Wright aircraft engines; complete instructions for their installation, operation and maintenance; (1921)
Wright Aeronautical Corporation, Cautley, John R., ed · Paterson, N.J., Wright aeronautical corporation · leaf 85
End ClearanceVanes in b.001 Min..002 desired.003 Max. End Clearance in Shaft .OOlMm. .004 Loose desired .007Max. Oil pump and release valve fits for Models E and I .0005Loose desired.001 Max. End clearance Total f~\of assembly.004 Min..008 desired Key Top Clearance 002 C/earonce O08 Clearance… … 0002 Mm Loose■001 desired00Z Max.Loose 0005 Tight Min..0015 Tight desired0025 Tiaht Max. Fits and tolerances for magneto drive parts, Models E. I, H and H-2 WRIGHT AERONAUTICAL ENGINES 63 separate the vanes should have approximately the samedegree of tension. The efficiency of this type of pump…
Airplanes
Internet Archive · Library of Congress · Public Domain Mark 1.0. Free to use for anything.
