JPS6327031B2 - - Google Patents
Info
- Publication number
- JPS6327031B2 JPS6327031B2 JP8358886A JP8358886A JPS6327031B2 JP S6327031 B2 JPS6327031 B2 JP S6327031B2 JP 8358886 A JP8358886 A JP 8358886A JP 8358886 A JP8358886 A JP 8358886A JP S6327031 B2 JPS6327031 B2 JP S6327031B2
- Authority
- JP
- Japan
- Prior art keywords
- assembly
- paper
- synthetic resin
- frame members
- board
- 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
- 238000004519 manufacturing process Methods 0.000 claims description 11
- 229920003002 synthetic resin Polymers 0.000 claims description 11
- 239000000057 synthetic resin Substances 0.000 claims description 11
- 238000000034 method Methods 0.000 claims description 5
- 238000004026 adhesive bonding Methods 0.000 claims description 4
- 230000003014 reinforcing effect Effects 0.000 claims description 4
- 238000005452 bending Methods 0.000 claims description 2
- 230000001681 protective effect Effects 0.000 claims description 2
- 239000000853 adhesive Substances 0.000 description 4
- 230000001070 adhesive effect Effects 0.000 description 4
- 240000007182 Ochroma pyramidale Species 0.000 description 2
- 238000005520 cutting process Methods 0.000 description 2
- 238000010586 diagram Methods 0.000 description 2
- 230000000694 effects Effects 0.000 description 2
- 230000014759 maintenance of location Effects 0.000 description 2
- 239000000463 material Substances 0.000 description 2
- 239000002023 wood Substances 0.000 description 2
- 230000015572 biosynthetic process Effects 0.000 description 1
- 239000000470 constituent Substances 0.000 description 1
- 238000004080 punching Methods 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 230000035939 shock Effects 0.000 description 1
Landscapes
- Toys (AREA)
Description
【発明の詳細な説明】
本発明はバルサ材等で形成される骨組を有し、
エンジン及び受信機を搭載して無線操縦により飛
行する模型飛行機の製造方法に関するものであ
る。DETAILED DESCRIPTION OF THE INVENTION The present invention has a skeleton made of balsa wood or the like,
The present invention relates to a method of manufacturing a model airplane that is equipped with an engine and a receiver and flies by radio control.
従来の模型飛行機の製造方法は、例えば実開昭
49−120394号の公報で示されているように予め木
材製の骨組部材を接着剤で接着して骨組を形成
し、しかるのちこの骨組に外皮を貼り付けるよう
にしていた。しかしかかる方法だと骨組の組立作
業のほかに外皮の析り曲げ作業を別個に要し、し
かも骨組の接着剤が固まつて強度を発現するまで
外皮の貼り付け作業ができず、その結果製作工程
が複雑化し且つ製造時間も長くなるという問題が
あつた。更に骨組部材同志を接着する際には骨組
部材を位置決めしなければならず骨組の組立作業
体にも熟練を要するという問題があつた。 The conventional manufacturing method for model airplanes is, for example,
As disclosed in Japanese Patent No. 49-120394, a framework was formed by bonding wooden framework members with adhesive in advance, and then an outer skin was attached to the framework. However, with this method, in addition to the work of assembling the frame, it is necessary to separately bend and bend the outer skin, and furthermore, the work of pasting the outer skin cannot be done until the adhesive of the frame hardens and develops strength, resulting in fabrication. There were problems in that the process became complicated and the manufacturing time increased. Furthermore, when adhering the frame members to each other, the frame members must be positioned, and there is a problem in that the frame assembly workers also require skill.
本発明はかかる点に鑑みてなされたものであつ
て、その目的とするところは外皮として曲げ加工
が容易でしかも保形性を有するものを用い、骨組
部材の組立が容易で、しかも製造工程が簡略化で
きる無線操縦模型飛行機の製造方法を提供するに
ある。 The present invention has been made in view of these points, and its purpose is to use a material that is easy to bend and has shape retention properties as the outer skin, so that the assembly of the frame members is easy and the manufacturing process is easy. An object of the present invention is to provide a method for manufacturing a radio-controlled model airplane that can be simplified.
以下、本発明を図に示す飛行機の各構成部材の
うち胴体の実施例に基づいて詳述する。 DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS The present invention will be described in detail below based on an example of a fuselage among the constituent members of an airplane shown in the drawings.
