146分別設置於該等凹槽內。 Each of the buckles 146 has a head section 147 and a body section 148 connecting the head section 147 and the body portion 141. The head section 147 cooperates with the outer circumference of the body section 148 and the body portion 141 to define an engagement space 149. It is to be noted that the outer peripheral edge of the main body portion 141 can form a plurality of grooves matching the convex buckles 146, so that the convex buckles 146 are respectively disposed in the grooves.
藉由將該幹骨積木11、該等翼骨積木12,及該等翼接積木14連接,構成一骨架單元1。連接方式為將該幹骨積木11插設於該十字連接積木13I的第一插孔131中,並將該等翼骨積木12分別插設於該十字連接積木13I的第二插孔132中,最後將每二個翼接積木14設於每一翼骨 積木12的二相反端部上。 The skeleton unit 1 is constructed by joining the dry bone building block 11, the wing building blocks 12, and the wing building blocks 14. The connection method is that the dry bone building block 11 is inserted into the first insertion hole 131 of the cross-connected building block 13I, and the wing-shaped building blocks 12 are respectively inserted into the second insertion holes 132 of the cross-connecting building block 13I. Finally, each of the two wing blocks 14 is placed on each wing bone. The opposite ends of the building blocks 12 are opposite.
每一翼片21具有位於兩相反端部的二卡合組211。每一卡合組211為可供該等翼接積木14的每一結合組143可移除地卡固,並具有與該等凸扣146相配合的三個穿孔212。藉由將該等卡合組211分別卡固於該等結合組143上,使每一翼片21設於二個該等翼接積木14上,完成一機翼單元2。 Each flap 21 has a two snap group 211 at opposite ends. Each of the engagement sets 211 is removably secured for each of the sets 143 of the winged bricks 14 and has three perforations 212 that cooperate with the male buckles 146. By attaching the engaging groups 211 to the coupling groups 143, each of the flaps 21 is disposed on the two wing-connecting blocks 14 to complete a wing unit 2.
值得一提的是,該機翼單元2可包括四片翼片21(如圖1所示)。每一翼片21被二個翼接積木14卡固而服貼於該翼接積木14的本體部141的外周緣,使每一翼接積木14連接二個翼片21。此一連接的方式可任意選用。 It is worth mentioning that the wing unit 2 can comprise four flaps 21 (as shown in Figure 1). Each of the flaps 21 is fastened by the two winged bricks 14 to the outer periphery of the body portion 141 of the winged building block 14, such that each winged building block 14 connects the two flaps 21. The way of this connection can be arbitrarily selected.
該重力單元3設於該幹骨積木11上,且鄰近該十字連接積木13I之一端部。該重力單元3由一個長方形積木31,及一個方形積木32構成。該長方形積木31長方向的一末端部側面與該幹骨積木11相連。該方形積木32連接在該長方形積木31的另一相反末端。 The gravity unit 3 is disposed on the dry bone block 11 and adjacent to one end of the cross-connected building block 13I. The gravity unit 3 is composed of a rectangular block 31 and a square block 32. A side end side surface of the rectangular block 31 in the longitudinal direction is connected to the dry bone block 11. The square block 32 is attached to the other opposite end of the rectangular block 31.
該等尾翼4之間相互垂直,並設於該幹骨積木11的兩相反端上,且包括至少一用於被該幹骨積木11或該翼骨積木12插設的尾翼插孔41。 The empennages 4 are perpendicular to each other and are disposed on opposite ends of the dry bone building block 11 and include at least one empennage insertion hole 41 for being inserted by the dry bone building block 11 or the splanchnic building block 12.
藉由調整該重力單元3、該等尾翼4的位置及組合狀態,使該傳統型飛機組合於滑行時有較佳的平衡,且該機翼單元2能於滑行時提供一浮升力,使該傳統型飛機組合能穩固地自由滑翔飛行。 By adjusting the position and combined state of the gravity unit 3, the tail fins 4, the conventional aircraft combination has a better balance when sliding, and the wing unit 2 can provide a floating force when coasting, so that the The traditional aircraft combination can steadily fly freely.
