JP2965201B2 - Flying object - Google Patents
Flying objectInfo
- Publication number
- JP2965201B2 JP2965201B2 JP34578897A JP34578897A JP2965201B2 JP 2965201 B2 JP2965201 B2 JP 2965201B2 JP 34578897 A JP34578897 A JP 34578897A JP 34578897 A JP34578897 A JP 34578897A JP 2965201 B2 JP2965201 B2 JP 2965201B2
- Authority
- JP
- Japan
- Prior art keywords
- rotation mechanism
- attached
- drive device
- rotating
- flying
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired - Fee Related
Links
- 238000010586 diagram Methods 0.000 description 10
- 230000005540 biological transmission Effects 0.000 description 3
- 230000033001 locomotion Effects 0.000 description 2
- 238000004804 winding Methods 0.000 description 2
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
Landscapes
- Toys (AREA)
Description
【0001】[0001]
【発明の属する技術分野】本発明は飛行させて遊ぶこと
ができる鳥の形状をした飛行体に関する。BACKGROUND OF THE INVENTION 1. Field of the Invention The present invention relates to a bird-shaped flying object which can be played by flying.
【0002】[0002]
【従来の技術】従来、この種の飛行体は左右の羽根を上
下移動させる羽根上下移動機構が取付けられている。2. Description of the Related Art Conventionally, a flying body of this kind is provided with a blade vertical movement mechanism for vertically moving left and right blades.
【0003】[0003]
【発明が解決しようとする課題】従来の左右の羽根を上
下移動させる飛行体では、左右の羽根の形状を種々考え
ても下方と上方への移動時の空気抵抗がほぼ同じにな
り、揚力や推進力が得られないという欠点があった。In a conventional flying body in which the left and right blades are moved up and down, the air resistance when moving in the downward and upward directions is substantially the same even if the shapes of the left and right blades are considered in various ways. There was a drawback that propulsion could not be obtained.
【0004】本発明は以上のような従来の欠点に鑑み、
左右の翼を十分な揚力や推進力が得られるように動かし
て、長く飛行させて遊ぶことができる飛行体を提供する
ことを目的としている。The present invention has been made in view of the above-mentioned conventional drawbacks,
It is an object of the present invention to provide a flying object in which the left and right wings are moved so as to obtain sufficient lift and propulsion so that they can fly and play for a long time.
【0005】本発明の前記ならびにそのほかの目的と新
規な特徴は次の説明を添付図面と照らし合わせて読む
と、より完全に明らかになるであろう。ただし、図面は
もっぱら解説のためのものであって、本発明の技術的範
囲を限定するものではない。The above and other objects and novel features of the present invention will become more completely apparent when the following description is read in conjunction with the accompanying drawings. However, the drawings are for explanation only, and do not limit the technical scope of the present invention.
【0006】[0006]
【課題を解決するための手段】上記目的を達成するため
に、本発明は鳥の胴体形状に形成された飛行体本体と、
この飛行体本体の前部寄りの両側面に取付けられた左右
の翼の前部を回転させる前部回転機構、前記飛行体本体
の後部寄りの両側面に取付けられた左右の翼の後部を前
方が斜め上方となる8の字状あるいは楕円形状に回転さ
せる後部回転機構およびこの後部回転機構と前記前部回
転機構とを回転駆動させるように前記飛行体本体に取付
けられた駆動装置とからなる翼駆動装置と、この翼駆動
装置の前部回転機構に前部根元部が取付けられ、後部回
転機構に後部根元部が取付けられた左右の翼とで飛行体
を構成している。SUMMARY OF THE INVENTION In order to achieve the above object, the present invention provides an aircraft body formed in the shape of a bird's fuselage,
A front rotation mechanism for rotating the front of the left and right wings attached to the both sides near the front of the aircraft main body, and the rear of the left and right wings attached to both sides near the rear of the aircraft main body forward. A wing comprising a rear rotating mechanism for rotating the figure in a figure-eight or elliptical shape obliquely upward, and a driving device attached to the flying body so as to rotationally drive the rear rotating mechanism and the front rotating mechanism. A flying body is constituted by a driving device and left and right wings each having a front root portion attached to a front rotation mechanism of the wing driving device and a rear root portion attached to the rear rotation mechanism.
