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
GB1958118A
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.)
Societe des Moteurs Salmson
Original Assignee
Societe des Moteurs Salmson
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 Societe des Moteurs SalmsonfiledCriticalSociete des Moteurs Salmson
Publication of GB121465ApublicationCriticalpatent/GB121465A/en
121,465. Soc. des Moteurs Salmson, (SystÞme Canton UnnÚ). Dec. 12, 1917, [Convention date]. Framework.-A metal fitting for connecting together the wing spars and interplane struts of aeroplanes, comprising a member through which the spar a passes and to which it is secured by bolts b, and a socket c for the strut i, is provided with integral lugs i formed of metal plates bent over at their outer edges and provided with holes j adjacent these edges for the attachment of staywires. The pins f of the stay-wires g are received by lugs e formed by a metal plate folded and welded as shown. Further, the socket c is extended at k for the attachment of other stay-wires.
GB1958118A1917-12-121918-11-27An Improved Metal Fitting for Assembling Longitudinals and Uprights in Aeroplanes.
ExpiredGB121465A
(en)