Disc type rotating knocking turbine engine based on kerosene

• Main Authors: GONG JISHUANG, TENG YULIN, HAN QIXIANG, ZHANG YINING
• Format: Patent
• Language: Chinese; English
• Published: 17.12.2019
• Subjects: AIR INTAKES FOR JET-PROPULSION PLANTS; BLASTING; COMBUSTION APPARATUS; COMBUSTION ENGINES; COMBUSTION PROCESSES; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS; GAS-TURBINE PLANTS; GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGHVELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS; HEATING; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS; LIGHTING; MECHANICAL ENGINEERING; WEAPONS

The invention provides a disc type rotating knocking turbine engine based on kerosene. The disc type rotating knocking turbine engine comprises an inner core body, an outer barrel body, a disc type end cover, a mixing isolation barrel, an oil spraying ring, an oil splashing ring and a swirler. A first gap is formed between the outer wall of the inner core body and the inner wall of the outer barrel body to serve as an air inflow passageway. A second gap is formed between the inner wall of the inner core body and the inner wall of the disc type end cover to serve as an annular combustion chamber. The oil spraying ring is provided with an axially-through hollow cavity and sleeves two sections of the inner core body in an embedded manner, a fuel inlet is formed in the side wall of the oil spraying ring, and an annular fuel cavity is formed in the oil spraying ring. The fuel inlet is connected with the air inflow passageway through the annular fuel cavity. A fuel storage tank is connectedwith the annular fuel cav