【0007】[0007]
【発明の実施の形態】以下、図面に示す実施の形態によ
り、本発明を詳細に説明する。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described below in detail with reference to the embodiments shown in the drawings.
【0008】図1ないし図9に示す本発明の第1の実施
の形態において、1は鳥の胴体形状に形成された飛行体
本体で、この飛行体本体1は軽量化を図るような軽い材
質を用いて形成されている。In the first embodiment of the present invention shown in FIGS. 1 to 9, reference numeral 1 denotes a flying body formed in the shape of a bird's body, and the flying body 1 is made of a light material to reduce the weight. It is formed using.
【0009】2は前記飛行体本体1に取付けられた翼駆
動装置で、この翼駆動装置2は前記飛行体本体1の前部
寄りの両側面に取付けられた左右の翼の前部を回転させ
る前部回転機構3と、前記飛行体本体1の後部寄りの両
側面に取付けられた左右の翼の後部を前方が斜め上方と
なる8の字形状に回転させる後部回転機構4と、この後
部回転機構4と前記前部回転機構3とを回転駆動させる
ように前記飛行体本体1に取付けられた駆動装置5とで
構成されている。Reference numeral 2 denotes a wing drive unit attached to the aircraft main body 1. The wing drive unit 2 rotates front portions of left and right wings attached to both side surfaces near the front of the aircraft body 1. A front rotation mechanism 3; a rear rotation mechanism 4 for rotating the rear portions of the left and right wings attached to both sides near the rear of the flying body 1 in a figure-eight shape with the front diagonally upward; It comprises a mechanism 4 and a drive unit 5 attached to the flying body 1 so as to rotate the front rotation mechanism 3.
【0010】前記前部回転機構3は前記飛行体本体1の
前部寄りの両側面部位に取付けられた軸受6、6に回転
可能に取付けられた前部回転軸7と、この前部回転軸7
の前記飛行体本体1の両側面より外方へ突出する両端部
に固定された回転アーム8、8とで構成されている。The front rotation mechanism 3 includes a front rotation shaft 7 rotatably mounted on bearings 6, 6 mounted on both sides of the body 1 near the front, and a front rotation shaft. 7
Rotating arms 8, 8 fixed to both ends protruding outward from both side surfaces of the flying body 1.
【0011】前記後部回転機構4は前記飛行体本体1の
後部寄りの両側面部位に取付けられた軸受9、9に回転
可能に取付けられた後部回転軸10と、この後部回転軸
10の前記飛行体本体1の両側面より外方へ突出する両
端部に固定された後部回転アーム11、11と、この後
部回転アーム11、11の先端部にそれぞれ回転可能に
取付けられた軸受12、12と、この軸受12、12に
それぞれスライド移動可能に取付けられた翼取付け部材
13、13とで構成されている。The rear rotating mechanism 4 includes a rear rotating shaft 10 rotatably mounted on bearings 9, 9 mounted on both side portions of the flying body 1 near the rear thereof, and the flight of the rear rotating shaft 10. Rear rotating arms 11, 11 fixed to both ends protruding outward from both side surfaces of the body main body 1, bearings 12, 12 rotatably attached to the distal ends of the rear rotating arms 11, 11, respectively; The wing mounting members 13, 13 are slidably mounted on the bearings 12, 12, respectively.
【0012】前記駆動装置5は前記前部回転軸7に固定
された傘歯車14と、この傘歯車14と噛み合うように
前記飛行体本体1に固定された軸受15に回転可能に取
付けられた駆動傘歯車16と、この駆動傘歯車16に固
定されたフック部材17に一端が係止され、他端が前記
飛行体本体1の尾翼18の先端部寄りの部位に回転可能
に取付けられた外側部にハンドル19が形成された係止
金具20に係止された輪ゴム21と、前記飛行体本体1
の尾翼18の根元近傍に取付けられた前記輪ゴム21の
ガイドローラー22と、前記前部回転軸7および後部回
転軸10にそれぞれ固定された前・後部歯車23、24
と、この前・後部歯車23、24間に介装された伝達歯
車25、26とで構成されている。The drive unit 5 is rotatably mounted on a bevel gear 14 fixed to the front rotary shaft 7 and a bearing 15 fixed to the flying body 1 so as to mesh with the bevel gear 14. One end is locked to a bevel gear 16 and a hook member 17 fixed to the drive bevel gear 16, and the other end is rotatably attached to a portion of the flying body 1 near the tip of the tail wing 18. A rubber band 21 locked to a lock fitting 20 having a handle 19 formed thereon, and the flying body 1
Guide rollers 22 of the rubber band 21 attached near the base of the tail fin 18 of the vehicle, and front and rear gears 23 and 24 fixed to the front rotation shaft 7 and the rear rotation shaft 10, respectively.
