FIELD: helicopters. SUBSTANCE: detachable external fuel tanks are located on sides of helicopter in upper portion above fuel tanks as close fuselage as possible, near helicopter of mass without disturbing the CG position of helicopter and ensuring minimum length of main pipe line. Location of tanks above main fuel tanks of helicopter reliable utilization of fuel by gravity without impairing observation for passengers and without increasing the overall dimensions of helicopter in width. EFFECT: increased flying range. 2 cl, 4 dwg
Title | Year | Author | Number |
---|---|---|---|
HELICOPTER FUSELAGE DETACHABLE FUEL TANKS | 1993 |
|
RU2072950C1 |
HELICOPTER | 2003 |
|
RU2248306C1 |
METHOD OF TRANSPORTATION OF MI-8 HELICOPTERS BY IL-76 AIRCRAFT AND RIGGING FOR PLACING AND MOORING THE HELICOPTERS ON IL-76 AIRCRAFT | 2005 |
|
RU2310584C2 |
METHOD OF TRANSPORTING Mi-8 HELICOPTER BY TRAILER AND EQUIPMENT FOR LOCATING AND LOCKING HELICOPTER FOR TRANSPORTATION | 2007 |
|
RU2347711C2 |
MULTI-PURPOSE HELICOPTER AND HELICOPTER FUEL SYSTEM | 2020 |
|
RU2752810C1 |
HELICOPTER FOR CRANE-ASSEMBLY WORK | 2007 |
|
RU2341410C1 |
UNIVERSAL GENERATING SET OF HEAT GAS FLOW ON TANK CHASSIS | 2004 |
|
RU2273816C1 |
ULTRA LOW MASS AIRPLANE | 2005 |
|
RU2336200C2 |
HELICOPTER-AEROSTAT COMPLEX | 1994 |
|
RU2104903C1 |
SHOCK-ABSORBER - HYDRAULICALLY OPERATED HOIST | 1998 |
|
RU2154594C2 |
Authors
Dates
1998-06-10—Published
1996-01-16—Filed