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
Application number
GB23548/30A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
UGO ABATE
Original Assignee
UGO ABATE
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.)
Filing date
Publication date
Application filed by UGO ABATEfiledCriticalUGO ABATE
Publication of GB366899ApublicationCriticalpatent/GB366899A/en
B64C1/00—Fuselages; Constructional features common to fuselages, wings, stabilising surfaces or the like
Landscapes
Engineering & Computer Science
(AREA)
Mechanical Engineering
(AREA)
Aviation & Aerospace Engineering
(AREA)
Preliminary Treatment Of Fibers
(AREA)
Superconductors And Manufacturing Methods Therefor
(AREA)
Electron Beam Exposure
(AREA)
Abstract
366,899. Aeroplane fuselages. ABATE, U. and BONOMI, V., 6, Via Gesu, Milan, Italy. Aug. 6, 1930, No. 23548. Convention date, Aug. 7, 1929. Void [Published under Sect. 91 of the Acts]. [Class 4.] Aeroplane fuselages at their major section are reinforced by four plates c .. f having large portions cut away so that they bridge the interior of the fuselage. The plates are positioned as shown in Fig. 1, the lower points m, n forming points of attachment for longitudinal and cross ties while the upper parts t, u, v, z are joined to plates.
GB23548/30A1929-08-071930-08-06Improvements in or relating to aeroplane structure
ExpiredGB366899A
(en)