一种航空发动机清洗设备
By combining a lightweight, high-pressure resistant cylinder design with locking components, the problem of large size and complex operation of traditional aircraft engine cleaning equipment has been solved, achieving miniaturization, convenient operation, and strong adaptability of the equipment.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- TIANSHI RUIFENG AVIATION TECHNOLOGY (JIANGSU) CO LTD
- Filing Date
- 2025-07-02
- Publication Date
- 2026-07-17
AI Technical Summary
Traditional aircraft engine cleaning equipment is bulky and complex to operate, making it difficult to use in confined spaces or outdoor environments.
It features a lightweight, high-pressure resistant cylinder design, combined with locking components and a manual switch to simplify the operation process. It also uses a pressure relief valve to prevent overpressure, resulting in a compact and highly adaptable structure.
It achieves miniaturization, ease of operation, and strong adaptability, making it suitable for confined spaces and outdoor environments.
Smart Images
Figure CN224511468U_ABST
Abstract
Claims
1. An aircraft engine washing apparatus, characterized by: It includes a high-pressure resistant cylinder (1) and a cylinder cover (2). The high-pressure resistant cylinder (1) is provided with a locking component (3) for locking the cylinder cover (2). The cylinder cover (2) is equipped with a pressure charging connector (4) for charging high-pressure gas, a pressure relief valve (5) for discharging pressure, and a pipeline connector (6) for connecting a cleaning pipeline. The end of the pipeline connector (6) is connected to a manual switch (61).
2. An aircraft engine washing apparatus according to claim 1, wherein: The locking assembly (3) includes a hinge seat (31), a pin (32), a bent rod (33), and a locking bolt (34). The hinge seat (31) is fixedly connected to the side wall of the high-pressure resistant cylinder (1). Several hinge seats (31) are evenly arranged along the circumference of the high-pressure resistant cylinder (1). One end of the bent rod (33) is connected to the hinge seat (31) through the pin (32). The locking bolt (34) is connected to the end of the bent rod (33) away from the hinge seat (31). The bent rod (33) has a threaded hole through which the locking bolt (34) passes.
3. An aircraft engine washing apparatus as claimed in claim 1, wherein: The high-pressure resistant cylinder (1) and the cylinder cover (2) are both made of aluminum alloy. The internal working pressure of the high-pressure resistant cylinder (1) is 30-50 psi.