And transmission gears 25 and 26 interposed between the front and rear gears 23 and 24.
【0013】27、27は前記飛行体本体1の両側部に
取付けられる左右の翼で、この左右の翼27、27は前
後方向に弧状に曲げられ、前部の根元部は前記前部回転
機構3の回転アーム8、8の遊端部に枢支ピン28、2
8で枢支され、後部の根元部は前記後部回転機構4の翼
取付け部材13、13の一端部が固定されている。Reference numerals 27, 27 denote left and right wings attached to both sides of the flying object body 1. The left and right wings 27, 27 are bent in an arc in the front-rear direction. The pivot pins 28, 2 are attached to the free ends of the rotating arms 8,
At the base of the rear part, one end of the wing mounting members 13 of the rear rotation mechanism 4 is fixed.
【0014】上記飛行体34は左右の翼27、27を押
さえるとともに、駆動装置5のハンドル19を外方へ引
き出し、回転させて輪ゴム21をねじ曲げ、回転エネル
ギーを蓄える。輪ゴム21に十分な回転エネルギーが蓄
えられたところで、上空に向けて図9に示すように飛ば
すと、左右の翼27、27は翼駆動装置2の前部回転機
構3と後部回転機構4の回転により、図7及び図8に示
すように揚力や推進力が得られるように下部後方へ回動
した後、小さな抵抗しか受けないように前方上部へ回動
する。このため、鳥と同様に左右の翼27、27が回動
して、長く飛行することができる。The flying body 34 holds the left and right wings 27, 27, pulls the handle 19 of the drive unit 5 outward, rotates the rubber band 21 by twisting, and stores rotational energy. When sufficient rotational energy is stored in the rubber band 21, the wings 27, 27 are rotated toward the sky as shown in FIG. As a result, as shown in FIG. 7 and FIG. 8, the robot rotates backward and downward so that lift and propulsion are obtained, and then rotates forward and upward so as to receive only a small resistance. For this reason, the left and right wings 27, 27 rotate similarly to the bird, and can fly long.
【0015】[0015]
【発明の異なる実施の形態】次に、図10ないし図33
に示す本発明の異なる実施の形態につき説明する。な
お、これらの本発明の異なる実施の形態の説明に当っ
て、前記本発明の第1の実施の形態と同一構成部分には
同一符号を付して重複する説明を省略する。FIG. 10 to FIG.
Hereinafter, different embodiments of the present invention will be described. In the description of the different embodiments of the present invention, the same components as those of the first embodiment of the present invention are denoted by the same reference numerals, and duplicate description will be omitted.
【0016】図10ないし図18に示す本発明の第2の
実施の形態において、前記本発明の第1の実施の形態と
主に異なる点は、飛行体本体1の後部寄りの両側面部位
に前方が斜め上方となるガイド溝29、29を形成する
とともに、左右の翼27、27の後部に前記ガイド溝2
9、29に沿ってスライド移動するガイドピン30、3
0を用いた点と、一端部が飛行体本体1の前部寄りの部
位の係止片31に係止され、他端が尾翼18の先端部寄
りの部位に取付けられたローラー32を介して前部回転
軸7に取付けられた、外部より回転できる一方向にのみ
回転する機構を備えるゴム紐巻取りドラム33に固定さ
れた駆動装置5Aを用いた点で、このように構成された
飛行体34Aにしても、前記本発明の第1の実施の形態
と同様な作用効果が得られる。The second embodiment of the present invention shown in FIGS. 10 to 18 is different from the first embodiment of the present invention mainly in that both sides of the body 1 near the rear of the flying body 1 are provided. The guide grooves 29 are formed so that the front is obliquely upward, and the guide grooves 2 are formed at the rear of the left and right wings 27.
