FIELD: aeronautical engineering. SUBSTANCE: compound helicopter includes landing gear, fuselage with wings and main rotors at their tips. Landing gear is secured on helicopter fuselage by means of four pylons which hold cargo-carrying member secured by means of detachable unit. Cargo-carrying member is made in form of platform or van provides with its own landing gear. Each pylon is provided with shock-absorber strut containing hydraulic chamber for change of working volume in chamber for equalizing clearances of helicopter landing gear and landing gear of cargo-carrying member. Main rotors are mounted under planes of wings for turning them to position causing pushing action on flying vehicle. EFFECT: enhanced reliability. 28 dwg
Title | Year | Author | Number |
---|---|---|---|
HEAVY HIGH-SPEED ROTARY-WING AIRCRAFT | 2016 |
|
RU2608122C1 |
AIRCRAFT ROCKET COMPLEX WITH UNMANNED ATTACK HELICOPTER-AIRPLANE | 2017 |
|
RU2674742C1 |
AEROMOBILE OF HOVER TAKE-OFF | 2017 |
|
RU2648937C1 |
MULTI-PURPOSE TWO-FUSELAGE HELICOPTER AIRCRAFT | 2017 |
|
RU2650258C1 |
HEAVY-DUTY MULTI-PROPELLER CONVERTER PLATE | 2012 |
|
RU2492112C1 |
HEAVY CONVERTIBLE ELECTRIC DRONE | 2013 |
|
RU2532672C1 |
MULTIPURPOSE HELICOPTER AIRPLANE WITH REMOTE CONTROL | 2008 |
|
RU2370414C1 |
ADAPTIVE AIRBORNE MISSILE SYSTEM | 2019 |
|
RU2720592C1 |
HIGH-SPEED HELICOPTER-AMPHIBIOUS AIRCRAFT | 2017 |
|
RU2655249C1 |
CRYOGENIC ELECTRICAL CONVERTIPLANE | 2013 |
|
RU2529568C1 |
Authors
Dates
1997-09-10—Published
1994-03-16—Filed