FIELD: transport.
SUBSTANCE: invention relates to aircraft engineering, particularly, to water bombers water intake systems. Water intake consists of the hatch at tank bottom, cylindrical manifold to house the pump, vertical shaft to engage the latter with the drive mechanism composed by sealed motor-driven conical gears, sliding carriage fitted in said vertical shaft with tight cover to allow water feed to said pump by means of levers and hydraulic cylinder. Water intake from pool into tank is performed at stay thereat via one hatch at tank bottom equipped with the pump driven by self-contained DC motor supplied from onboard storage batteries.
EFFECT: possibility of water intake from small pools.
6 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| FIREFIGHTING AIRCRAFT | 2010 |
|
RU2483981C2 |
| DEVICE FOR EXTINGUISHING FOREST FIRES | 2016 |
|
RU2642029C2 |
| HELICOPTER FIRE-FIGHTING PLANT | 1996 |
|
RU2097276C1 |
| AQUA AEROSPACE VEHICLE | 2012 |
|
RU2626418C2 |
| WATER BOMBER HELICOPTER | 2004 |
|
RU2347596C2 |
| EXTINGUISHING LIQUID TANK | 2020 |
|
RU2739020C1 |
| NON-FREEZING WATER INTAKE | 1992 |
|
RU2031674C1 |
| AIRCRAFT SYSTEM FOR DETECTION AND EXTINGUISHING OF FIRES AT INCIPIENT STAGE AND METHOD FOR ITS USE | 2017 |
|
RU2674640C1 |
| FIREPROOF HYDROPLANE | 1991 |
|
RU2028253C1 |
| DEVICE FOR THE AIR REMOVING FROM THE WATER-AIR JET, INCOMING WHILE THE WATER WITHDRAWAL AT THE AMPHIBIOUS AIRCRAFT GLIDING | 2015 |
|
RU2628632C2 |
