FLYING VEHICLE LANDING GEAR SHOCK-ABSORBER

mechanical engineering; aeronautical engineering; construction of flying vehicle landing gear shock-absorbers. SUBSTANCE: shock-absorber has body with cover on which plunger with diaphragm and level indication tube are mounted. Rod provided with hollow needle is mounted inside body forming above-plu...

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Bibliographische Detailangaben
Hauptverfasser:	BOCHKAREV V.N, KOGAN A.JA
Format:	Patent
Sprache:	eng
Schlagworte:	AEROPLANES AIRCRAFT AVIATION BLASTING COSMONAUTICS ENGINEERING ELEMENTS AND UNITS GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVEFUNCTIONING OF MACHINES OR INSTALLATIONS HEATING HELICOPTERS LIGHTING MEANS FOR DAMPING VIBRATION MECHANICAL ENGINEERING PERFORMING OPERATIONS SHOCK-ABSORBERS SPRINGS THERMAL INSULATION IN GENERAL TRANSPORTING WEAPONS
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Beschreibung
Zusammenfassung:	mechanical engineering; aeronautical engineering; construction of flying vehicle landing gear shock-absorbers. SUBSTANCE: shock-absorber has body with cover on which plunger with diaphragm and level indication tube are mounted. Rod provided with hollow needle is mounted inside body forming above-plunger and under-plunger cavities. Level indication tube is provided with member having spherical outer surface and hole in its wall showing level of working fluid in shock-absorber in charging it. Level indicating tube is mounted coaxially relative to hollow needle for sliding in its cavity. Axle box is provided with through slots communicating the above-plunger cavity with cavity in needle. EFFECT: possibility of obtaining required level of fluid in filling the shock-absorber inclined from vertical position; enhanced reliability. 4 dwg