Guide pins 30, 3 sliding along 9, 29
0 and one end is locked by a locking piece 31 at a position near the front of the flying object main body 1, and the other end is via a roller 32 attached to a position near the tip of the tail unit 18. The flying object configured in this way is characterized by using a driving device 5A fixed to a rubber string winding drum 33 provided on the front rotation shaft 7 and having a mechanism that can rotate only in one direction that can be externally rotated. Even with 34A, the same operation and effect as those of the first embodiment of the present invention can be obtained.
【0017】図19ないし図25に示す本発明の第3の
実施の形態において、前記本発明の第1の実施の形態と
主に異なる点は、前部回転軸7に固定された歯車35
と、この歯車35と噛み合う後部回転軸10に固定され
た歯車36と、後部回転軸10を尾翼18の内側面に取
付けられたゴム風船状のエアータンク37からのエアー
の供給によって回転させるエアーモーター38とからな
る駆動装置5Bを用いた点で、このように構成された飛
行体34Bにしても、前記本発明の第1の実施の形態と
同様な作用効果が得られる。The third embodiment of the present invention shown in FIGS. 19 to 25 is mainly different from the first embodiment of the present invention in that a gear 35 fixed to the front rotating shaft 7 is used.
A gear 36 fixed to the rear rotating shaft 10 that meshes with the gear 35; and an air motor that rotates the rear rotating shaft 10 by supplying air from a rubber balloon-shaped air tank 37 attached to the inner surface of the tail fin 18. The same operational effects as those of the first embodiment of the present invention can be obtained in the flying body 34B configured as described above in that the driving device 5B including the driving device 38 is used.
【0018】図26ないし図31に示す本発明の第4の
実施の形態において、前記本発明の第2の実施の形態と
主に異なる点は、前方が斜め上方となる楕円形状のガイ
ド溝29A、29Aを形成した点と尾翼18の先端部寄
りの部位に垂直尾翼39を設けた点で、このように構成
した飛行体34Cにしても、前記本発明の第2の実施の
形態と同様な作用効果が得られるとともに、垂直尾翼3
9により水平方向の飛行をより安定させることができ
る。The fourth embodiment of the present invention shown in FIGS. 26 to 31 is mainly different from the second embodiment of the present invention in that an elliptical guide groove 29A whose front is obliquely upward. , 29A and the vertical tail 39 provided at a position near the tip of the tail 18 in the same manner as the second embodiment of the present invention in the flying vehicle 34C configured as described above. The function and effect can be obtained, and the vertical tail 3
9, the flight in the horizontal direction can be further stabilized.
【0019】図32および図33に示す本発明の第5の
実施の形態において、前記本発明の第1の実施の形態と
主に異なる点は、前記飛行体本体1に固定された軸受1
5に回転可能に取付けられた駆動傘歯車16をスイッチ
41をON状態にすることにより電池42からの電流に
より作動するモーター40を用いた点で、このように形
成された駆動装置5Cを用いて構成された飛行体34D
にしても、前記本発明の第1の実施の形態と同様な作用
効果が得られる。The fifth embodiment of the present invention shown in FIGS. 32 and 33 is different from the first embodiment of the present invention mainly in that a bearing 1 fixed to the flying body 1 is provided.
The drive device 5C thus formed is different from the drive device 5C in that the drive bevel gear 16 rotatably mounted on the switch 5 is driven by the current from the battery 42 by turning on the switch 41. The composed flying object 34D
In this case, the same operation and effect as those of the first embodiment of the present invention can be obtained.
【0020】[0020]
【発明の効果】以上の説明から明らかなように、本発明
にあっては次に列挙する効果が得られる。As apparent from the above description, the following effects can be obtained in the present invention.
【0021】(1)鳥の胴体形状に形成された飛行体本
体と、この飛行体本体の前部寄りの両側面に取付けられ
た左右の翼の前部を回転させる前部回転機構、前記飛行
体本体の後部寄りの両側面に取付けられた左右の翼の後
部を前方が斜め上方となる8の字状あるいは楕円形状に
回転させる後部回転機構およびこの後部回転機構と前記
前部回転機構とを回転駆動させるように前記飛行体本体
に取付けられた駆動装置とからなる翼駆動装置と、この
翼駆動装置の前部回転機構に前部根元部が取付けられ、
後部回転機構に後部根元部が取付けられた左右の翼とか
らなるので、翼駆動装置によって左右の翼を揚力や推進
力が得られるように下部後方へ回動させるとともに、抵
抗が小さくなるように斜め上方へ回動させることができ
る。したがって、十分な揚力や推進力が得られ、長く飛
行することができる。(1) A flying body formed in the shape of a bird's fuselage, and a front rotation mechanism for rotating the front parts of left and right wings attached to both sides near the front of the flying body. A rear rotation mechanism for rotating the rear parts of the left and right wings attached to both side surfaces near the rear part of the body in an eight-shaped or elliptical shape with the front obliquely upward, and the rear rotation mechanism and the front rotation mechanism A wing drive device comprising a drive device attached to the aircraft body so as to rotate and drive, and a front root portion attached to a front rotation mechanism of the wing drive device;
Since it consists of left and right wings with a rear root attached to the rear rotation mechanism, the wing drive device rotates the left and right wings backward and downward so that lift and propulsion can be obtained, and reduces resistance. It can be turned diagonally upward. Therefore, sufficient lift and propulsion are obtained, and a long flight is possible.
