CN114812267A - Laser transmitter shaft adjustment mechanism - Google Patents
Laser transmitter shaft adjustment mechanism Download PDFInfo
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- CN114812267A CN114812267A CN202210380417.XA CN202210380417A CN114812267A CN 114812267 A CN114812267 A CN 114812267A CN 202210380417 A CN202210380417 A CN 202210380417A CN 114812267 A CN114812267 A CN 114812267A
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41A—FUNCTIONAL FEATURES OR DETAILS COMMON TO BOTH SMALLARMS AND ORDNANCE, e.g. CANNONS; MOUNTINGS FOR SMALLARMS OR ORDNANCE
- F41A33/00—Adaptations for training; Gun simulators
- F41A33/02—Light- or radiation-emitting guns ; Light- or radiation-sensitive guns; Cartridges carrying light emitting sources, e.g. laser
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- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F41—WEAPONS
- F41G—WEAPON SIGHTS; AIMING
- F41G1/00—Sighting devices
- F41G1/06—Rearsights
- F41G1/16—Adjusting mechanisms therefor; Mountings therefor
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Abstract
Description
技术领域technical field
本申请涉及实兵模拟训练领域,尤其涉及一种激光发射器调轴机构。The present application relates to the field of actual soldier simulation training, and in particular, to an axis adjustment mechanism of a laser transmitter.
背景技术Background technique
在实兵模拟训练系统中,激光发射器作为核心部分,是每次演习中使用数量最多,频率最高的器材,演习时需要将其安装在武器上并与武器准星保持平行,只有经过光轴调校,才能精准模拟实装准星方向,稳定射击。现有的激光发射光轴调节装置,大多采用调节光学模组结构,一端粗略固定,另一端顶丝调节,此方式精度低、稳定性差,使用过程中战术战斗动作带来的冲击和震动极易使光轴方向发生变化,严重影响武器射击的精准度;也有采用调节发射机整体的形式,外置调节平台,体积重量大,影响武器装备携行和正常操作;还有采用整形镜与激光器分离的形式,调节镜片与激光器之间的侧向位移改变光束方向,但会导致光斑形状变化和能量损耗。缺少一种高精度、强稳定性的快速调节机构,真实模拟武器的射击精度,保障战场训练的效果。In the actual soldier simulation training system, the laser transmitter, as the core part, is the equipment with the largest number and the highest frequency in each exercise. It needs to be installed on the weapon and kept parallel to the weapon crosshair during the exercise. Only after the optical axis is adjusted In order to accurately simulate the direction of the installed crosshairs and stabilize the shooting. Most of the existing laser-emitting optical axis adjustment devices adopt an adjustment optical module structure, one end is roughly fixed, and the other end is adjusted by a top wire. This method has low precision and poor stability, and is very easy to shock and vibration caused by tactical combat actions during use. The direction of the optical axis changes, which seriously affects the accuracy of weapon shooting; some also use the form of adjusting the overall transmitter and an external adjustment platform, which has a large volume and weight, which affects the carrying and normal operation of weapons and equipment; there are also plastic mirrors and lasers. form, adjusting the lateral displacement between the mirror and the laser changes the beam direction, but results in spot shape changes and energy loss. There is a lack of a high-precision, strong-stability rapid adjustment mechanism, which can truly simulate the shooting accuracy of weapons and ensure the effect of battlefield training.
发明内容SUMMARY OF THE INVENTION
本申请的目的在于提供一种激光发射器调轴机构,该激光发射器调轴机构提高了激光发射器光轴精度以及稳定性。The purpose of the present application is to provide an axis adjustment mechanism for a laser transmitter, which improves the accuracy and stability of the optical axis of the laser transmitter.
为此,本申请实施例提供了一种激光发射器调轴机构,包括:激光模组,沿自身长度方向设置有两端,一端为激光发射端,所述激光模组远离发射端设置有调节环,所述调节环背离所述激光模组的一面呈弧形设置,所述调节环开设有多个球槽,多个球槽绕调节环周向排布;壳体,开设有放置腔,所述壳体通过所述放置腔套设于所述激光模组;调节组件,包括多个适配于所述球槽的调节球,多个所述调节球沿所述调节环周向排布,所述调节球的部分伸入所述球槽中,所述调节球远离所述球槽的部分位于所述壳体的内腔壁中。To this end, an embodiment of the present application provides an axis adjustment mechanism for a laser transmitter, including: a laser module, which is provided with two ends along its own length direction, one end is a laser emission end, and the laser module is provided with an adjustment mechanism away from the emission end. The side of the adjustment ring facing away from the laser module is arranged in an arc shape, the adjustment ring is provided with a plurality of ball grooves, and the plurality of ball grooves are circumferentially arranged around the adjustment ring; the casing is provided with a placement cavity, The housing is sleeved on the laser module through the placement cavity; the adjustment assembly includes a plurality of adjustment balls adapted to the ball groove, and the plurality of adjustment balls are arranged along the circumference of the adjustment ring , the part of the adjusting ball protrudes into the ball groove, and the part of the adjusting ball away from the ball groove is located in the inner cavity wall of the housing.
