The invention relates to the technical field of turbojet engine stator casing installation auxiliary tools, and discloses a low-thrust turbojet engine installation structure. The low-thrust turbojet engine mounting structure comprises a mounting frame, the mounting frame is of a semi-surrounding structure, one end of the mounting frame is fixedly connected with a main mounting section and at least one auxiliary mounting section, and inserting rods are inserted into the main mounting section and the auxiliary mounting sections; one end of the inserting rod is shrunk into a circular truncated cone-shaped structure, the other end of the inserting rod is fixedly connected with a hanging rod, a clamping plate is clamped on the hanging rod, and a first fixing bolt is arranged on the clamping plate in a penetrating manner; a bolt penetrating hole is formed in the mounting frame, and a second fixing bolt is mounted through the bolt penetrating hole; a pin penetrating hole is formed in the mounting frame, and a positioning pin is mounted through the pin penetrating hole; the fixing device has the advantages that the fixing device is convenient to install and fix on the stator casing, the stator casing can be conveniently installed in a narrow space, and threats to the safety performance of an engine can be effectively avoided.
本发明涉及涡喷发动机静子机匣安装辅助工具技术领域,且公开了一种小推力涡喷发动机安装结构。该小推力涡喷发动机安装结构包括安装架,安装架为半包围结构,在安装架的一端固定连接有一个主安装节和至少一个辅助安装节,在主安装节和辅助安装节上均插设有插杆;插杆的一端收缩成圆台形结构,插杆的另一端固定连接有挂杆,在挂杆上卡设有卡板,在卡板上穿设有一号固定螺栓;安装架上开设有螺栓穿孔,并通过螺栓穿孔安装有二号固定螺栓;安装架上开设有销钉穿孔,并通过销钉穿孔安装有定位销;具有在静子机匣上的安装固定操作方便,方便静子机匣在狭小空间内的安装的优点,可有效避免对发动机的安全性能造成威胁的优点。
Mounting structure of low-thrust turbojet engine
一种小推力涡喷发动机安装结构
2025-05-30
Patent
Electronic Resource
Chinese
IPC: | B64D Ausrüstung für Flugzeuge , EQUIPMENT FOR FITTING IN OR TO AIRCRAFT / B64F GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT , Boden- oder Flugzeugträgerdeckeinrichtungen besonders ausgebildet für die Verwendung in Verbindung mit Luftfahrzeugen |
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