第1図は本発明に使用する外皮である組立板A
の断面図である。この組立板Aは、第2図のよう
に発泡合成樹脂板1の表面に適宜截断面柄を印刷
した印刷紙2を接着し、更に印刷紙2の表面に合
成樹脂フイルム3を接着するとともに、発泡合成
樹脂板1の裏面に補強紙4を接着した構成となつ
ている。組立板Aは截断線5に沿つて切り取つて
組立体Bを形成する。そして組立体Bは極細線で
描いた中央線6が模型飛行機の胴体Cの中央部と
なるように組立体Bを湾曲させて胴体側部X,
X′を構成し、更に折曲線7,7′に沿つて略直角
に折曲させて胴部Cの底部Y,Y′を形成せしめ
る。底部Y,Y′は嵌合材8によつて一体的に接
合される。切欠き部10,10′はそれぞれ主翼
及び尾翼を嵌合接着して胴部Cと一体化するため
のものである。11はエンジン、12は操縦席用
の透明部分の切欠き、12′は操縦部透明体、1
4はプロペラである。 Figure 1 shows assembly plate A, which is the outer skin used in the present invention.
FIG. As shown in FIG. 2, this assembly board A is made by gluing a printed paper 2 on which a cut section pattern is appropriately printed on the surface of a foamed synthetic resin board 1, and then gluing a synthetic resin film 3 to the surface of the printed paper 2, as shown in FIG. It has a structure in which reinforcing paper 4 is adhered to the back surface of a foamed synthetic resin board 1. Assembly plate A is cut along cutting line 5 to form assembly B. Then, the assembly B is made by curving the assembly B so that the center line 6 drawn with a very thin line becomes the center part of the fuselage C of the model airplane, and the fuselage side parts X,
X' is formed, and further bent at a substantially right angle along folding lines 7, 7' to form bottom parts Y, Y' of the body C. The bottom portions Y and Y' are integrally joined by a fitting material 8. The notches 10 and 10' are for fitting and bonding the main wing and the tail to integrate with the body C, respectively. 11 is the engine, 12 is the cutout of the transparent part for the cockpit, 12' is the transparent body of the control part, 1
4 is a propeller.
第4図は同上の組立工程を示す図である。同図
aは組立体Bを裏返した状態を示してあり折曲部
には断面V字形の折曲線7,7′を設けている。
同図bは組立体Cの裏面のうち胴体側部X,
X′にバルサ材等で形成した骨組部材16(側胴
15,15′及び木粋9,9′)を接着剤で接着し
た状態を示している。同図cは組立体Bを失印の
ように折曲線7,7′で折曲げて木粋9,9′にて
側胴15,15′同士を一体化して組立体Bの内
側に骨組Dを形成した図を示している。第4図は
胴体Cの完成図である。尚、組立体Bを折曲げた
のちに木粋9aを適宜補充してもよい。 FIG. 4 is a diagram showing the assembly process same as above. Figure a shows the assembly B turned upside down, and the bent portion is provided with folding lines 7 and 7' having a V-shaped cross section.
Figure b shows the fuselage side part X on the back side of the assembly C,
A frame member 16 (side shells 15, 15' and wood trims 9, 9') made of balsa wood or the like is bonded to X' with adhesive. Figure c shows assembly B bent at folding lines 7 and 7', and the side bodies 15 and 15' integrated at wooden lines 9 and 9', and the frame D is placed inside assembly B. The figure shows the formation of the . FIG. 4 is a completed view of the fuselage C. Incidentally, after the assembly B is bent, the wood grain 9a may be replenished as appropriate.
本発明は上述のように、組立板を印刷紙の印刷
に沿つて全体を切断して組立体を形成し、次にこ
の組立体の裏面に骨組部材を貼着し、しかるのち
組立体を適宜形状に折り曲げて必要個所を接着し
て組立体を組立てると同時に、組立体内に骨組部
材にて機体の骨組を形成するので、組立体を組立
てるとき、それにともなつて骨組部材も立体的に
骨組されることとなり、したがつて骨組部材を別
個に骨組みする手間が省け、製作工程が簡略化で
きるという効果を奏する。 As described above, in the present invention, an assembly is formed by cutting the entire assembly board along the printing paper, and then a frame member is attached to the back side of this assembly, and then the assembly is cut as appropriate. At the same time as the assembly is assembled by bending it into a shape and gluing the necessary parts, the frame of the aircraft is formed using the frame members within the assembly, so when assembling the assembly, the frame members are also assembled three-dimensionally. Therefore, it is possible to save the effort of separately assembling the frame members and to simplify the manufacturing process.
一方発.合成樹脂板の表面に適宜模様を印刷し
た印刷紙を貼着し、更に該印刷紙の表面に保護用
透明フイルムをラミネート加工するとともに、発
泡合成樹脂板の裏面には補強紙を貼着した組立板
を用いるので、従来のように外皮として用いられ
るフイルムに比べて組立体自体に保形性を有し、
したがつて組立体の組立てと同時に骨組部材を骨
組みした状態での位置決めが組立体によつてなさ
れることとなり組立作業の熟練はさほど要求され
ず、また骨組部材のみを先に組立てて接着する場
合に比べて骨組部材専用の保持手断を用いずに済
み、しかも組立精度が向上できる。更に組立体と
骨組部材の組立が同時におこなえるから骨組部材
へ接着する接着剤の強度の発現のための時間を置
く必要がなく製作時間が短縮化できるという効果
を奏する。更に組立体と骨組部材との接着はフラ
ツトな状態で行うことできて接着作業が容易にな
り組立体と骨組部材とがずれることがなくなると
いう効果を奏する。 From one side. An assembly in which printed paper with an appropriate pattern printed on it is pasted on the surface of a synthetic resin board, a protective transparent film is laminated on the surface of the printed paper, and reinforcing paper is pasted on the back side of the foamed synthetic resin board. Since a plate is used, the assembly itself has better shape retention than the conventional film used as the outer cover.
