一种航空光电瞄准吊舱测试用工作车
Through innovative design of the drive and monitoring components, the problem of angle instability of the photoelectric aiming pod testing equipment in complex environments was solved, achieving stable locking of the pod and precise angle control, thereby improving the accuracy and reliability of the test.
Patent Information
- Authority / Receiving Office
- CN · China
- Patent Type
- Utility models(China)
- Current Assignee / Owner
- 中国人民解放军95875部队
- Filing Date
- 2025-09-18
- Publication Date
- 2026-07-17
AI Technical Summary
Existing airborne optoelectronic targeting pod testing equipment is susceptible to external factors in complex flight environments, resulting in unstable test angles, lack of locking measures and angle feedback, which affects the accuracy and precision of test results.
The design employs a combination of drive and monitoring components. The arc plate is reliably locked through the cooperation of threaded rod, toothed block and toothed ring, and real-time angle monitoring is achieved through the cooperation of connecting shaft and dial, ensuring the stability and precise angle control of the pod during the test.
It achieves stable locking and precise angle adjustment of the pod during the test, improving the accuracy and reliability of the test results and supporting tracking stability tests at different angles.
Smart Images
Figure CN224511473U_ABST
Abstract
Claims
1. An airborne electro-optical targeting pod test vehicle, characterized in that, The support frame (1) is provided with a plurality of connecting plates (2) on its upper part. A mounting frame (3) is provided between two connecting plates (2). An arc plate (4) is provided inside the mounting frame (3). A drive assembly (5) for driving the arc plate (4) to rotate is provided between two connecting plates (2) and the mounting frame (3). A monitoring assembly (6) for monitoring the rotation angle of the arc plate (4) is provided on both sides of the arc plate (4). The drive assembly (5) includes a threaded rod (51) rotatably disposed between two corresponding connecting plates (2), a threaded sleeve (52) is threaded on the threaded rod (51), a plurality of toothed blocks (53) are disposed on the upper part of the threaded sleeve (52), and a toothed ring (12) that meshes with the toothed blocks (53) is disposed on the outer side of the arc plate (4). The monitoring component (6) includes connecting shafts (61) arranged on the left and right sides of the arc plate (4), and an indicator block (62) is provided at the end of the connecting shaft (61) away from the arc plate (4).
2. The test vehicle of claim 1, wherein: A handle (54) is rotatably provided on one side of the connecting plate (2) located on the front side. The handle (54) is connected to one end of the threaded rod (51). A guide groove (13) is provided at the bottom inner side of the mounting frame (3). A guide block (14) is slidably provided in the guide groove (13). The upper part of the guide block (14) is connected to the bottom of the threaded sleeve (52).
3. The testing vehicle for an aircraft optoelectronic targeting pod as described in claim 1, characterized in that: A connecting rod (55) is rotatably provided on one side of the connecting plate (2) located at the rear. One end of the connecting rod (55) is connected to the end of the threaded rod (51) away from the handle (54). A gear (56) is provided on the outside of the connecting rod (55). The two gears (56) are connected by a gear belt (57).
4. The test vehicle of claim 1 wherein: The mounting frame (3) has arc-shaped openings (7) on both the left and right sides. The side of the connecting shaft (61) away from the arc plate (4) passes through the arc-shaped opening (7) and is slidably connected to the arc-shaped opening (7).
5. The test vehicle of claim 4 wherein: The left and right sides of the mounting frame (3) are provided with dials (8) for use with the indicator block (62) below the arc-shaped opening (7).
6. The testing vehicle for an aircraft optoelectronic targeting pod as described in claim 1, characterized in that: The bottom of the arc plate (4) is provided with a plurality of symmetrically distributed rollers (9), and the left and right sides inside the mounting frame (3) are provided with support plates (10), and the rollers (9) and the support plates (10) are in rolling contact.
7. The test vehicle of claim 1 wherein: the test vehicle is an airborne electro-optical targeting pod test vehicle. The upper part of the arc-shaped plate (4) is provided with two symmetrically distributed straps (11).