JPH048472Y2 - - Google Patents
Info
- Publication number
- JPH048472Y2 JPH048472Y2 JP6488887U JP6488887U JPH048472Y2 JP H048472 Y2 JPH048472 Y2 JP H048472Y2 JP 6488887 U JP6488887 U JP 6488887U JP 6488887 U JP6488887 U JP 6488887U JP H048472 Y2 JPH048472 Y2 JP H048472Y2
- Authority
- JP
- Japan
- Prior art keywords
- band
- towing
- wing
- main rod
- advertising display
- 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
Links
- 230000002265 prevention Effects 0.000 claims description 9
- 239000004744 fabric Substances 0.000 description 5
- 238000005452 bending Methods 0.000 description 1
- 230000000694 effects Effects 0.000 description 1
- 238000005516 engineering process Methods 0.000 description 1
- 239000000463 material Substances 0.000 description 1
- 239000002184 metal Substances 0.000 description 1
- 238000005096 rolling process Methods 0.000 description 1
- 238000007665 sagging Methods 0.000 description 1
Landscapes
- Illuminated Signs And Luminous Advertising (AREA)
- Displays For Variable Information Using Movable Means (AREA)
Description
【考案の詳細な説明】
A 産業上の利用分野
本考案は航空機を利用して空中を曳航するに適
した広告表示体の改良に関する。[Detailed Description of the Invention] A. Field of Industrial Application The present invention relates to the improvement of an advertising display suitable for being towed in the air using an aircraft.
B 従来の技術
本出願人が先に開発した航空機を用いた広告装
置(実開昭59−53393号公報実公平2−14079号公
報参照)は、横桟と縦桟とを格子状に組み合わせ
た広告部材に多数のランプを等距離、等間隔に設
け、これら各ランプに対し、点滅用コンピユータ
によつて数字、アルフアベツトまたは片仮名等の
表示が行われるよう点滅するようにしたものであ
つた。B. Prior Art An advertising device using an aircraft (see Utility Model Application Publication No. 59-53393 and Publication No. 2-14079) which was previously developed by the present applicant is a combination of horizontal bars and vertical bars in a grid pattern. A large number of lamps were placed on the advertising member at equal distances and intervals, and a flashing computer caused each lamp to flash to display numbers, alphabets, katakana, etc.
C 考案が解決しようとする問題点
上記従来の技術によると、広告部材に格子状体
が用いられるので重量が重くなり、そのうえ該格
子状体が機体に直接支持されたことにより該機体
の振動と共振する。このため広告部材の長さが制
限され、表示可能な文字は6〜10字に限られるな
どの問題点があつた。また、表示体の真下では広
告は読めなかつた。C. Problems to be solved by the invention According to the above-mentioned conventional technology, since a grid-like body is used for the advertising member, the weight becomes heavy, and in addition, the grid-like body is directly supported on the aircraft body, which causes vibrations of the aircraft body. resonate. For this reason, there were problems such as the length of the advertising member was limited and the characters that could be displayed were limited to 6 to 10 characters. Also, advertisements could not be read directly below the display.
本考案は上記問題点を解決するものであつて、
前記格子状体に代えて可撓性の帯体を用いること
により広告表示体を長くでき、従つて、多くの文
字を表示でき、しかも、表示体の真下でも視認で
き、該帯体がはためいたり、垂れ下がることがな
く、水平状態を維持したまま曳航可能な広告表示
体を提供することを目的とする。 The present invention solves the above problems, and
By using a flexible strip instead of the grid, the advertising display can be made longer, and therefore more characters can be displayed, and it can be seen even directly below the display, and the strip can be folded. To provide an advertisement display body that can be towed while maintaining a horizontal state without bending or sagging.
