| 摘要 |
<p>An aircraft pipeline wheel gas engine is provided with a rotary pipeline burning power wheel (17). The burning power wheel (17) is formed by a burning power wheel disc (18) and a flame gas pipe (20). The burning power wheel disc (18) is connected to a transmission shaft (5) of a rotor. A front portion of the flame gas pipe (20) is wound and fixed on the burning power wheel (17) along a running direction of the burning power wheel (17) from front to back along an axial direction of the burning power wheel (17). A rear portion of the flame gas pipe (20), close to an outlet part of the flame gas pipe, is bent against the running direction of the burning power wheel (17) and is arranged on the burning power wheel (17) along a tangential direction. A direction of an outlet (22) of the flame gas pipe is opposite to a rotating tangential direction of the burning power wheel (17). The outlet (22) of the flame gas pipe is communicated with an exhaust passage (3) of an engine. An inlet (21) of the flame gas pipe is communicated with a reversing and reduction air pipe (11) of an air pipe wheel. A discharge hole (26) of a fuel storage tank is communicated with an admission passage (2) of the engine. The aircraft pipeline wheel gas engine has a simple structure and a wide application range and can meet the use requirements in multiple special situations.</p> |