【0022】(2)前記(1)によって、左右の翼の前
部を回転させるとともに、後部を斜め上方に8の字ある
いは楕円形状となるように回転させるので、スムーズに
左右の翼を駆動させることができるとともに、騒音の発
生を防止でき、静かに飛行させることができる。(2) According to the above (1), the front portions of the left and right wings are rotated and the rear portion is rotated obliquely upward so as to form a figure 8 or an elliptical shape, so that the left and right wings are driven smoothly. And noise can be prevented, and the aircraft can fly quietly.
【0023】(3)前記(1)によって、左右の翼の駆
動に回転運動を用いるので、小さな駆動力でも左右の翼
を駆動させることができる。したがって、効率よく飛行
させることができる。(3) According to the above (1), since the left and right wings are driven by rotary motion, the left and right wings can be driven with a small driving force. Therefore, it is possible to fly efficiently.
【0024】(4)請求項2、3、4、5も前記(1)
〜(3)と同様な効果が得られる。(4) Claims 2, 3, 4, and 5 also have the above (1).
The same effects as in (3) can be obtained.
【図面の簡単な説明】[Brief description of the drawings]
【図1】本発明の第1の実施の形態の正面図。FIG. 1 is a front view of a first embodiment of the present invention.
【図2】本発明の第1の実施の形態の平面図。FIG. 2 is a plan view of the first embodiment of the present invention.
【図3】本発明の第1の実施の形態の要部断面図。FIG. 3 is a sectional view of a main part of the first embodiment of the present invention.
【図4】本発明の第1の実施の形態の駆動装置の説明
図。FIG. 4 is an explanatory diagram of a driving device according to the first embodiment of the present invention.
【図5】前後の回転アームを回動させた状態の説明図。FIG. 5 is an explanatory view of a state in which front and rear rotating arms are rotated.
【図6】本発明の第1の実施の形態の翼の回動状態を示
した説明図。FIG. 6 is an explanatory diagram showing a rotating state of the blade according to the first embodiment of the present invention.
【図7】本発明の第1の実施の形態の翼が下部後方へ回
動した状態の説明図。FIG. 7 is an explanatory view of a state in which the wing of the first embodiment of the present invention has rotated downward and rearward.
【図8】本発明の第1の実施の形態の翼が前方上部へ回
動した状態の説明図。FIG. 8 is an explanatory view of a state in which the wing of the first embodiment of the present invention has rotated to the upper front.
【図9】本発明の第1の実施の形態の使用状態を示した
説明図。FIG. 9 is an explanatory diagram showing a use state of the first embodiment of the present invention.
【図10】本発明の第2の実施の形態の正面図。FIG. 10 is a front view of a second embodiment of the present invention.
【図11】本発明の第2の実施の形態の平面図。FIG. 11 is a plan view of a second embodiment of the present invention.
【図12】本発明の第2の実施の形態の要部断面図。FIG. 12 is a sectional view of a main part according to a second embodiment of the present invention.
【図13】駆動装置のゴム紐を巻き取った状態の説明
図。FIG. 13 is an explanatory diagram of a state where a rubber cord of a driving device is wound up.
【図14】本発明の第2の実施の形態の駆動装置の駆動
状態の説明図。FIG. 14 is an explanatory diagram of a driving state of a driving device according to a second embodiment of the present invention.
【図15】本発明の第2の実施の形態の回転アームを回
動させた状態の説明図。FIG. 15 is an explanatory diagram illustrating a state where a rotary arm according to a second embodiment of the present invention is rotated.
