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
GB1689218A
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.)
Fairey Aviation Co Ltd
Original Assignee
Fairey Aviation Co Ltd
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 Fairey Aviation Co LtdfiledCriticalFairey Aviation Co Ltd
Priority to GB1689218ApriorityCriticalpatent/GB125019A/en
Publication of GB125019ApublicationCriticalpatent/GB125019A/en
125,019. Fairey Aviation Co., and Fairey, C. R. Oct. 16, 1918. Framework.-The metal cheek plates a of aircraft wing-spar fittings are secured to the spar by hollow rivets c expanded over the curved edges e of holes in the plates.
GB1689218A1918-10-161918-10-16Improved Means of Securing Fittings to the Spars of Aircraft.
ExpiredGB125019A
(en)