參閱圖1、圖2及圖4,為本發明的第二較佳實 施例,為一傾翼型的飛機組合。使用一個幹骨積木11、二個翼骨積木12、一個傾翼連接積木13II、四個翼接積木14、二片翼片21、一個重力單元3,及二片尾翼4所構成。 Referring to FIG. 1 , FIG. 2 and FIG. 4 , it is a second preferred embodiment of the present invention. The example is a combination of a winged aircraft. A dry bone building block 11, two wing bone building blocks 12, a tilting connection building block 13II, four wing connecting blocks 14, two flaps 21, a gravity unit 3, and two tail fins 4 are used.
該傾翼連接積木13II為本發明連接積木13之第二種實施態樣,具有一沿直線方向延伸的第一插孔131,及一中心與該第一插孔131相交的第二插孔132。該第二插孔132為沿與該第一插孔131垂直的方向配置,且外形呈V形。因為該第二插孔132呈現V形,因此在***該等翼骨積木12後會呈現傾揚形態,使得該機翼單元2呈現對稱的V形。 The tilting connection building block 13II is a second embodiment of the connecting building block 13 of the present invention, having a first insertion hole 131 extending in a straight line direction, and a second insertion hole 132 having a center intersecting the first insertion hole 131 . The second insertion hole 132 is disposed in a direction perpendicular to the first insertion hole 131 and has a V shape. Because the second receptacle 132 assumes a V-shape, it will assume a tilted configuration upon insertion of the slats 12 such that the wing unit 2 assumes a symmetrical V-shape.
該重力單元3是由一長方形積木31、二方形積木32,及一弧形積木33堆疊而成。該長方形積木31的長方向的一末端連接在該幹骨積木11的一端,且另一末端連接該弧形積木33。該長方形積木31及該弧形積木33的下側面連接二個相連的方形積木32。該重力單元3構成一機頭形。 The gravity unit 3 is formed by stacking a rectangular block 31, a square block 32, and a curved block 33. One end of the rectangular building block 31 in the longitudinal direction is connected to one end of the dry bone building block 11, and the other end is connected to the curved building block 33. The rectangular building block 31 and the lower side of the curved building block 33 are connected to two connected square blocks 32. The gravity unit 3 constitutes a head shape.
該等尾翼4是以相互垂直的方式連接,並設於該幹骨積木11遠離該重力單元3的一末端上。藉由調整該重力單元3與該等尾翼4的位置及組合狀態,使該傾翼型飛機組合於滑行時有較佳的平衡,且該機翼單元2能於滑行時提供一浮升力,使該傾翼型飛機組合能穩固地自由滑翔飛行。 The tail fins 4 are connected to each other in a perpendicular manner and are disposed on an end of the dry bone building block 11 away from the gravity unit 3. By adjusting the position and combination state of the gravity unit 3 and the tail fins 4, the tilting type aircraft combination has a better balance when sliding, and the wing unit 2 can provide a floating force when coasting, so that The tilt-wing aircraft combination is capable of steadily gliding freely.
本較佳實施例是利用具有傾角的該傾翼連接積木13II而使該機翼單元2的該等翼片21之間形成一角度, 與傳統的飛機形態不同。使用者可任意的變換該連接積木13的態樣而完成具有角度或不具有角度的該機翼單元2。 The preferred embodiment uses the tilting wing connecting block 13II having an inclination to form an angle between the fins 21 of the wing unit 2, Different from the traditional aircraft form. The user can arbitrarily change the aspect of the connecting block 13 to complete the wing unit 2 with or without angle.
參閱圖1、圖2及圖5,為本發明的第三較佳實施例,為一展翼型的飛機組合。本較佳實施例為該第一較佳實施例的變化,其為多增加二個翼骨積木12、二個傾翼連接積木13II、四個翼接積木14,及二片翼片21。 Referring to Figures 1, 2 and 5, a third preferred embodiment of the present invention is a wing-type aircraft combination. The preferred embodiment is a variation of the first preferred embodiment in which two additional scurved building blocks 12, two slanting wing connecting blocks 13II, four winged building blocks 14, and two flaps 21 are added.
