Airplane surface protection film kits
IPC분류정보
국가/구분 |
United States(US) Patent
등록
|
국제특허분류(IPC7판) |
|
출원번호 |
US-0016309
(2004-12-18)
|
등록번호 |
US-7334759
(2008-02-26)
|
발명자
/ 주소 |
- Castillo,Francisco J.
- Castillo,Jeanne M.
|
출원인 / 주소 |
- Castillo,Francisco J.
- Castillo,Jeanne M.
|
대리인 / 주소 |
Law Offices of Michael N. Cohen, PC
|
인용정보 |
피인용 횟수 :
2 인용 특허 :
9 |
초록
▼
Described herein is a computer design-aided shield for exposed surfaces on aircraft, a method for manufacture, and kits derived from collections of shields, each kit appropriate for use on a single aircraft type. The shield is contemplated for first use on general and corporate aviation aircraft. Th
Described herein is a computer design-aided shield for exposed surfaces on aircraft, a method for manufacture, and kits derived from collections of shields, each kit appropriate for use on a single aircraft type. The shield is contemplated for first use on general and corporate aviation aircraft. The kits are designed for convenient distribution to private pilots, and easy use by them on their aircraft. The shields can be transparent, or can bear lettering or insignia.
대표청구항
▼
We claim: 1. A protective shield for the exposed surfaces of aircraft, comprising: a film element, form-fitted to correspond to a designated area of the surface of an aircraft, said area comprising an exposed surface of said aircraft; said film element being fixedly attachable to said designated ar
We claim: 1. A protective shield for the exposed surfaces of aircraft, comprising: a film element, form-fitted to correspond to a designated area of the surface of an aircraft, said area comprising an exposed surface of said aircraft; said film element being fixedly attachable to said designated area by attachment means on the back of said film element is comprised of a weather-resistant polymeric material that is at least 1 mm thick, capable of withstanding external forces experienced by aircraft during flight and is pre-cut using computer generated forms to ensure close fitting to said designated area of the surface of an aircraft. 2. The shield of claim 1, wherein said film element is transparent. 3. The shield of claim 1, wherein said film element comprises surface lettering or other surface design. 4. The shield of claim 1, wherein said attachment means are comprised of film adhesive. 5. The shield of claim 1, wherein said designated areas, include exposed areas on the Landing gear struts of said aircraft. 6. The shield of claim 1, wherein said designated areas include exposed areas on or attached to the wing of said aircraft. 7. The shield of claim 1, wherein said designated areas include exposed areas on or attached to the tail of said aircraft. 8. The shield of claim 1, wherein the designated areas include exposed areas on or attached to the fuselage of said aircraft. 9. A method for the production of protective shields of claim 1, comprising; Operation of a computerized program to generate forms to closely fit the parameters of designated areas of the exposed surface of an aircraft; iterating said operation as necessary to refine forms; cutting a polymeric film sheet pre-coated with adhesive backing to form shields corresponding to said forms, wherein said polymeric sheets comprise weather-resistant and element-resistant material. 10. The method of claim 9, wherein all said shields in any one kit are cut to fit surfaces of one specific aircraft type. 11. A kit for assembly and distribution of the protective shields of claim 1, comprising: a plurality of pre-cut film elements, cut from polymeric sheets, said film elements being form-fitted to designated areas of the surface of an aircraft, wherein said polymeric sheets comprise weather-resistant and element-resistant material; said film clement being fixedly attachable to said designated areas by attachment means on the back of each said shield. 12. The kit of claim 11, wherein all said shields in any one kit are cut to fit surfaces of one specific aircraft type.
이 특허에 인용된 특허 (9)
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Rawlings Diane C. ; Dull Dennis L., Appliques providing corrosion protection.
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Morita Yoshitsugu,JPX ; Furukawa Haruhiko,JPX ; Aso Takayuki,JPX, Coating material.
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Fronek Daniel R. ; Kryzer Timothy J.,BEX, Drag reduction article.
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Otsuji Atsuo,JPX ; Takuma Keisuke,JPX ; Suzuki Rihoko,JPX ; Urakami Tatsuhiro,JPX ; Motoshima Toshihiro,JPX ; Yamashita Wataru,JPX ; Yoshimura Tomomi,JPX ; Shibuya Atsushi,JPX ; Sakata Yoshihiro,JPX , Low-birefringent organic optical component and a spirobiindan polymer.
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Servanty Guy (Leguevin FRX) Obry Philippe (Beauzelle FRX), Method and device for manufacturing adhesive elements to be applied to a three-dimensional surface for the purpose of de.
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Keener, Steven G.; Byrd, Norman R., Method for coating faying surfaces of aluminum-alloy components and faying surfaces coated thereby.
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Steven G. Keener ; Norman R. Byrd, Method for coating faying surfaces of aluminum-alloy components and faying surfaces coated thereby.
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Wayde R. Schmidt ; Harry E. Eaton, Jr., Nanocomposite layered airfoil.
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Ogawa, Kazufumi; Mino, Norihisa; Soga, Mamoru, Transparent substrate and method of manufacturing the same.
이 특허를 인용한 특허 (2)
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McGuire, James E.; Strange, Andrew C., Erosion protection sleeve.
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Toews, Garold, Kit for modifying a strut of an aircraft with an aerodynamic cover.
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