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
GB18582/44A
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.)
ThyssenKrupp Budd Co
Original Assignee
Edward G Budd Manufacturing Co
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 Edward G Budd Manufacturing CofiledCriticalEdward G Budd Manufacturing Co
Publication of GB591499ApublicationCriticalpatent/GB591499A/en
591,499. Airfoils. BUDD MANUFACTURING CO., E. G. Sept. 28,1944, No. 18582. Convention date, March 6, 1943. [Class 4] An airfoil such as a wing shown in Figs. 1 and 13 is connected to a wing or fuselage section 23 through a bar 33 arranged transversely of span-wise extending stringers 26, to the ends of which are welded edges of stress transfer plates 37 secured at their other edges to bar 33 by projections 38 pressed into grooves 36 formed in the edges of the bar 33; wider re-inforcing plates 47 are welded over plates 37 and covered by the skin 25 which is welded to flanges 30 of the stringers 26. Bolts 35 secure the bar 33 to the section 23 ; apertures with detachable covers provide access to the boltheads.
GB18582/44A1943-03-061944-09-28Improvements in or relating to airfoils
ExpiredGB591499A
(en)