藉由新增的該等傾翼連接積木13II的第二插孔132,將新增的該等翼接積木12分別連結至該第一較加實施例的該等翼骨積木12的末端,再將每二個新增的翼接積木14設於每一新增的翼骨積木12的二相反端部上,形成延展的骨架單元1。 Adding the newly added wing blocks 12 to the ends of the stalked building blocks 12 of the first comparative embodiment by adding the second insertion holes 132 of the inclined wing connecting blocks 13II, respectively. Each of the two newly added wing blocks 14 is placed on the opposite ends of each of the newly added slats 12 to form an extended skeleton unit 1.
藉由將新增的每一翼片21卡固於位在每一新增的翼骨積木12上的二個翼接積木14,構成一延長的機翼單元2。 An elongated wing unit 2 is formed by snapping each of the newly added flaps 21 to the two wing-joined blocks 14 on each of the newly added slats 12.
藉由調整該重力單元3、該等尾翼4及該等機翼單元2,而使該展翼型飛機組合於滑行時能自該機翼單元2獲得一浮升力,並藉該重力單元3調整飛機整體的重心及該等尾翼4平衡飛機整體,使該展翼型飛機組合能穩固地自由滑翔飛行。 By adjusting the gravity unit 3, the empennage 4 and the wing units 2, the wing-type aircraft can obtain a floating force from the wing unit 2 when it is slid, and is adjusted by the gravity unit 3 The overall center of gravity of the aircraft and the empennage 4 balance the aircraft as a whole, so that the wing-type aircraft combination can steadily glider freely.
本實施態樣為利用二不同形態的該等連接積木13I、13II延長機翼的骨架,進而增加該機翼單元2的長度。使用者藉著使用該等連接積木13I、13II而可以任意的調整該機翼單元2的長度,不受到該等翼骨積木12長度的限制。 In this embodiment, the connecting blocks 13I and 13II of the two different forms are used to extend the skeleton of the wing, thereby increasing the length of the wing unit 2. The user can arbitrarily adjust the length of the wing unit 2 by using the connecting blocks 13I, 13II without being limited by the length of the splanchnic building blocks 12.
參閱圖1、圖2及圖6,為本發明的第四較佳實施例,為一多翼型的飛機組合。本較佳實施例為該第二較佳實施例的變化,特色在於捨棄尾翼4而改用另一機翼單元2代替,以及簡化該重力單元3。 Referring to Figures 1, 2 and 6, a fourth preferred embodiment of the present invention is a multi-wing aircraft combination. The preferred embodiment is a variation of the second preferred embodiment, characterized in that the tail 4 is discarded and replaced by another wing unit 2, and the gravity unit 3 is simplified.
本實施例為多增加二個翼骨積木12、一個傾翼連接積木13II、四個翼接積木14、二片翼片21。其為將該第二較佳實施例的該尾翼4移除,並將該第二較佳實施例的該幹骨積木11插設入該新增的傾翼連接積木13II的第一插孔131上,而使該骨架單元1增加機翼單元2成為可能。 In this embodiment, two splanchnic building blocks 12, one slanting connecting block 13II, four wing connecting blocks 14, and two flaps 21 are added. The rear wing 4 of the second preferred embodiment is removed, and the dry bone building block 11 of the second preferred embodiment is inserted into the first insertion hole 131 of the newly added tilting connection building block 13II. It is possible to increase the wing unit 2 by the skeleton unit 1.
為了方便說明,以下僅說明新增元件的連接方式:該等翼骨積木12分別***該傾翼連接積木13II的第二插孔132上,再將每二個翼接積木14設於每一翼骨積木12的二相反端部上,完成該骨架單元1。將每一翼片21卡固於位在每一該等翼接積木14上,構成二個機翼單元2。 For convenience of explanation, only the connection manner of the newly added components will be described below: the wing building blocks 12 are respectively inserted into the second insertion holes 132 of the tilting connection building block 13II, and each of the two wing connecting blocks 14 is disposed on each wing bone. The skeleton unit 1 is completed at the opposite ends of the building block 12. Each of the fins 21 is fastened to each of the wing-mounted blocks 14 to form two wing units 2.
