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
GB19607/21A
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
Publication of GB173206ApublicationCriticalpatent/GB173206A/en
173,206. International All-Steel Aircraft Syndicate, Ltd. Dec. 18, 1920, [Convention date]. Drawings to Specification. Fuselages; planes, arrangement of.-A fuselage, of aerofoil construction, and cantilever wings are arranged so that the angle of incidence of the wings is greater than the angle of incidence of the fuselage. The tail plane may be above the chord of the wings. The contour of the fuselage may be similar to that of the wings. Reference has been directed by the Comptroller to Specification 148,891.
GB19607/21A1920-12-181921-07-21Improvements in aircraft
ExpiredGB173206A
(en)