D 問題点を解決するための手段
上記目的を達成するため本考案の構成は次の通
りとする。即ち、広告表示が付される可撓性帯体
と、該帯体の曳航方向前端に沿つて結着された主
杆と、該主杆に平行で前記帯体にその曳航方向に
間隔を存して結着された複数の副杆と、前記帯体
の前部上部に取り付けられ、長さ方向を前記帯体
の幅方向に沿わせた揺れ止め翼と、前記帯体の後
端に設けられて鉛直断面が曳航方向に開口するU
字状をなし、かつ、平面視で該帯体の曳航方向に
向いて直角又は、凹弧状とされた風受けを持つは
ためき防止部材とを含むことである。D. Means for solving the problems In order to achieve the above object, the structure of the present invention is as follows. That is, a flexible strip on which an advertising display is attached, a main rod tied along the front end of the strip in the towing direction, and a gap parallel to the main rod and on the strip in the towing direction. a plurality of sub-rods tied together; a swing prevention wing attached to the upper front part of the band whose length direction is along the width direction of the band; and a swing prevention wing provided at the rear end of the band. U whose vertical cross section opens in the towing direction
The present invention includes a flapping prevention member that is shaped like a letter and has a wind catch that is perpendicular or concave to the towing direction of the band in plan view.
E 作用
広告表示体は揺れ止め翼によつて水平状態に維
持され、主杆の後方に接続された帯体と、最後尾
に設けられたはためき防止部材とにより幅方向を
水平状態に保持したまま、空中を水平後方へ延展
され、帯体に貼着された文字布等によつて広告表
示される。E Function The advertising display body is maintained in a horizontal state by the anti-sway wings, and kept in a horizontal state in the width direction by the band connected to the rear of the main rod and the anti-flapping member provided at the rear end. , is extended horizontally backward through the air, and advertisements are displayed using letter cloth, etc. affixed to the band.
F 実施例
以下本考案を図面に示す一実施例に基づいて説
明する。F. Embodiment The present invention will be described below based on an embodiment shown in the drawings.
第1図に示すごとく、本考案の広告表示体は前
端(曳航方向前方端)に取り付けられた主杆1
と、該主杆に結合された複数の文字表示片13か
らなる帯体Aと、該帯体の前部上面に取り付けら
れた揺れ止め翼Bと、帯体の最後尾(曳航方向後
方端)に設けられたはためき防止部材14とを備
えている。 As shown in Figure 1, the advertising display of the present invention has a main rod 1 attached to the front end (front end in the towing direction).
, a band A consisting of a plurality of character display pieces 13 connected to the main rod, a swing prevention wing B attached to the front upper surface of the band, and the rear end of the band (rear end in the towing direction). A flapping prevention member 14 is provided.
しかして、前記主杆1は軽量のパイプよりな
り、その長さ方向複数箇所(実施例では4箇所)
に設けられた軽量金属製の留金4に係止されたロ
ープ3によつて航空機に曳航される。そして、該
主杆1には長さ方向に複数本(実施例では8本)
の主杆用テープ5が係合される。即ち、主杆テー
プ5は前端部および後端部が輪部とされ、前端輪
部が前記主杆1を挿通して係止されている。主杆
1は前記ロープ3が集束結着された集束環2、ワ
イヤ6および図示外の安全リング等を経て航空機
の尾部に設けられたフツクに接続される。主杆用
テープ5は主杆1に平行な連結テープ5aにより
互いが連結されている。 The main rod 1 is made of a lightweight pipe, and has multiple locations along its length (four locations in the embodiment).
The aircraft is towed to an aircraft by a rope 3 that is secured to a lightweight metal clasp 4 provided in the aircraft. The main rod 1 has a plurality of rods (eight rods in the example) in the length direction.
The main rod tape 5 is engaged. That is, the main rod tape 5 has ring portions at its front end and rear end, and the front end ring portion is inserted through the main rod 1 and locked therein. The main rod 1 is connected to a hook provided at the tail of the aircraft via a bundle ring 2 to which the rope 3 is bundled, a wire 6, a safety ring (not shown), and the like. The main rod tapes 5 are connected to each other by a connecting tape 5a parallel to the main rod 1.