【図16】本発明の第2の実施の形態の翼の回動状態を
示した説明図。FIG. 16 is an explanatory view showing a rotating state of a blade according to the second embodiment of the present invention.
【図17】本発明の第2の実施の形態の翼が下部後方へ
回動した状態の説明図。FIG. 17 is an explanatory view of a state in which the wing of the second embodiment of the present invention has been pivoted rearward and downward.
【図18】本発明の第2の実施の形態の翼が前方上部へ
回動した状態の説明図。FIG. 18 is an explanatory view of a state in which the wing of the second embodiment of the present invention has been rotated forward and upward.
【図19】本発明の第3の実施の形態の平面図。FIG. 19 is a plan view of a third embodiment of the present invention.
【図20】本発明の第3の実施の形態の要部断面図。FIG. 20 is an essential part cross-sectional view of the third embodiment of the present invention.
【図21】本発明の第3の実施の形態の駆動装置の説明
図。FIG. 21 is an explanatory diagram of a driving device according to a third embodiment of the present invention.
【図22】前後の回転アームを回動させた状態の説明
図。FIG. 22 is an explanatory diagram of a state in which front and rear rotating arms are rotated.
【図23】本発明の第3の実施の形態の翼の回動状態を
示した説明図。FIG. 23 is an explanatory view showing a rotating state of the blade according to the third embodiment of the present invention.
【図24】本発明の第3の実施の形態の翼が下部後方へ
回動した状態の説明図。FIG. 24 is an explanatory view of a state in which the wing of the third embodiment of the present invention has rotated downward and rearward.
【図25】本発明の第3の実施の形態の翼が前方上部へ
回動した状態の説明図。FIG. 25 is an explanatory diagram of a state in which the wing of the third embodiment of the present invention has been rotated forward and upward.
【図26】本発明の第4の実施の形態の平面図。FIG. 26 is a plan view of a fourth embodiment of the present invention.
【図27】本発明の第4の実施の形態の要部断面図。FIG. 27 is a sectional view of a main part of a fourth embodiment of the present invention.
【図28】本発明の第4の実施の形態の楕円形状のガイ
ド溝を示した説明図。FIG. 28 is an explanatory view showing an elliptical guide groove according to the fourth embodiment of the present invention.
【図29】本発明の第4の実施の形態の翼の回動状態を
示した説明図。FIG. 29 is an explanatory diagram showing a rotating state of the blade according to the fourth embodiment of the present invention.
【図30】本発明の第4の実施の形態の翼が下部後方へ
回動した状態の説明図。FIG. 30 is an explanatory view of a state in which the wing of the fourth embodiment of the present invention has rotated downward and rearward.
【図31】本発明の第4の実施の形態の翼が前方上部へ
回動した状態の説明図。FIG. 31 is an explanatory view of a state in which the wing of the fourth embodiment of the present invention has been rotated forward and upward.
【図32】本発明の第5の実施の形態の平面図。FIG. 32 is a plan view of a fifth embodiment of the present invention.
【図33】本発明の第5の実施の形態の要部断面図。FIG. 33 is an essential part cross-sectional view of the fifth embodiment of the present invention.
1:飛行体本体、 2:翼駆動装置、3:前部回
転機構、 4:後部回転機構、5、5A、5B、5
C:駆動装置、6:軸受、 7:前部回転
軸、8:回転アーム、 9:軸受、10:後部回
転軸、 11:後部回転アーム、12:軸受、
13:翼取付け部材、14:傘歯車、
15:軸受、16:駆動傘歯車、 17:フック
部材、18:尾翼、 19:ハンドル、2
0:係止金具、 21:輪ゴム、22:ガイドロ
ーラー、 23:前部歯車、24:後部歯車、
25:伝達歯車、26:伝達歯車、 27:左右
の翼、28:枢支ピン、 29、29A:ガイド
溝、30:ガイドピン、 31:係止片、32:ロ
ーラー、 33:ゴム紐巻取りドラム、34、3
4A、34B、34C、34D:飛行体、35:歯車、
36:歯車、37:エアータンク、 3
8:エアーモーター、39:垂直尾翼、 40:
モーター、41:スイッチ、 42:電池。1: flying body 2: wing drive 3: front rotating mechanism 4: rear rotating mechanism: 5, 5A, 5B, 5
C: drive, 6: bearing, 7: front rotating shaft, 8: rotating arm, 9: bearing, 10: rear rotating shaft, 11: rear rotating arm, 12: bearing,
13: wing mounting member, 14: bevel gear,
15: Bearing, 16: Drive bevel gear, 17: Hook member, 18: Tail, 19: Handle, 2
0: locking metal fittings, 21: rubber band, 22: guide roller, 23: front gear, 24: rear gear,
25: transmission gear, 26: transmission gear, 27: left and right wings, 28: pivot pin, 29, 29A: guide groove, 30: guide pin, 31: locking piece, 32: roller, 33: rubber cord winding Drums, 34, 3
4A, 34B, 34C, 34D: flying object, 35: gear,
36: gear, 37: air tank, 3
8: Air motor, 39: Vertical tail, 40:
Motor, 41: switch, 42: battery.