Therefore, the positioning of the frame members in the assembled state is done by the assembly at the same time as the assembly is assembled, and very skillful assembly work is not required. Compared to the above, it is not necessary to use a holding hand cut exclusively for the frame members, and assembly accuracy can be improved. Furthermore, since the assembly and the frame members can be assembled at the same time, there is no need to allow time for the adhesive bonded to the frame members to develop its strength, resulting in an effect that the manufacturing time can be shortened. Furthermore, the assembly and the frame member can be bonded together in a flat state, which facilitates the bonding work and prevents the assembly and the frame member from shifting.
また組立体は発泡合成樹脂板の両面に補強紙を
接着しているので、衝撃に充分耐えられるのは勿
論のこと、発泡合成樹脂板の厚みを4乃至5mmと
することによつて、模型飛行機のエンジンの振動
を吸収できて消音効果を有し飛行の安定性が図れ
る。 In addition, the assembly has reinforcing paper glued to both sides of the foamed synthetic resin board, so it can of course withstand shocks, and by making the foamed synthetic resin board 4 to 5 mm thick, it can be used for model airplanes. It can absorb engine vibrations, has a noise-muffling effect, and improves flight stability.
第1図は本発明の製造方法に用いる組立板の断
面図、第2図は同上の組立板に打ち抜き用印刷を
施した平面図、第3図は同上の飛行機の胴体の完
成図、第4図a,b,cは同上の製作工程を示す
図である。
1……発泡合成樹脂板、2……印刷紙、3……
合成樹脂フイルム、4……補強紙、16……骨組
部材、A……組立板、B……組立体。
Figure 1 is a cross-sectional view of the assembly board used in the manufacturing method of the present invention, Figure 2 is a plan view of the same assembly board printed for punching, Figure 3 is a completed view of the fuselage of the same airplane, and Figure 4 is Figures a, b, and c are diagrams showing the manufacturing process of the same. 1... Foamed synthetic resin board, 2... Printing paper, 3...
Synthetic resin film, 4... Reinforcement paper, 16... Frame member, A... Assembly board, B... Assembly.
Claims (1)
印刷紙を貼着し、更に該印刷紙の表面に保護用透
明フイルムをラミネート加工するとともに、発泡
合成樹脂板の裏面には補強紙を貼着した組立板を
用い、まず該組立板を印刷紙の印刷に沿つて全体
を切断して組立体を形成し、次にこの組立体の裏
面に骨組部材を貼着し、しかるのち組立体を適宜
形状に折り曲げて必要個所を接着して組立体を組
立てると同時に、組立体内に骨組部材にて機体の
骨組を形成することを特徴とする無線操縦模型飛
行機の製造方法。1 Paste printed paper with an appropriate pattern printed on the surface of a foamed synthetic resin board, further laminate a protective transparent film on the surface of the printed paper, and paste reinforcing paper on the back side of the foamed synthetic resin board. Using the assembled board, first cut the entire assembled board along the printing on the printing paper to form an assembly, then adhere the frame members to the back of this assembly, and then cut the assembly as appropriate. A method for manufacturing a radio-controlled model airplane, characterized by assembling an assembly by bending it into a shape and gluing necessary parts, and at the same time forming a frame of an aircraft body using frame members within the assembly.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8358886A JPS62240088A (en) | 1986-04-10 | 1986-04-10 | Production of radio wave operation type model airplane |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| JP8358886A JPS62240088A (en) | 1986-04-10 | 1986-04-10 | Production of radio wave operation type model airplane |
Publications (2)
| Publication Number | Publication Date |
|---|---|
| JPS62240088A JPS62240088A (en) | 1987-10-20 |
| JPS6327031B2 true JPS6327031B2 (en) | 1988-06-01 |
Family
ID=13806648
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| JP8358886A Granted JPS62240088A (en) | 1986-04-10 | 1986-04-10 | Production of radio wave operation type model airplane |
Country Status (1)
| Country | Link |
|---|---|
| JP (1) | JPS62240088A (en) |
Families Citing this family (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| JPH01305982A (en) * | 1988-06-03 | 1989-12-11 | Toshimitsu Takamatsu | Model plane and its manufacture |
-
1986
- 1986-04-10 JP JP8358886A patent/JPS62240088A/en active Granted
Also Published As
| Publication number | Publication date |
|---|---|
| JPS62240088A (en) | 1987-10-20 |
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