主杆1に結着されたテープ5にはクリツプ11
と副杆12を介して文字表示片13が着脱可能に
連結される。そして、文字表示片13は前後方向
に長い複数本(図示では8本)のテープ13a
と、これらテープ列面上に透明基布(図示せず)
を介して貼着された文字布13bとからなる。即
ち、クリツプ11は第3図示のごとく針金が屈曲
されてなり、副杆12が挿入可能な環部11a
と、該環部の両側に形成されたテープ止め部11
bとからなる。前記環部11aに副杆12を挿通
して該副杆の長さ方向等間隔に複数(図示8個)
が環部11aの弾性復元力により固定される。前
側(第3図の左側)の止め部11bには前記主杆
用のテープ5の輪部が、後側(第3図の右側)に
は文字表示片用のテープ13aの輪部が係止され
る。このようにして、文字表示片13aは複数
(第1図示では10)が直列にクリツプ11と副杆
12を介して着脱自在に接続されて帯体Aを形成
する。 A clip 11 is attached to the tape 5 tied to the main rod 1.
A character display piece 13 is detachably connected to the sub-rod 12. The character display piece 13 is made up of a plurality of tapes 13a (eight tapes in the illustration) that are long in the front-rear direction.
and a transparent base fabric (not shown) on the surface of these tape rows.
It consists of a character cloth 13b attached via a letter cloth 13b. That is, the clip 11 is made of bent wire as shown in the third figure, and has a ring portion 11a into which the sub-rod 12 can be inserted.
and tape fixing parts 11 formed on both sides of the ring part.
It consists of b. The sub-rods 12 are inserted into the ring portion 11a, and a plurality of sub-rods (8 pieces shown) are inserted at equal intervals in the length direction of the sub-rods.
is fixed by the elastic restoring force of the ring portion 11a. The ring part of the tape 5 for the main rod is fixed to the stop part 11b on the front side (left side in FIG. 3), and the ring part of the tape 13a for the character display piece is fixed on the rear side (right side in FIG. 3). be done. In this way, a plurality of character display pieces 13a (10 in the first illustration) are detachably connected in series via the clips 11 and sub-rods 12 to form the band A.
揺れ止め翼Bは第1図および第5図のごとく、
水平翼7と、その長さ方向両端部に延設され上方
へα=45°の角度を有して反り、かつ、前縁がβ
=30°の角度で後退した反り翼8とからなり、前
記水平翼7がその長さ方向を前記帯体の幅方向に
沿わせてねじ等を介して主杆1に固定されてい
る。 The anti-sway wing B is as shown in Figures 1 and 5.
The horizontal wing 7 extends at both ends in the length direction, is curved upward at an angle of α=45°, and has a leading edge of β.
The horizontal blade 7 is fixed to the main rod 1 via a screw or the like with its length direction along the width direction of the band.
はためき防止部材14は第1,4図示のごとく
前記帯体Aの後方に前記クリツプ11と副杆12
を介して接続される。この部材14はクリツプ1
1に係止されたテープ14aと、該テープの後端
に接続された風受け14bとからなる。また、風
受け14bは平面視で前記帯体Aの曳航方向に向
いて凹弧状に曲げられるとともに、鉛直断面がU
字状をなし、その開口部分が前側に向くよう前記
テープ14aによつて保持される。 The flapping prevention member 14 is attached to the clip 11 and the secondary rod 12 at the rear of the band A as shown in the first and fourth figures.
connected via. This member 14 is the clip 1
1, and a wind receiver 14b connected to the rear end of the tape. Further, the wind catcher 14b is bent into a concave arc shape facing the towing direction of the band A in plan view, and has a vertical cross section of U.
It has a letter shape and is held by the tape 14a so that its opening faces toward the front.