該重力單元3僅包括一長方形積木31,且該長方形積木31長方向的一末端部側面與該幹骨積木11相連。 The gravity unit 3 includes only one rectangular block 31, and a distal end side of the rectangular block 31 is connected to the dry bone block 11.
藉由調整該重力單元3及該等機翼單元2,而使該多翼型飛機組合於滑行時能自該等機翼單元2獲得一浮升力,並藉該重力單元3調整飛機整體的重心,使該多翼型飛機組合能穩固地自由滑翔飛行。 By adjusting the gravity unit 3 and the wing units 2, the multi-wing aircraft can be combined with the wing unit 2 to obtain a floating force when the vehicle is gliding, and the gravity unit 3 is used to adjust the overall center of gravity of the aircraft. This allows the multi-wing aircraft combination to steadily glider freely.
本較佳實施例是藉由使用將多個傾翼連接積木13II設於該幹骨積木11上,而增加該等機翼單元2的數量 。使用者可利用增加連接積木13的方式,而簡單的達到其所欲的該等機翼單元2數量。 The preferred embodiment increases the number of the wing units 2 by using a plurality of tilting connection blocks 13II on the dry bone block 11. . The user can simply increase the number of such wing units 2 as desired by increasing the number of connecting blocks 13.
參閱圖1、圖2及圖7,為本發明的第五較佳實施例,為一疊翼型的飛機組合,是利用二不同形態的連接積木13I、13III,組裝複數機翼單元2的飛機。使用二個幹骨積木11、四個翼骨積木12、一個十字連接積木13I、一個正交連接積木13III、八個翼接積木14、四片翼片21、一個重力單元3,及一片尾翼4所構成。 Referring to FIG. 1 , FIG. 2 and FIG. 7 , a fifth preferred embodiment of the present invention is a stack of airfoil aircraft combinations, which are assembled by using two different types of connecting blocks 13I and 13III to assemble a plurality of wing units 2 . . Use two dry bone blocks 11, four sacral blocks 12, one cross-connected building block 13I, one orthogonal connecting block 13III, eight winged building blocks 14, four flaps 21, one gravity unit 3, and one piece of tail 4 Composition.
該正交連接積木13III為本發明連接積木13的第三實施態樣,具有沿直線方向延伸且相互正交的一第一插孔131、一第二插孔132,及一第三插孔133。值得一提的是,該正交連接積木13III可使用二個十字連接積木13I交叉堆疊而成,其堆疊方式是將該等第二插孔132的軸線方向相互垂直,並使該等第一插孔131相互對準並相通。 The orthogonal connection building block 13III is a third embodiment of the connecting building block 13 of the present invention, and has a first insertion hole 131, a second insertion hole 132, and a third insertion hole 133 extending in a straight line direction and orthogonal to each other. . It is worth mentioning that the orthogonal connecting building block 13III can be formed by stacking two cross connecting blocks 13I in a stacking manner, such that the axial directions of the second insertion holes 132 are perpendicular to each other, and the first insertion is made. The holes 131 are aligned and in communication with each other.
藉由將該等幹骨積木11、該等翼骨積木12,及該等翼接積木14連接,構成一骨架單元1。連接方式為將該等幹骨積木11其中之一插設於該正交連接積木13III的第一插孔131中,另一幹骨積木11插設於該第三插孔133中。***該第三插孔133中的該幹骨積木11另一末端插設入該十字連接積木13I的第一插孔131中。將該等翼骨積木12分別插設於該正交連接積木13III及該十字連接積木13I的第二插孔132中。將每二個翼接積木14設於每一翼骨積木12的二相反端部上。 The skeleton unit 1 is constructed by joining the dry bone blocks 11, the wing building blocks 12, and the wing building blocks 14. The connection is made by inserting one of the dry bone blocks 11 into the first insertion hole 131 of the orthogonal connection block 13III, and the other dry bone building block 11 is inserted into the third insertion hole 133. The other end of the dry bone building block 11 inserted into the third insertion hole 133 is inserted into the first insertion hole 131 of the cross-connected building block 13I. The slats 12 are respectively inserted into the orthogonal connecting block 13III and the second insertion hole 132 of the cross-connecting block 13I. Each of the two winged blocks 14 is placed on the opposite ends of each of the splanchnic blocks 12.
