This application claims the benefit of Chinese patent application CN 201210299797.0, which was filed on Aug. 21, 2012, and which is incorporated herein in its entirety by reference.
The present disclosure pertains to the technical field of X-ray generator, and in particular, relates to an integrated flying-spot X-ray apparatus.
A conventional X-ray apparatus emits an X-ray along a conical plane or a sector plane and cannot dynamically scan an object spot by spot. At present, scanning by means of an integrated flying-spot X-ray apparatus is desired in the field of safety inspection and medical treatment. To this end, there is a need to provide an integrated flying-spot X-ray apparatus which can alleviate or eliminate at least one the foregoing technical problems.
The present invention has been made bearing in mind of the above technical problems existing in the prior art.
An object of this disclosure is to provide an integrated flying-spot X-ray apparatus so as to meet requirements of the field of safety inspection and medical treatment.
According to one aspect of the present disclosure, there is provided an integrated flying-spot X-ray apparatus comprising a ray generator configured to generate the X-ray; a revolving collimator device provided thereon with at least one aperture and arranged to be rotatable about the ray generator; a frameless torque motor configured to drive the revolving collimator device to rotate about the ray generator; and a cooling device configured to cool the ray generator, wherein the ray generator, the revolving collimator device, the frameless torque motor and the cooling device are mounted on an integrated mounting frame.
With the above structure, the X-ray apparatus emits a sector-shaped X-ray, and the dynamic spot-by-spot scanning operation of the ray can be achieved by rotating the revolving collimator device with an aperture provided outside of the sector-shaped X-ray.
Furthermore, the integrated mounting frame comprises a supporting frame configured to support the frameless torque motor and the cooling device, and a bracket configured to be fixedly connected with the supporting frame to fix the ray generator. With such structure, the supporting frame and the bracket are used to integrate the above-mentioned respective functional devices to form an integrated flying-spot X-ray apparatus with a compact structure.
Specifically, the ray generator comprises an X-ray tube, a high voltage generator configured to drive the X-ray tube, an inner protecting sleeve provided outside of the X-ray tube, and an outer sleeve provided outside of the inner protecting sleeve, wherein the inner protecting sleeve and the outer sleeve each have a ray outlet, and the ray outlets are aligned with each other and communicate with each other to direct the X-ray from the X-ray tube out of the ray generator.
Furthermore, an anode end cap is provided at a side of an anode target of the X-ray tube, and between the anode end cap and the anode target is further provided a first anode insulation protecting seat and a second anode insulation protecting seat which are combined to form a labyrinth channel. A cathode protecting end cap is provided at a side of a cathode of the X-ray tube, and between the cathode protecting end cap and the cathode of the X-ray tube is further provided a labyrinth protecting ring.
In the above embodiments, the respective ray outlets of the inner protecting sleeve and the outer sleeve are provided therein with a calking window, and calking window is made of a material through which the X-ray can pass or penetrate.
More specifically, a cavity around the X-ray tube is filled with high voltage insulation oil, and between the labyrinth protecting ring and the cathode protecting end cap is further provided an expansion drum.
In the above embodiments, the cathode protecting end cap, the inner protecting sleeve, the second anode insulation protecting seat, the first anode insulation protecting seat and the labyrinth protecting ring are made of a material that can shield the X-ray, and the second anode insulation protecting seat and the first anode insulation protecting seat exhibits insulation property.
In an embodiment, the cathode protecting end cap is provided with a bending through hole, and the cathode protecting end cap and the expansion drum are fitted together to form a gas chamber. Thus, when the expansion drum is pressed, the gas therein is discharged through the hole of the cathode protecting end cap.
Specifically, the outer sleeve is provided with a beam exiting opening opened at a certain angle, and the outer sleeve is further formed on the outer side wall thereof with a boss having a shaft shoulder.
More specifically, the first anode insulation protecting seat and the second anode insulation protecting seat are combined integrally to form a cavity, and a fluid guiding hole on the first anode insulation protecting seat and a liquid injecting hole on the second anode insulation protecting seat are misaligned with each other, so that a labyrinth structure is formed. The first anode insulation protecting seat and the second anode insulation protecting seat have a high voltage insulation performance and can prevent leakage of the ray. Thus, the outer cavity of the X-ray tube can be ensued to have high voltage insulation and prevent leakage of the ray.
In an embodiment, the revolving collimator device comprises at least one bearing supported on the boss having the shaft shoulder of the outer sleeve, a flying-spot revolving protecting ring supported by the at least on bearing and configured to be revolvable about the outer sleeve, and side protecting plates provided at two sides of the flying-spot revolving protecting ring, respectively, and right and left end caps. With this structure and construction, the revolving collimator device with the aperture is provided around the outer sleeve of the ray generator, and the collimator device of the revolving collimator device revolves by means of the bearing. Furthermore, the revolving collimator device with the aperture is driven by the frameless torque motor, and the dynamic spot-by-spot scanning of the ray is achieved by revolving about the aperture of the collimator device provided outside of the ray generator.
Specifically, the cooling device comprises a magnetic pump configured to pump the heated high voltage insulation oil, a heat exchanger configured to cool the pumped high voltage insulation oil, and an oil passage configured to convey the pumped high voltage insulation oil into the heat exchanger for heat exchanging, and the cooled high voltage insulation oil returns back into the cavity around the X-ray tube. Since the cavity of the ray generator is filled with the high voltage insulation oil, the circulation system constituted by connecting the above components in series can be used to cool the anode target of the bulb tube so as to ensure the normal operation of the integrated X-ray apparatus.
With the above configuration and construction, at least one of the following advantages can be achieved:
(1) a dynamic spot-by-spot scanning of the ray can be achieved;
(2) a compact structure is obtained; and
(3) the material used can efficiently shield the ray.
Next, embodiments of the present disclosure are further described in combination with the drawings.
With reference to
With reference to
As shown in
Specifically, the anode end cap 47 is provided at an anode target 56 side of the X-ray tube 53. The first anode insulation protecting seat 52 and the second anode insulation protecting seat 50 are further provided between the anode end cap 47 and the anode target 56, and they form a labyrinth channel. The cathode protecting end cap 41 is provided at a cathode side of the X-ray tube 53. The labyrinth protecting ring 54 is further provided between the cathode protecting end cap 41 and the cathode of the X-ray tube 53. As shown in
As shown in
As shown in
With reference to
As shown in
Furthermore, as shown
As shown in
Next, the operation of the integrated flying-spot X-ray apparatus according to the specific embodiments of the present disclosure is explained in combination with
As shown in
Although the flying-spot revolving protecting ring 64 is provided with a small through hole along the radial direction in the above embodiment, the present disclosure is not limited thereto. A plurality of through holes may be provided.
While the present disclosure has been described in conjunction with the drawings, the embodiment shown in the drawings is only an example for explaining preferred embodiments of the present disclosure and is not intended to limit the present disclosure. Although some embodiments for the general concept of the present disclosure have been shown and explained, the skilled person in the art will appreciate that modifications to the above embodiments can be carried out without departing from the spirit and principle of the present general inventive concept. The scope of the present disclosure should be defined by the appended claims and equivalents thereof.
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