US 12,449,311 B2
Optical probe with high stability for measurement of radiation information of turbine disks
Chao Wang, Sichuan (CN); Jing Jiang, Sichuan (CN); Yi Niu, Sichuan (CN); Hongzu Li, Sichuan (CN); Zezhan Zhang, Sichuan (CN); Lihao Yang, Sichuan (CN); Peifeng Yu, Sichuan (CN); and Shan Gao, Sichuan (CN)
Assigned to Universityof Electronic Science and Technology of China, Sichuan (CN)
Filed by University of Electronic Science and Technology of China, Sichuan (CN)
Filed on May 2, 2022, as Appl. No. 17/735,102.
Claims priority of application No. 202110913744.2 (CN), filed on Aug. 10, 2021.
Prior Publication US 2022/0260423 A1, Aug. 18, 2022
Int. Cl. G01J 5/00 (2022.01); G01J 5/08 (2022.01); G01J 5/0806 (2022.01); G01J 5/0821 (2022.01); G01J 5/0875 (2022.01)
CPC G01J 5/0088 (2013.01) [G01J 5/0806 (2013.01); G01J 5/0821 (2013.01); G01J 5/0875 (2013.01); G01J 5/08 (2013.01)] 2 Claims
OG exemplary drawing
 
1. An optical probe with high stability for measurement of radiation information of a turbine disk of an aeroengine, comprises a one-piece outer casing, a pressing ring, a sapphire window piece, an inner spacer, an outer spacer, a lens, first fixing nuts, second fixing nuts, fixing ropes and fixing screws, wherein:
the one-piece outer casing is made from GH3044 solid solution strengthened nickel-based antioxidant alloy;
an interior of the probe is divided into eight parts, which are as follows from a proximal hot end to a right end of the probe in sequence:
a pressing ring chamber for installing the pressing ring;
a cold air vent through which cold air is able to come in and out;
a sapphire window piece chamber reserved for thermal expansion of the proximal hot end of the sapphire window piece;
an outer spacer fixing chamber for installing the outer spacer and fixing the sapphire window piece;
a lens chamber for installing the outer spacer, the lens and the pressing ring;
a beam chamber for allowing beam to pass through, which is able to be customized according to a focal length of a lens;
a beam focusing chamber for transmitting the collected beam signal to the fiber at the focal point; and
an optical fiber chamber,
wherein due to threaded holes and high-temperature sealant, the proximal hot end of the outer casing has high tightness for preventing high-temperature gas from entering the outer casing and damaging the lens inside the outer casing; at the same time, due to an integrated design of the outer casing, an influence of external environment on an internal structure is able to be controlled only by an external pressing ring; the sapphire window piece chamber is reserved at the proximal hot end of the sapphire window piece to prevent the sapphire window piece from thermal expansion and resulting in collapse; the cold air vent at the proximal hot end is able to prevent damage to components caused by high temperature inside the probe;
the first fixing nuts, the second fixing nuts, the pressing ring, the outer spacer, the inner spacer, the fixing ropes, and the fixing screws are all made from GH3044 high-temperature resistant superalloy which has high plasticity, moderate thermal strength, excellent oxidation resistance, good stamping and welding process performance;
the sapphire window piece is coated with a layer of an antireflective film with a thickness in a range of 1.5-2.3 μm for increasing light transmittance; the lens is made from infrared fused quartz, which has higher working and melting temperature to be adapted to high temperature and high pressure environment of the turbine disk compared with traditional glass; a size of the spacer nut is able to be changed according to actual working conditions, and when the optical fiber is connected with an optical fiber interface integrated on the outer casing, the optical fiber and the optical fiber interface are prevented from being locked due to severe temperature changes, thereby affecting the acquisition effect.