Loading device for airplane spoiler function test

• Main Authors: SUN XI, CUI BAOZHONG, CHEN TIJUN, ZHANG FENG, ZHANG ZHENHUAN
• Format: Patent
• Language: Chinese; English
• Published: 12.01.2024
• Subjects: AIRCRAFT; AVIATION; COSMONAUTICS; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING ORREPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLYADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFTCOMPONENTS, NOT OTHERWISE PROVIDED FOR; MEASURING; PERFORMING OPERATIONS; PHYSICS; TESTING; TESTING STATIC OR DYNAMIC BALANCE OF MACHINES ORSTRUCTURES; TESTING STRUCTURES OR APPARATUS NOT OTHERWISE PROVIDED FOR; TRANSPORTING

The utility model provides a loading device for an airplane spoiler function test, and the device comprises a spoiler supporting bracket which is disposed on an iron bird test bench; wherein the spoiler is arranged on the II beam plane of the frame 30 of the iron bird test bench; one end of the spoiler loading actuator is connected with the spoiler supporting bracket, and the other end of the spoiler loading actuator is connected with the spoiler; one end of the spoiler driving actuator is arranged on the II beam plane of the frame 30 of the iron bird test bed, and the other end of the spoiler driving actuator is connected with the spoiler; according to the loading device for the spoiler function test, the aerodynamic load borne by the spoiler in the air can be simulated vividly. 本申请提供了一种用于飞机扰流板功能试验的加载装置，所述加载装置包括：扰流板支撑支架，设置在铁鸟试验台架上；其中，扰流板设置在所述铁鸟试验台架30框的Ⅱ梁平面上；扰流板加载作动器，所述扰流板加载作动器的一端与所述扰流板支撑支架连接，所述扰流板加载作动器的另一端与所述扰流板连接；扰流板驱动作动器，所述扰流板驱动作动器的一端设置在所述铁鸟试验台架30框的Ⅱ梁平面上，所述扰流板驱动作动器的另一端与所述扰流板连接；本申请提供的一种用于扰流板功能试验的加载装置，能够较逼真的