The present invention claims priority under 35 U.S.C. 119(a-d) to CN 202010434918.2, filed May 21, 2020.
The present invention relates to the field of aeroengine, and more particularly to a device for measuring a surface temperature of a turbine blade based on a rotatable prism.
The strength and life of turbine blades determine the life of an aeroengine. Under extreme engine conditions at high speeds, the turbine blades carry the cyclic thermal load and the large centrifugal force. In order to ensure the stability and reliability of the engine during operation, it is necessary to accurately monitor the surface temperature and distribution of the turbine blades to evaluate the thermal load thereof, which is beneficial to the maintenance of the engine. Judging from the current research status, there are many institutions dedicated to the study of temperature measurement on the surface of turbine blades, but most of the researches are based on single-point temperature measurement and combined with the motion scanning of the probe and other devices, so as to achieve the surface temperature measurement of the entire turbine blade. This method is feasible, but the efficiency is slow, and it is inevitably for moving the probe position to affect the focus or stability of the optical system inside the probe. Therefore, the present invention proposes a non-single-point temperature measuring device with a rotatable prism.
In order to solve the problems that the current temperature measuring device for turbine blades are low in efficiency and single in function, the present invention provides a device for measuring a surface temperature of a turbine blade based on a rotatable prism.
Accordingly, the present invention provides technical solutions as follows.
A device for measuring a surface temperature of a turbine blade based on a rotatable prism comprises a probe, a prism rotating apparatus and an optical focusing apparatus, wherein:
the prism rotating apparatus and the optical focusing apparatus are located at an outer wall of the probe;
the probe comprises a probe outer casing, a probe inner casing, a water-cooled casing pipe, a sapphire window piece, a quartz prism, a light pipe, a collimating lens, a focusing lens and an infrared array detector, wherein:
the prism rotating apparatus comprises a rotary motor, a worm, a gear and a prism rotary table, wherein one end of the prism rotary table is located within the probe, another end of the prism rotary table is located outside the probe, a rotary through hole is provided in the probe inner casing and the probe outer casing for accommodating the prism rotary table, the one end of the prism rotary table is fixed with the quartz prism, the another end of the prism rotary table is mechanically connected with the rotary motor, so that the rotary motor rotates to drive the prism rotary table to rotate;
the optical focusing apparatus comprises a telescopic motor, a coupler, a lead screw and a drive rod, wherein the drive rod is fixed with an outer wall of the light pipe, a slot is provided in the probe inner casing and the probe outer casing for allowing the drive rod to move, the drive rod is sleeved to the lead screw, the telescopic motor is connected with the lead screw through the coupler, so that the telescopic motor rotates to drive the lead screw, so as to further drive the drive rod to move along the slot.
Further, a winding density of the water-cooled casing pipe which is wound on the probe inner casing from the lower portion of the probe inner casing to the upper portion of the probe inner casing is gradually increased.
Further, the gear is located at the another end of the prism rotary table which is located outside the probe, and the worm is cooperated with the gear.
Compared with the prior art, the present invention has some beneficial effects as follows.
The present invention provides an innovative simple double-shaft composite structure, which overcomes the installation difficulties and serious optical pollution caused by the excessive length of the traditional turbine blade measuring device extending into the engine. The spiral water cooling device is introduced based on heat transfer, which greatly increases the cooling efficiency. The rotation of the prism replaces the traditional rotation of the whole device, which not only reduces the instability of the optical system caused by the rotation of the whole device, but also improves the scanning efficiency. The simple transmission structure of the optical pipe solves the focusing problem that is not realized by the traditional probe device. The use of the array detector is able to simultaneously detect the temperature of multiple facets, which also greatly improves the scanning efficiency.
In the drawings, 1: probe outer casing; 2: water entry pipe; 3: cooling water inlet; 4: telescopic motor; 5: coupler; 6: lead screw; 7: drive rod; 8: slot; 9: rotary motor; 10: worm; 11: gear; 12: rotary through hole; 13: water discharging pipe; 14: cooling water outlet; 15: sapphire window piece; 16: quartz prism; 17: water-cooled casing pipe; 18: light pipe; 19: infrared array detector; 20: focusing lens; 21: collimating lens; 22: prism rotary table; 23: bottle neck; 24: probe inner casing.
