KR960021083A - Fuselage skin for model aircraft and its manufacturing method - Google Patents

Fuselage skin for model aircraft and its manufacturing method Download PDF

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Publication number
KR960021083A
KR960021083A KR1019940032873A KR19940032873A KR960021083A KR 960021083 A KR960021083 A KR 960021083A KR 1019940032873 A KR1019940032873 A KR 1019940032873A KR 19940032873 A KR19940032873 A KR 19940032873A KR 960021083 A KR960021083 A KR 960021083A
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KR
South Korea
Prior art keywords
fuselage skin
film layer
balsa wood
model airplane
skin
Prior art date
Application number
KR1019940032873A
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Korean (ko)
Other versions
KR0134257B1 (en
Inventor
김형오
Original Assignee
하재기
주식회사 일 산
Priority date (The priority date 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 date listed.)
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Publication date
Application filed by 하재기, 주식회사 일 산 filed Critical 하재기
Priority to KR1019940032873A priority Critical patent/KR0134257B1/en
Publication of KR960021083A publication Critical patent/KR960021083A/en
Application granted granted Critical
Publication of KR0134257B1 publication Critical patent/KR0134257B1/en

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Classifications

    • AHUMAN NECESSITIES
    • A63SPORTS; GAMES; AMUSEMENTS
    • A63HTOYS, e.g. TOPS, DOLLS, HOOPS OR BUILDING BLOCKS
    • A63H27/00Toy aircraft; Other flying toys

Abstract

가. 청구범위에 기재된 발명이 속한 기술분야end. The technical field to which the invention described in the claims belongs

모형비행기용 동체 스킨(skin).Fuselage skin for model airplanes.

나. 발명이 해결하려고 하는 기술적 과제I. The technical problem that the invention is trying to solve

모형 비행기용 동체 스킨(skin)의 곡면가공성을 용이하게 하면서 경량화와 내구성 증대를 기하고, 보수유지상의 편익제공 및 표면디자인 작업의 불편등을 일소코져 하는 것이다.It is designed to reduce the weight and durability of the fuselage skin of the model airplane, and to provide convenience in maintenance and inconvenience of surface design work.

다. 발명의 해결방법의 요지All. Summary of Solution of the Invention

모형비행기용 동체 스킨(1)을 발사나무(2)를 주재로 하여 이들을 상호 에폭시 계열의 수지층(3)으로 접착시키고, 필요에 따라서는 발사나무(2) 상간에는 내구성 증대를 위하여 화이버글라스(9) 또는 카아본화이버(10)등을 적층삽입할수 있도록 하였으며, 발사나무(2) 표면에는 다양한 디자인이 배하여진 인쇄필름층(4)과 폴리에스텔필름층(5)을 순차적으로 중찹한 후 열압착성형으로 견고히 성형하되, 동체 스킨(1)의 곡면부도 동시에 밴딩성형이 될수 있도록 한 것이다.The fuselage skin (1) for model airplanes is bonded to each other by balsa wood (2), and is bonded to each other by epoxy resin layer (3). If necessary, fiberglass ( 9) Or carbon fiber (10), etc. can be laminated and inserted, and the heat of the firing wood (2) after the center of the print film layer (4) and polyester film layer (5) with various designs are sequentially stacked Molded by compression molding, but the curved portion of the body skin (1) is to be a banding molding at the same time.

라. 발명의 중요한 용도la. Important uses of the invention

모형비행기용 동체 스킨Fuselage Skin for Model Airplanes

Description

모형비행기용 동체 스킨(skin) 및 그 제조방법Fuselage skin for model aircraft and its manufacturing method

본 내용은 요부공개 건이므로 전문내용을 수록하지 않았음As this is a public information case, the full text was not included.

제1도는 본 발명의 바람직한 동체 스킨의 일실시예를 보인 사시도,1 is a perspective view showing an embodiment of a preferred fuselage skin of the present invention,

제2도는 본 발명의 제조공정을 보인 단면도.2 is a cross-sectional view showing a manufacturing process of the present invention.

