CPC B64C1/06
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Fuselage Frames; Stringers; Longerons ; source: patbase
Patent class info:
- CPC B64C1/06 Frames; Stringers; Longerons; Fuselage sections
- CPC B64C1/061 {Frames}
- CPC B64C1/062 {specially adapted to absorb crash loads}
- CPC B64C1/063 {Folding or collapsing to reduce overall dimensions, e.g. foldable tail booms (folding or collapsing wings B64C 3/56)}
- CPC B64C1/064 {Stringers; Longerons}
- CPC B64C1/065 {Spars}
- CPC B64C1/066 {Interior liners}
- CPC B64C1/067 {comprising means for preventing icing or condensation conditions}
- CPC B64C1/068 {Fuselage sections}
- CPC B64C1/069 {Joining arrangements therefor}
- CPC B64C1/08 Geodetic or other open-frame structures
- CPC B64C1/061 {Frames}
Patents in category CPC B64C1/06
- Patent DE-1914-325537 (Filing date: 1914-02-26)
- Patent GB-1917-113467 (Inventors: Serge Vincent De Bolotoff, Filing date: 1917-02-17)
- Patent GB-1918-122710 (Inventors: Serge Vincent De Bolotoff, Filing date: 1918-02-05)
- Patent DE-1918-376071 (Filing date: 1918-09-27, Applicant firm: Dornier Metallbauten)
- Patent FR-1909-396231 (English title: Assembly methods for extra light parts, Filing date: 1908-11-13, Applicant firm: Société Anonyme de Construction d'Appareils Aériens)
- Patent GB-1909-27673 (English title: Hollow tubes in the construction of aeroplanes and other light apparatus, Inventors: Georges-Henri-Marius Canton • Pierre-Georges Unné, Supplementary to patent: Patent FR-1909-399591, Filing date: 1909-11-27)
- Patent FR-1913-446246.16546 (English title: Improvements in the means used in aeronautical construction and "architecture" (design), Inventors: Henri-Marie Coandă, Supplementary to patent: Patent FR-1911-446246, Filing date: 1911-12-16)
- Patent FR-1913-447825 (Inventors: Paul Rime-Bruneau, Filing date: 1912-08-30)
- Patent FR-1912-448726 (English title: Airplane fuselage assembly arrangement allowing for very rapid break-down and re-configuration of the constutuent elements, Inventors: Roger Sommer, Filing date: 1912-09-09)
- Patent FR-1913-451243 (Inventors: Louis Bachelier, Filing date: 1912-12-02)
- Patent GB-1913-17438 (Filing date: 1913-07-29)
- Patent GB-1913-17534 (Filing date: 1913-07-30)
- Patent DE-1916-372627 (English title: Tubular or hollow thin-gauge building elements, made of steel or light metal, for aircraft, Inventors: Claude Dornier, Filing date: 1916-09-01, Applicant firm: Dornier Metallbauten G. m. b. H.)
- Patent GB-1917-110798 (Inventors: Frank Ford Peregrine Walsh, Filing date: 1916-11-02)
- Patent FR-1917-492088.21606 (English title: Wood reinforcement system used for the construction of airplanes, and for all industrial uses, Inventors: Jean Salibon, Supplementary to patent: Patent FR-1916-492088, Filing date: 1917-07-21)
- Patent FR-1917-495840 (English title: Improvements to aeroplanes, Inventors: James Joseph Murray, Filing date: 1917-11-14)
- Patent GB-1918-120701 (English title: Structural elements and parts for aeroplanes, Filing date: 1918-05-23, Applicant firm: British Westinghouse Electric and Manufacturing Co.)
- Patent FR-1921-525360 (Inventors: Pierre-Casimir-Louis Claverie, Filing date: 1918-08-16)
- Patent US-1920-1340626 (English title: Metal fitting for connecting together certain structural members of an aeroplane, Inventors: Pierre-Jean-René Postel-Vinay, Filing date: 1918-12-19, Applicant firm: Moteurs Salmson)
- Patent NL-1919-5367 (English title: Wooden girder, Inventors: Walter George Tarrant, Filing date: 1919-03-12)
Enclosing categories | CPC B64C1/00 |
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Subcategories | CPC B64C1/065, CPC B64C1/068 |
Keywords | Fuselage |
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