Claims (5)
と、この飛行体本体の前部寄りの両側面に取付けられた
左右の翼の前部を回転させる前部回転機構、前記飛行体
本体の後部寄りの両側面に取付けられた左右の翼の後部
を前方が斜め上方となる8の字状あるいは楕円形状に回
転させる後部回転機構およびこの後部回転機構と前記前
部回転機構とを回転駆動させるように前記飛行体本体に
取付けられた駆動装置とからなる翼駆動装置と、この翼
駆動装置の前部回転機構に前部根元部が取付けられ、後
部回転機構に後部根元部が取付けられた左右の翼とから
なることを特徴とする飛行体。An aircraft body formed in the shape of a bird's fuselage, a front rotation mechanism for rotating front portions of left and right wings attached to both side surfaces near the front portion of the aircraft body, and the aircraft. A rear rotation mechanism for rotating the rear parts of the left and right wings attached to both side surfaces near the rear part of the main body in an eight-shaped or elliptical shape with the front obliquely upward, and rotating the rear rotation mechanism and the front rotation mechanism A wing drive device comprising a drive device attached to the aircraft body so as to be driven; a front root portion attached to a front rotation mechanism of the wing drive device; and a rear root portion attached to a rear rotation mechanism. A flying object comprising left and right wings.
と、この飛行体本体の前部寄りの両側面に取付けられた
左右の翼の前部を回転させる前部回転機構、前記飛行体
本体の後部寄りの両側面に取付けられた左右の翼の後部
を前方が斜め上方となる楕円形状に回転させる後部回転
機構およびこの後部回転機構と前記前部回転機構とを回
転駆動させるように前記飛行体に取付けられたゴム紐を
用いた駆動装置とからなる翼駆動装置と、この翼駆動装
置の前部回転機構に前部根元部が取付けられ、後部回転
機構に後部根元部が取付けられた前後方向に弧状に曲げ
られた左右の翼とからなることを特徴とする飛行体。2. A flying body which is formed in the shape of a bird's fuselage, a front rotating mechanism for rotating front parts of left and right wings attached to both side surfaces near the front part of the flying body, and the flying body. A rear rotation mechanism for rotating the rear portions of the left and right wings attached to both side surfaces near the rear portion of the main body in an elliptical shape in which the front is obliquely upward, and the rear rotation mechanism and the front rotation mechanism are rotationally driven. A wing drive device comprising a drive device using a rubber cord attached to a flying object, a front root portion was attached to a front rotation mechanism of the wing drive device, and a rear root portion was attached to a rear rotation mechanism. A flying object comprising left and right wings bent in an arc in the front-rear direction.
と、この飛行体本体の前部寄りの両側面に回転可能に取
付けられた前部回転軸に固定された前部回転アームとか
らなる左右の翼の前部を回転させる前部回転機構、前記
飛行体本体の後部寄りの両側面に回転可能に取付けられ
た後部回転軸に固定された後部回転アーム、この後部回
転アームの先端部に回転可能に取付けられた軸受、この
軸受にスライド移動可能に取付けられた翼取付け部材と
からなる後部回転機構およびこの後部回転機構の後部軸
と前記前部回転機構の前部軸とを回転駆動させる前記飛
行体本体に取付けられた駆動装置とからなる翼駆動装置
と、この翼駆動装置の前部回転機構の前部アームの先端
部に前部根元部が枢支され、後部回転機構の翼取付け部
材の一端部が後部根元部に取付けられた左右の翼とから
なることを特徴とする飛行体。3. A flying body formed in the shape of a bird's fuselage, and a front rotating arm fixed to a front rotating shaft rotatably mounted on both sides near the front of the flying body. A front rotation mechanism for rotating the front portions of the left and right wings, a rear rotation arm fixed to a rear rotation shaft rotatably mounted on both sides of the aircraft main body near the rear, and a front end of the rear rotation arm. And a wing mounting member slidably mounted on the bearing, a rear rotating mechanism, and a rear shaft of the rear rotating mechanism and a front shaft of the front rotating mechanism. A wing drive device comprising: a drive device attached to the flying object body; and a front root portion pivotally supported at a tip end of a front arm of a front rotation mechanism of the wing drive device; One end of the mounting member is at the base of the rear A flying object comprising left and right wings attached to a part.