Claims (4)

모형비행기용 동체 스킨(1)을 제조함에 있어서; 상기 동체 스킨(1)은 발사나무(2)를 에폭시 계열의 수지층(3)으로 이중적층한 후, 인쇄용 필름층(4), 폴리에스텔 필름층(5)을 순차적으로 적층하여 금형(7)상에 안치시켜 소정형의 지그(8)로서 열압착성형하여, 이들 구성부재를 접착 및 밴딩성형되도록 한 것을 특징으로 하는 모형비행기용 동체 스킨(skin)의 제조방법.In the manufacture of a fuselage skin 1 for a model airplane; The fuselage skin (1) is a laminate of balsa wood (2) with an epoxy-based resin layer (3), and then laminated with a printing film layer (4) and a polyester film layer (5) in a mold (7) A method for manufacturing a fuselage skin for a model airplane, characterized in that the sheet is thermocompression-molded as a jig (8) of a predetermined type so as to bond and band these components. 모형비행기용 동체 스킨(1)을 구성함에 있어서; 상기 동체 스킨(1)은 주재를 발사나무(2)로 하고, 상기한 발사나무(2)는 이중으로 중첩구성하되, 상호 에폭시계열의 수지층(3)으로서 상호 접착구성되고, 발사나무(2) 상면부에는 다양한 디자인이 배하여진 인쇄필름층(4)과 폴리에스텔 필름층(5)을 순차적으로 접착구성한 것을 특징으로 하는 모형비행기용 동체 스킨(skin).In constructing a fuselage skin 1 for a model airplane; The fuselage skin (1) is the main material of the balsa wood (2), the balsa wood (2) is a double overlapping configuration, mutually adhesive composition as a resin layer (3) of mutual epoxy series, balsa wood (2) ) The fuselage skin for a model airplane, characterized in that the upper surface portion is formed by sequentially bonding the print film layer 4 and the polyester film layer 5, which have various designs. 제2항에 있어서; 상기한 발사나무(2) 상간에는 화이버 글라스(9)를 적층삽입한 것을 특징으로 하는 모형 비행기용 동체 스킨(skin).The method of claim 2; A fuselage skin for a model airplane, characterized in that a fiberglass (9) is laminated and inserted between the balsa wood (2). 제2항에 있어서; 상기한 발사나무(2) 상간에는 카아본 화이버(10)를 적층삽입한 것을 특징으로 하는 모형 비행기용 동체 스킨(skin).The method of claim 2; The fuselage skin for a model airplane, characterized in that the carbon fiber (10) is laminated and inserted between the balsa wood (2). ※ 참고사항 : 최초출원 내용에 의하여 공개하는 것임.※ Note: The disclosure is based on the initial application.
KR1019940032873A 1994-12-01 1994-12-01 The fuselage skin of model aircraft and the manufacturing method KR0134257B1 (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
KR1019940032873A KR0134257B1 (en) 1994-12-01 1994-12-01 The fuselage skin of model aircraft and the manufacturing method

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
KR1019940032873A KR0134257B1 (en) 1994-12-01 1994-12-01 The fuselage skin of model aircraft and the manufacturing method

Publications (2)

Publication Number Publication Date
KR960021083A true KR960021083A (en) 1996-07-18
KR0134257B1 KR0134257B1 (en) 1998-04-24

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Family Applications (1)

Application Number Title Priority Date Filing Date
KR1019940032873A KR0134257B1 (en) 1994-12-01 1994-12-01 The fuselage skin of model aircraft and the manufacturing method

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KR (1) KR0134257B1 (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113998112A (en) * 2021-11-23 2022-02-01 河北悟科智能科技有限责任公司 Flying wing unit

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN113998112A (en) * 2021-11-23 2022-02-01 河北悟科智能科技有限责任公司 Flying wing unit

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Publication number Publication date
KR0134257B1 (en) 1998-04-24

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