The probe outer casing is a double-pass Inconel-600 pipe, which has a cooling water inlet and a cooling water outlet. A water-cooled casing pipe is an irregular spiral pipe and located within the probe outer casing. A water entry pipe of the water-cooled casing pipe passes through the cooling water inlet of the probe outer casing, and a water discharging pipe of the water-cooled casing pipe passes through the cooling water outlet of the probe outer casing, such that the cooling water is introduced through the water entry pipe while cooling, flows along a spiral direction of the water-cooled casing pipe, takes away heat from an inner wall and an outer wall of the probe outer casing, and finally flows out through the water discharging pipe, thereby achieving cooling. Moreover, the screw pitch of the water-cooled casing pipe from the water entry pipe to the water discharging pipe is gradually decreased for ensuring that cooling is sufficiently achieved when the cooling water flows towards the front end of the probe outer casing, so as to protect the entire device. A sapphire window piece is located at the top portion of the probe outer casing for allowing radiation to pass through and blocking high-temperature gas. A quartz prism is a triangular prism and located behind the sapphire window piece for refracting the radiation beam on the blade surface which penetrates through the sapphire window piece to the light pipe. The prism rotating apparatus comprises a rotary motor, a worm, a gear and a prism rotary table, wherein the gear is externally engaged with the worm, one end of the worm is engaged with the gear for transmission, another end of the worm is connected with the output shaft of the rotary motor, the gear is connected with the prism rotary table, the prism rotary table is configured to accommodate the quartz prism, the rotary motor drives the worm to rotate; when the worm rotates, the gear is driven for further driving the prism rotary table to rotate. The prism rotating apparatus is able to drive the quartz prism to rotate at any angle, so that the quartz prism is able to observe different target areas on the blade and refract the light into the light pipe. The light pipe is a stainless steel metal pipe. A collimating lens, a focusing lens and an infrared array detector are installed within the light pipe. The light pipe is located behind the quartz prism. The radiation from the surface of the blade penetrates through the quartz prism, and then passes through the collimating lens and the focusing lens in sequence both of which are located within the light pipe, and then reaches the infrared array detector, and then is converted into an electrical signal to be transmitted to an upper computer. A drive rod is welded with the light pipe for driving the light pipe to move back and forth. An optical focusing apparatus comprises a telescopic motor, a lead screw and a drive rod, wherein the telescopic motor drives the lead screw to rotate for further driving the drive rod to telescopically move along the lead screw, the drive rod drives the light pipe to telescopically move back and forth within the probe outer casing, so as to achieve focusing through telescopically adjusting an object distance of the optical system. The infrared array detector is able to divide a target surface corresponding to a detection unit into discrete units corresponding to different temperature points. Therefore, output voltage signals represent temperature values of different positions, so that when the turbine blade rotates, the temperature scanning measurement of the entire surface is completed.
The present invention is further explained in detail with embodiments and drawings as follows.
Referring to
As shown in
Referring to
Referring to
Moreover, the infrared array detector 19 is able to divide a target surface corresponding to a detection unit into discrete units corresponding to different temperature points. Therefore, output voltage signals represent temperature values of different positions, so that when the turbine blade rotates, the temperature scanning measurement of the entire surface is completed.
Number | Date | Country | Kind |
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202010434918.2 | May 2020 | CN | national |
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Entry |
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CN-103180700-A (Year: 2013)—translation. |
CN-103261859-B (Year: 2017)—translation. |
CN-2395290-Y (Year: 2000)—translation. |
JP-2003130734-A (Year: 2003)—translation. |
JP-2011515671-A (Year: 2011)—translation. |
SE-455443-B (Year: 1988)—translation. |
Number | Date | Country | |
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20210270674 A1 | Sep 2021 | US |