| 摘要 |
aeronautical engineering; fuel systems of special heavy aircraft. SUBSTANCE: fuel tank has shell with front and rear end heads, fuel intake device and rotary knife. Hydrocarbon polymer material in form of tape is used as fuel. Tape is located in cassettes. Fuel intake device is located between cylinder of knife and intermediate casing surrounding it. Low-molecular hydrocarbon gas generator is mounted inside tank. EFFECT: enhanced explosion proofness and fire safety in emergency situations. 6 cl, 9 dwg
|