と、この飛行体本体の前部寄りの両側面に取付けられた
左右の翼の前部を回転させる前部回転機構、前記飛行体
本体の後部寄りの両側面に形成された前方が斜め上方と
なるガイド溝および前記前部回転機構を回転駆動させる
ように前記飛行体本体に取付けられた駆動装置とからな
る翼駆動装置と、この翼駆動装置の前部回転機構に前部
根元部が回転可能に取付けられ、前記ガイド溝に後部根
元部がスライド移動可能に取付けられた左右の翼とから
なることを特徴とする飛行体。4. A flying body which is formed in the shape of a bird's fuselage, a front rotation mechanism for rotating front parts of left and right wings attached to both side surfaces near the front part of the flying body, and the flying body. A wing drive device comprising a guide groove formed on both side surfaces near the rear of the main body and having a front obliquely upward and a drive device attached to the flying body so as to rotationally drive the front rotation mechanism; A flying object comprising: a left and right wing having a front root portion rotatably mounted on a front rotation mechanism of a wing drive device and a rear root portion slidably mounted on the guide groove.
と、この飛行体本体の前部寄りの両側面に取付けられた
左右の翼の前部を回転させる前部回転機構、前記飛行体
本体の後部寄りの両側面に形成された前方が斜め上方と
なる楕円形状のガイド溝および前記前部回転機構を回転
駆動させるように前記飛行体本体に取付けられた駆動装
置とからなる翼駆動装置と、この翼駆動装置の前部回転
機構に前部根元部が回転可能に取付けられ、前記ガイド
溝に後部根元部がスライド移動可能に取付けられた左右
の翼とからなることを特徴とする飛行体。5. A flying body which is formed in the shape of a bird's fuselage, a front rotation mechanism for rotating front parts of left and right wings attached to both side surfaces near the front part of the flying body, and the flying body. A wing drive device comprising: an elliptical guide groove formed on both sides near the rear of the main body and having a front obliquely upward, and a drive device attached to the flying body so as to rotationally drive the front rotation mechanism. And a left and right wing having a front root portion rotatably mounted on the front rotation mechanism of the wing drive device and a rear root portion slidably mounted on the guide groove. body.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP34578897A JP2965201B2 (en) | 1997-12-01 | 1997-12-01 | Flying object |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP34578897A JP2965201B2 (en) | 1997-12-01 | 1997-12-01 | Flying object |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPH11156061A JPH11156061A (en) | 1999-06-15 |
| JP2965201B2 true JP2965201B2 (en) | 1999-10-18 |
Family
ID=18378989
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP34578897A Expired - Fee Related JP2965201B2 (en) | 1997-12-01 | 1997-12-01 | Flying object |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JP2965201B2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI580463B (en) * | 2016-01-20 | 2017-05-01 | Genius Toy Taiwan Co Ltd | Wings flying toys |
Families Citing this family (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| KR20040046628A (en) * | 2002-11-28 | 2004-06-05 | 이영범 | a remote control for aplaying flapping bug |
| JP4681062B2 (en) * | 2004-03-08 | 2011-05-11 | 三菱電機株式会社 | Floating body |
-
1997
- 1997-12-01 JP JP34578897A patent/JP2965201B2/en not_active Expired - Fee Related
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| TWI580463B (en) * | 2016-01-20 | 2017-05-01 | Genius Toy Taiwan Co Ltd | Wings flying toys |
Also Published As
| Publication number | Publication date |
|---|---|
| JPH11156061A (en) | 1999-06-15 |
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