藉由將每一翼片21卡固於位在每一翼骨積木 12上的二個翼接積木14,構成二個機翼單元2。 By tying each flap 21 in place in each stalk building block The two wings on the 12 are connected to the building block 14 to form two wing units 2.
該重力單元3是由一長方形積木31、一方形積木32,及一弧形積木33堆疊而成。該長方形積木31的長方向的一末端連接在該幹骨積木11中鄰近該正交連接積木13III的一端。該長方形積木31的長方向的另一末端連接該弧形積木33。該長方形積木31的下側面連接該方形積木32。該重力單元3構成一機頭形。 The gravity unit 3 is formed by stacking a rectangular block 31, a square block 32, and a curved block 33. An end of the rectangular building block 31 in the longitudinal direction is connected to one end of the dry bone building block 11 adjacent to the orthogonal connecting block 13III. The other end of the rectangular block 31 in the longitudinal direction is connected to the curved block 33. The lower side of the rectangular block 31 is connected to the square block 32. The gravity unit 3 constitutes a head shape.
該尾翼4設於該幹骨積木11遠離該重力單元3的一末端上。藉由調整該重力單元3、該尾翼4及該等機翼單元2,而使該疊翼型飛機組合於滑行時能自該等機翼單元2獲得一浮升力,並藉該重力單元3調整飛機整體的重心及該等尾翼4平衡飛機整體,使該疊翼型飛機組合能穩固地自由滑翔飛行。 The empennage 4 is disposed on an end of the dry bone block 11 away from the gravity unit 3. By adjusting the gravity unit 3, the empennage 4 and the wing units 2, the stacking aircraft can be combined with the wing unit 2 to obtain a lifting force when sliding, and adjusted by the gravity unit 3 The overall center of gravity of the aircraft and the empennage 4 balance the aircraft as a whole, so that the stack of aircraft can be steadily gliding freely.
本實施態樣是使用該正交連接積木13III作為骨架連接的中樞。因為該正交連接積木13III具有三軸的連接方向,因此相較傳統的飛機態樣,使用該正交連接積木13III能多增一連接位置,使完成疊翼型態的飛機組合成為可能。使用者可以輕易的使用該正交連接積木13III而增加連接的自由度。 The present embodiment uses the orthogonally connected building block 13III as a backbone connection. Since the orthogonal connecting block 13III has a three-axis connecting direction, the orthogonal connecting block 13III can be used to increase the connecting position more than the conventional aircraft aspect, making it possible to complete the stacking type of aircraft combination. The user can easily use the orthogonal connection block 13III to increase the degree of freedom of connection.
參閱圖1、圖2及圖8,為本發明的第六較佳實施例,是一折翼型的飛機組合。使用二個幹骨積木11、五個翼骨積木12、三個十字連接積木13I、二個傾翼連接積木13II、八個翼接積木14、四片翼片21,及一片尾翼4所構成。 Referring to Figures 1, 2 and 8, in accordance with a sixth preferred embodiment of the present invention, a wing-type aircraft combination is illustrated. Two dry bone blocks 11, five sacral building blocks 12, three cross-connecting blocks 13I, two slanting connecting blocks 13II, eight winged building blocks 14, four flaps 21, and one piece of empennage 4 are used.
以下為了方便說明,將該等翼骨積木12依連接方式區分為一個翼骨積木12’,及四個翼骨積木12”。將該等十字連接積木13I依連接方式區分為一個十字連接積木13I’,及二個十字連接積木13I”。 Hereinafter, for convenience of description, the splanchnic building blocks 12 are divided into one scurved building block 12' and four sacral building blocks 12' by connection. The cross-connected building blocks 13I are divided into a cross-connected building block 13I according to the connection manner. ', and two cross-connected building blocks 13I".
