Device for Filling Aircraft Landing Gear Shock Struts with Hydraulic Fluid,

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Abstract:

A microfiche of the abstract contains graphic information about filling aeroplane shock absorbers with hydraulic fluid. The device consists of a conduit along which liquid flows from the tank to the shock absorber pillar with a pump and its conduit connected to a source of compressed air. The new device increases the accuracy of the dose during the filling action, and saves the unnecessary time spent during the filling. The dosing device is mounted in the liquid conduit and cooperates with a two position hydraulic switch. Author

Author(s):
Rips, L. D. ; Shcheglovitov, A. A. ; Borisov, M. F.
Author Organization(s):
FOREIGN TECHNOLOGY DIV WRIGHT-PATTERSON AFB OHIO
Supplementary Note:
Edited trans. of Patent (USSR) 265 731 p1-2 1970, by Charles T. Ostertag.
Annotation:
Device for Filling Aircraft Landing Gear Shock Struts with Hydraulic Fluid--Translation.
Pagination:
0007

Security Markings

DOCUMENT & CONTEXTUAL SUMMARY

Distribution:
Approved For Public Release

RECORD

Collection: TR
Identifying Numbers
Report Number(s):
FTD-HT-23-359-72
Project Number(s):
AF-7343
 Subject Terms
Communities of Interest:
Air Platforms
Descriptor(s):
(*HYDRAULIC EQUIPMENT, MAINTENANCE), (*LANDING GEAR, HYDRAULIC EQUIPMENT), HYDRAULIC FLUIDS, AIRCRAFT EQUIPMENT, SHOCK ABSORBERS, PATENTS, FILLING, USSR
Field(s)/Group(s):
Aircraft, Hydraulic and Pneumatic Equipment
Keyword(s):
TRANSLATIONS
Report Date:
1972 Mar 27