FIELD: weaponry.
SUBSTANCE: invention relates to arms, particularly to aircraft torpedoes. The proposed aircraft torpedo comprises an axisymmetric body accommodating explosive, compressed air cylinder and control system. The torpedo gas turbine engine runs on liquid propellant and incorporates an air intake, compressor and fuel tank connected to fuel pipeline. Air turbine is connected the gas turbine engine rotor for the gas turbine to be used as a propeller hydraulic engine for the torpedo to move submerged.
EFFECT: higher speed and accuracy of hitting.
6 cl, 6 dwg
| Title | Year | Author | Number |
|---|---|---|---|
| AVIATION TORPEDO | 2007 |
|
RU2345317C1 |
| AVIATION TORPEDO | 2007 |
|
RU2345316C1 |
| AIR BOMB WITH BIROTARY GAS TURBINE ENGINE | 2007 |
|
RU2347179C1 |
| AVIATION BOMB | 2007 |
|
RU2345318C1 |
| AIR BOMB | 2007 |
|
RU2347178C1 |
| TORPEDO | 2014 |
|
RU2571664C1 |
| NUCLEAR BOMB | 2011 |
|
RU2480706C2 |
| UNIVERSAL TORPEDO | 2012 |
|
RU2477448C1 |
| CRUISE MISSILE | 2007 |
|
RU2351888C1 |
| HYDROGEN BOMB | 2011 |
|
RU2477449C1 |