藉由將該等幹骨積木11、該等翼骨積木12,及該等翼接積木14連接,構成一骨架單元1。連接方式為將該翼骨積木12’穿設於該十字連接積木13I’的第二插孔132內,再將該等幹骨積木11分別插設於該十字連接積木13I’的第一插孔131內。該翼骨積木12’的兩相反端分別藉由該等傾翼連接積木13II的第二插孔132與該等翼骨積木12”其中之二者的一端連接。該等翼骨積木12”的另一端藉由該等十字連接積木13I”的第二插孔132與該等翼骨積木12”剩餘之二者連接。最後,將每二個翼接積木14設於每一翼骨積木12的二相反端部上,完成該骨架單元1。 The skeleton unit 1 is constructed by joining the dry bone blocks 11, the wing building blocks 12, and the wing building blocks 14. The connection mode is that the splanchnic building block 12' is inserted into the second insertion hole 132 of the cross-connecting building block 13I', and the dry bone building blocks 11 are respectively inserted into the first insertion hole of the cross-connecting building block 13I'. Within 131. The opposite ends of the splanchnic building block 12' are respectively connected to one end of the spheroid building blocks 12" by the second insertion holes 132 of the slanting wing connecting blocks 13II. The spheroidal building blocks 12" The other end is connected to the remaining two of the splanchnic building blocks 12" by the second receptacle 132 of the cross-connecting blocks 13I". Finally, each of the two winged bricks 14 is placed on the opposite ends of each of the splanchnic blocks 12 to complete the skeleton unit 1.
藉由將每一翼片21卡固於位在每一翼骨積木12上的二個翼接積木14,構成一個機翼單元2。 A wing unit 2 is constructed by snapping each of the flaps 21 to two wing-connected blocks 14 positioned on each of the splanchnic blocks 12.
該尾翼4為設於該幹骨積木11遠離該十字連接積木13I’的一末端上。藉由調整該尾翼4及該機翼單元2,而使該折翼型飛機組合於滑行時能自該尾翼4及該機翼單元2獲得一浮升力,使該折翼型飛機組合能自由滑翔飛行。 The empennage 4 is disposed at an end of the dry bone building block 11 away from the cross-connecting block 13I'. By adjusting the tail 4 and the wing unit 2, the wing-type aircraft can be combined with the wing unit 4 and the wing unit 2 to obtain a floating force when the vehicle is gliding, so that the wing-type aircraft combination can freely glide. flight.
本實施態樣是藉著使用將多種態樣的連接積木13’、13”相互連接於該等翼骨積木12之間,而形成變化形式的機翼單元2。使用者可利用此一方式而簡單的變化其所 欲的該機翼單元2形態。 The present embodiment forms a variant of the wing unit 2 by using a plurality of connection building blocks 13', 13" connected to each other between the wing building blocks 12. The user can use this method. Simple change The shape of the wing unit 2 is desired.
需注意的是,本發明的飛行積木組合,可僅由一幹骨積木11、一翼骨積木12、一正交連接積木13III(或為一十字連接積木13I)、二翼接積木14、一翼片21所構成。該幹骨積木11及該翼骨積木12分別穿設在該正交連接積木13III的第一插孔131及第二插孔132上,形成對稱的十字形,再將該翼接積木14設於該翼骨積木12的兩相反端部上,最後將該翼片21與該翼接積木14卡固,進而界定出二相對稱的翼片部(圖未示),完成一飛機。 It should be noted that the flying block combination of the present invention may consist of only a dry bone building block 11, a wing bone building block 12, an orthogonal connecting building block 13III (or a cross connecting building block 13I), a two wing connecting building block 14, and a wing piece. 21 constitutes. The dry bone building block 11 and the splanchnic building block 12 are respectively disposed on the first insertion hole 131 and the second insertion hole 132 of the orthogonal connecting block 13III to form a symmetrical cross shape, and the wing connecting block 14 is disposed on the wing block 14 At the opposite ends of the splanchnic building block 12, the wing piece 21 is finally clamped to the wing connecting block 14, thereby defining two symmetrical flap portions (not shown) to complete an aircraft.
