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
GB223819A
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 GB140545ApublicationCriticalpatent/GB140545A/en
F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
F01P—COOLING OF MACHINES OR ENGINES IN GENERAL; COOLING OF INTERNAL-COMBUSTION ENGINES
F01P3/00—Liquid cooling
F01P3/18—Arrangements or mounting of liquid-to-air heat-exchangers
Abstract
140,545. Soc. des Moteurs Salmson, (SystÞme Canton-UnnÚ). Feb. 6, 1918, [Convention date]. Propelling.-The radiators of aeroplane engines are supported upon elastic members such as rubber rings. Fig. 1 shows an annular tubular radiator having the rings e interposed between the plate d and the support g to take up vertical shocks, while the rings /, l take up axial shocks. The radiator is mounted upon the engine crankcase, and secured by a grooved cover-plate h.
GB223819A1918-02-061919-01-29Improvements in shock absorbers for airplane radiators
ExpiredGB140545A
(en)
Improvements in system of mounting of the fly-wheel on the shafts of thermic motors, and chiefly of multi-cylinder explosion engines for propelling land, sea, or aerial vehicles