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
GB2291721A
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.)
INTERNAT ALL STEEL AIRCRAFT SY
Original Assignee
INTERNAT ALL STEEL AIRCRAFT SY
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 INTERNAT ALL STEEL AIRCRAFT SYfiledCriticalINTERNAT ALL STEEL AIRCRAFT SY
Priority to GB2291721ApriorityCriticalpatent/GB192431A/en
Publication of GB192431ApublicationCriticalpatent/GB192431A/en
192,431. International All-Steel Aircraft Syndicate, Ltd., and Bolas, H. Aug. 30, 1921. Addition to 173,206. Drawings to Specification. Fuselages; planes, construction of.-In an aircraft as claimed in the parent Specification, the longitudinal sections of the body progressively increase in angle of incidence from the centre line to the edges of the body, which is usually coincident with edges of the planes. The leading edge of the aerofoil-section fuselage, or the trailing edge, or both, may be straight.
GB2291721A1921-08-301921-08-30Improvements in aircraft
ExpiredGB192431A
(en)