值得一提的是,一翼接積木14還有二種實施態樣,為與該等翼接積木14做為區別,區分第二實施態樣為翼接積木15,及第三實施態樣為翼接積木16。 It is worth mentioning that there are two implementations of a winged building block 14 in order to distinguish it from the wing-connected building blocks 14, distinguishing the second embodiment from a wing-connected building block 15, and the third embodiment is a wing. Connect the building blocks 16.
參閱圖9,為一第二實施態樣的翼接積木15。該翼接積木15具有一本體部151、三個形成於該本體部151上的翼骨插孔152,及一結合組153。該本體部151結構與第一實施態樣的該等翼接積木14(見圖2)相同。該等翼骨插孔152為米字形。 Referring to Figure 9, a winged building block 15 of a second embodiment is illustrated. The wing block 15 has a body portion 151, three wing hole sockets 152 formed on the body portion 151, and a coupling group 153. The structure of the body portion 151 is the same as that of the winged building block 14 (see Fig. 2) of the first embodiment. The wing bone hubs 152 are in the shape of a meter.
該結合組153具有三個設於該本體部151一側緣的凸塊154,及二個設於該本體部151二相反端的卡片155。每一凸塊154具有一頭段156,及一連接該頭段156與該本體部151的身段157。該頭段156與該身段157、該等卡片155及該本體部151的外周緣相配合界定出一卡合空間158。 The bonding group 153 has three protrusions 154 disposed on one side of the body portion 151 and two cards 155 disposed at opposite ends of the body portion 151. Each of the bumps 154 has a head section 156 and a body section 157 connecting the head section 156 and the body portion 151. The head segment 156 cooperates with the body segment 157, the card 155 and the outer periphery of the body portion 151 to define an engagement space 158.
參閱圖2及圖9當使用該翼接積木15取代該翼 接積木14,並用以連接一翼片21時,每一穿孔212能被每一凸塊154的頭段156穿入而使該翼片21容置於該卡合空間158內,並被設於該本體部151二相反端的卡片155可移除地夾持。 Referring to Figures 2 and 9, when the wing 15 is used to replace the wing When the bricks 14 are connected and used to connect the fins 21, each of the through holes 212 can be inserted into the head section 156 of each of the bumps 154 to receive the fins 21 in the engaging space 158, and is disposed in the The card 155 at the opposite end of the body portion 151 is removably clamped.
參閱圖10,為一第三實施態樣的翼接積木16,呈現一髮夾形。該翼接積木16具有一本體部161、三個形成於該本體部161上的翼骨插孔162,及一結合組163。該本體部161的結構與第一實施態的樣該等翼接積木14相同。該翼骨插孔162為米字形。 Referring to Figure 10, a wing block 16 of a third embodiment presents a hairpin shape. The wing block 16 has a body portion 161, three wing hole sockets 162 formed on the body portion 161, and a coupling group 163. The structure of the body portion 161 is the same as that of the wing block 14 of the first embodiment. The wing bone hub 162 is in the shape of a meter.
該結合組163具有三個設於該本體部161一側緣的凸塊164、設於該本體部161的兩相反端的一夾片165及一卡槽166。該夾片165的外形呈現與該本體部161的外周緣相配合的弧度,且具有三個分別與該等凸塊164相配合的穿孔168、位於兩相反端的一連接區167及一卡固區169。該夾片是藉由該連接區167而連接於該本體部161的一端上,且能藉著該卡固區169而卡設於該結合組163的卡槽166上。該夾片165與該本體部161的外周緣之間界定出一容置空間160。 The bonding group 163 has three protrusions 164 disposed on one side of the main body portion 161 , a clip 165 disposed at opposite ends of the main body portion 161 , and a latching groove 166 . The clip 165 has an outer shape that matches the outer circumference of the body portion 161, and has three through holes 168 respectively matching the protrusions 164, a connecting portion 167 at opposite ends, and a fastening portion. 169. The clip is connected to one end of the body portion 161 by the connecting portion 167, and can be locked on the card slot 166 of the coupling group 163 by the fastening portion 169. An accommodating space 160 is defined between the clip 165 and the outer periphery of the body portion 161.