以上において作動状態を説明する。広告表示体
は図示外の軽飛行機に曳航されるが、主杆1に固
定された揺れ止め部材Bの水平翼7によつて、該
帯体を含む広告表示体の重量相当の揚力が付与さ
れ、反り翼9により水平が保持されて横転するこ
となく前進する。前記反り翼8の反り角度αは広
告表示体の横転を防止可能な角度に設定され、ま
た、後退角度βは横滑り防止のための適正値とな
つている。また風受け14bは風を含んで膨ら
み、抵抗力を付与されて帯体Aのはためきが防止
される。また、前記風受け14bへの抵抗力は帯
体Aを水平後方になびかせるのに役立つ。そし
て、表示体は幅方向が水平状態を保つて曳航され
る。 The operating state will be explained above. The advertisement display body is towed by a light aircraft not shown, and the horizontal wings 7 of the anti-sway member B fixed to the main rod 1 provide lift force equivalent to the weight of the advertisement display body including the strip. , the warped wings 9 keep it horizontal and it moves forward without overturning. The warping angle α of the warping blade 8 is set to an angle that can prevent the advertisement display from rolling over, and the receding angle β is set to an appropriate value to prevent skidding. Further, the wind catcher 14b swells to contain the wind, and is given a resistance force to prevent the band A from flapping. Further, the resistance force applied to the wind catcher 14b serves to cause the band A to wave horizontally backward. Then, the display body is towed while keeping its width direction horizontal.
本実施例による帯体Aは約30mの長さまで可能
で、32文字まで表示ができる。また帯体Aは可撓
製のワイヤ6やロープ3を介して航空機に曳航さ
れるので、機体からの振動が伝わらず、帯体Aが
ぶれたり、はためくことがない。 The band A according to this embodiment can be up to about 30 m long and can display up to 32 characters. Furthermore, since the band A is towed by the aircraft via the flexible wire 6 and rope 3, vibrations from the aircraft body are not transmitted, and the band A does not shake or flap.
本考案の可撓製帯体Aとして、前記のほか、網
体や無孔のシート体なども適用される。 In addition to the above, net bodies, non-porous sheet bodies, etc. can also be used as the flexible band body A of the present invention.
G 考案の効果
本考案は以上のごとく広告表示が付される可撓
性帯体と、該帯体の曳航方向前端に幅方向に沿つ
て結着された主杆と、該主杆に平行で前記帯体に
その曳航方向に間隔を存して結着された複数の副
杆と、前記帯体の前部上面に取り付けられ、長さ
方向を前記帯体の幅方向に沿わせた揺れ止め翼
と、前記帯体の後端に設けられて鉛直断面が曳航
方向に開口するU字状をなし、かつ、平面視で該
帯体の曳航方向に向いて直角又は、凹弧状とされ
た風受けを持つはためき防止部材を含む。従つ
て、広告表示体の軽量化が可能でその分だけ長さ
を長くでき多くの文字を表示できる。また帯体は
水平状態で字が横になるような姿勢を保持したま
ま曳航されるので真下は勿論離れた位置からでも
広告文が解読できる。しかも本広告表示体は材料
費が安価で、更に軽飛行機を使えるので運行コス
トがヘリコプターに比べ大幅に安くなるなど多く
の効果を発揮する。G. Effects of the invention As described above, the present invention includes a flexible band on which an advertising display is attached, a main rod that is tied along the width direction to the front end of the band in the towing direction, and a main rod that is parallel to the main rod. a plurality of sub-rods tied to the band at intervals in the towing direction; and a sway stopper attached to the front upper surface of the band, the length direction of which is aligned with the width direction of the band. a wing, and a wind turbine which is provided at the rear end of the band and has a U-shape with a vertical cross section opening in the towing direction, and is perpendicular to the towing direction of the band or has a concave arc shape when viewed from above. It includes an anti-flapping member having a receiver. Therefore, the weight of the advertisement display body can be reduced, and the length can be increased accordingly, allowing more characters to be displayed. In addition, since the belt is towed horizontally with the letters lying on its side, the advertising text can be read not only directly below but also from a distance. Furthermore, this advertising display has many advantages, including low material costs and the ability to use light aircraft, making operating costs significantly lower than helicopters.
