The invention belongs to the technical field of
avionics tests, and especially relates to a vertical gyro tester. The vertical gyro tester is composed of a first single-pole single-throw switch (S1), a disconnecting switch (S2), a quick switch (S3), a first single-pole double-throw switch (S4), a second single-pole double-throw switch (S5), a third single-pole double-throw switch (S6), a fourth single-pole double-throw switch (S7), a fuse
radar pitch lower end output terminal F, a first
ampere meter (A1), a second
ampere meter (A2), a
voltage meter (V), and test holes (Rx, Ry, Rz, Px, Py, Pz, Rh, Rc, Ph, and Pc). When a worker uses the provided vertical gyro tester to detect a vertical gyro, the
external connection is simple, and the operation is convenient. On one hand, the vertical gyro tester can test the overall performances of a vertical gyro, thus the disqualified vertical gyro will not be applied to an
airplane, and the efficiency and quality of
airplane assembly are both improved; on the other hand, the fault points on a disqualified finished product can be rapidly found out by the vertical gyro tester, and a worker can quickly find and repair the fault points therefore.