參閱圖2及圖10,當使用該等翼接積木16取代該翼接積木14,並用以連接一翼片21時,每一穿孔212能被每一凸塊164穿入,並藉由扳動該夾片165將該翼片21夾設於該容置空間160內,且該夾片165的卡固區169能卡固於該卡槽166上而不脫落,使該翼片21被夾設固定。 Referring to Figures 2 and 10, when the wing blocks 16 are used to replace the wing blocks 14 and are used to connect a wing piece 21, each of the holes 212 can be penetrated by each of the blocks 164, and by pulling The clip 165 is disposed in the accommodating space 160, and the fastening portion 169 of the clip 165 can be clamped on the slot 166 without falling off, so that the flap 21 is clamped and fixed. .
需注意的是,該等翼接積木14、15及16於組合該骨架單元1時可擇一使用,或者任意地混合使用。本發明的各較佳實施例為方便說明,僅揭露該等翼接積木14作為該骨架單元1之元件。 It should be noted that the wing blocks 14, 15 and 16 may be used alternatively when the frame unit 1 is combined, or may be used arbitrarily. The preferred embodiments of the present invention are for convenience of explanation, and only the winged bricks 14 are disclosed as elements of the skeleton unit 1.
綜上所述,使用者能使用不同的積木任意的拼湊組合,完成所欲達成的外觀,且藉由調整該骨架單元1及翼片21的組裝方式而調整機翼單元2的大小及位置,使滑翔時能提供足夠的浮升力使飛行積木組合飛行,故確實能達成本發明之目的。 In summary, the user can use any patchwork combination of different building blocks to complete the desired appearance, and adjust the size and position of the wing unit 2 by adjusting the assembly manner of the skeleton unit 1 and the fins 21, It is indeed possible to achieve the object of the present invention by providing sufficient lifting force to allow the flying building blocks to fly when gliding.
惟以上所述者,僅為本發明之較佳實施例而已,當不能以此限定本發明實施之範圍,即大凡依本發明申請專利範圍及專利說明書內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內。 The above is only the preferred embodiment of the present invention, and the scope of the present invention is not limited thereto, that is, the simple equivalent changes and modifications made by the patent application scope and patent specification content of the present invention, All remain within the scope of the invention patent.
1‧‧‧骨架單元 1‧‧‧ skeleton unit
11‧‧‧幹骨積木 11‧‧‧Bone bone building blocks
12‧‧‧翼骨積木 12‧‧‧Spetal building blocks
13I‧‧‧十字連接積木 13I‧‧‧cross connecting blocks
14‧‧‧翼接積木 14‧‧‧ wing-connected blocks
2‧‧‧機翼單元 2‧‧‧wing unit
21‧‧‧翼片 21‧‧‧ wing
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TW103103533A TWI510274B (en) | 2014-01-29 | 2014-01-29 | Flight building blocks |
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CN2080862U (en) * | 1990-12-30 | 1991-07-17 | 丁森林 | Combined aeroplane toy |
TWM301081U (en) * | 2006-04-06 | 2006-11-21 | Yu-Chi Tsai | Novel combination for airframe, prow seat, and main wing rack of model plane |
IT1397748B1 (en) * | 2010-01-25 | 2013-01-24 | Vicentelli | ASSEMBLY OF CONSTRUCTIVE ELEMENTS FOR MODULAR GAMES BY MAGNETIC JOINT. |
CN201906466U (en) * | 2010-12-12 | 2011-07-27 | 上海谦毅儿童娱乐设备有限公司 | 3-dimensional children's educational building block capable of being assembled into model plane |
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