第1図は本考案の一実施例を示す底面図、第2
図はその要部拡大平面図、第3図は他の要部拡大
平面図、第4図ははためき防止部材の拡大正面
図、第5図は揺れ止め翼の拡大左側面図である。
1……主杆、2……集束環、3……ロープ、4
……留金、5……テープ、A……帯体、B……揺
れ止め翼、7……水平翼、8……反り翼、13…
…文字表示片、13a……テープ、13b……文
字布、14……はためき防止部材、14b……風
受け。
Fig. 1 is a bottom view showing one embodiment of the present invention;
3 is an enlarged plan view of another essential part, FIG. 4 is an enlarged front view of the flapping prevention member, and FIG. 5 is an enlarged left side view of the anti-sway wing. 1... Main rod, 2... Focusing ring, 3... Rope, 4
... Clasp, 5 ... Tape, A ... Band, B ... Anti-sway wing, 7 ... Horizontal wing, 8 ... Curved wing, 13 ...
...Character display piece, 13a...Tape, 13b...Character cloth, 14...Flapping prevention member, 14b...Wind catcher.
Claims (1)
曳航方向前端に幅方向に沿つて結着された主杆
と、該主杆に平行で前記帯体にその曳航方向に
間隔を存して結着された複数の副杆と、前記帯
体の前部上面に取り付けられ、長さ方向を前記
帯体の幅方向に沿わせた揺れ止め翼と、前記帯
体の後端に設けられて鉛直断面が曳航方向に開
口するU字状をなし、かつ、平面視で該帯体の
曳航方向に向いて直角又は、凹弧状とされた風
受けを持つはためき防止部材とを含むことを特
徴とする空中曳航用広告表示体。 (2) 前記可撓性帯体は、前記副杆とクリツプを介
して複数の表示片が曳航方向に直列に着脱自在
に接続されてなることを特徴とする実用新案登
録請求の範囲第1項記載の空中曳航用広告表示
体。 (3) 前記揺れ止め翼は、水平翼と、その長さ方向
両端部に延設され上方へ反り、かつ、前縁が後
退した反り翼とからなることを特徴とする実用
新案登録請求の範囲第1項記載の空中曳航用広
告表示体。[Claims for Utility Model Registration] (1) A flexible band with an advertising display attached, a main rod tied along the width direction to the front end of the band in the towing direction, and parallel to the main rod. a plurality of secondary rods connected to the belt body at intervals in the towing direction; and a swinging rod attached to the front upper surface of the belt body, the length direction of which is aligned with the width direction of the belt body. A stop wing is provided at the rear end of the band and has a U-shape with a vertical cross section opening in the towing direction, and has a right angle or a concave arc shape when viewed from above in the towing direction of the band. An advertising display for aerial towing, comprising a flapping prevention member having a wind catcher. (2) The flexible band includes a plurality of display pieces detachably connected in series in the towing direction via the secondary rod and the clip, Claim 1 of the Utility Model Registration Claim. Advertising display for aerial towing as described. (3) The scope of the utility model registration claim, characterized in that the anti-swaying wing consists of a horizontal wing and a warped wing that is extended at both longitudinal ends of the wing and is curved upward, and whose leading edge is receded. The advertising display for aerial towing as described in paragraph 1.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6488887U JPH048472Y2 (en) | 1987-04-28 | 1987-04-28 |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP6488887U JPH048472Y2 (en) | 1987-04-28 | 1987-04-28 |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS63173285U JPS63173285U (en) | 1988-11-10 |
| JPH048472Y2 true JPH048472Y2 (en) | 1992-03-03 |
Family
ID=30901457
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP6488887U Expired JPH048472Y2 (en) | 1987-04-28 | 1987-04-28 |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPH048472Y2 (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022062662A (en) * | 2020-10-08 | 2022-04-20 | 日鉄ソリューションズ株式会社 | Display device and display method |
-
1987
- 1987-04-28 JP JP6488887U patent/JPH048472Y2/ja not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JP2022062662A (en) * | 2020-10-08 | 2022-04-20 | 日鉄ソリューションズ株式会社 | Display device and display method |
Also Published As
| Publication number | Publication date |
|---|---|
| JPS63173285U (en) | 1988-11-10 |
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