在一种可能的实现方式中,所述调节球体积的三分之一位于所述球槽内,所述调节球体积的三分之一位于所述壳体的内腔壁。In a possible implementation manner, one third of the volume of the adjustment ball is located in the ball groove, and one third of the volume of the adjustment ball is located in the inner cavity wall of the housing.
在一种可能的实现方式中,沿所述壳体径向贯穿有用于放置所述调节球的球孔,还包括外筒,所述外筒套设于所述壳体的外周侧且与所述壳体可拆卸连接,所述球孔位于所述外筒内腔。In a possible implementation manner, a ball hole for placing the adjusting ball runs through the casing radially, and further includes an outer cylinder, the outer cylinder is sleeved on the outer peripheral side of the casing and is connected to the outer casing. The shell is detachably connected, and the ball hole is located in the inner cavity of the outer cylinder.
在一种可能的实现方式中,所述调节组件还包括:微调旋钮,位于所述发射端,所述壳体开设有适配所述微调旋钮的旋钮孔,所述微调旋钮的一端伸入所述放置腔与所述激光模组抵接,所述微调旋钮伸入所述放置腔的长度可调节设置;弹性件,所述壳体开设有放置孔,所述弹性件位于所述放置孔中且一端伸入所述放置腔中与所述激光模组抵接。In a possible implementation manner, the adjustment assembly further includes: a fine-tuning knob, located at the transmitting end, the casing is provided with a knob hole adapted to the fine-tuning knob, and one end of the fine-tuning knob extends into the The placement cavity is in contact with the laser module, and the length of the fine-tuning knob extending into the placement cavity can be adjusted; an elastic piece, the housing is provided with a placement hole, and the elastic piece is located in the placement hole And one end extends into the placement cavity and abuts with the laser module.
在一种可能的实现方式中,所述微调旋钮包括:调节部,设置于所述旋钮孔内可在旋钮孔中沿所述激光模组径向移动;第一抵接部,位于所述放置腔中,所述第一抵接部的一面与所述调节部连接且另一面与所述激光模组抵接,所述第一抵接部的外沿朝向所述调节部弯折设置。In a possible implementation manner, the fine-tuning knob includes: an adjustment part, which is arranged in the knob hole and can move in the radial direction of the laser module in the knob hole; a first abutting part is located in the placement In the cavity, one side of the first abutting portion is connected with the adjusting portion and the other side is abutting with the laser module, and the outer edge of the first abutting portion is bent and arranged toward the adjusting portion.
在一种可能的实现方式中,所述弹性件包括:弹簧,位于所述放置孔中;第二抵接部,位于所述放置腔中,所述第二抵接部一面与所述弹簧连接且另一面与所述激光模组抵接,所述第二抵接部的外沿朝向所述弹簧弯折设置。In a possible implementation manner, the elastic member includes: a spring, located in the placement hole; a second abutting portion, located in the placement cavity, and one side of the second abutting portion is connected with the spring The other side is in contact with the laser module, and the outer edge of the second contact portion is bent and arranged toward the spring.
在一种可能的实现方式中,所述微调旋钮设置有两个,两个所述微调旋钮与所述弹性件绕所述激光模组呈圆周设置,两个微调旋钮呈90°夹角,所述弹性件与任意一个所述微调旋钮的夹角呈135°设置。In a possible implementation, there are two fine-tuning knobs, the two fine-tuning knobs and the elastic member are circumferentially arranged around the laser module, and the two fine-tuning knobs form an included angle of 90°, so The included angle between the elastic piece and any one of the fine-tuning knobs is set at 135°.
在一种可能的实现方式中,所述调节环设置于所述激光模组远离所述激光发射的一端。In a possible implementation manner, the adjustment ring is disposed at an end of the laser module away from the laser emission.
根据本申请实施例提供的激光发射器调轴机构,包括激光模组、壳体以及调节组件,激光模组沿自身长度方向设置有两端,一端为激光发射端,激光模组远离发射设置有调节环,调节环远离激光模组的一面呈弧形设置调节环开设有多个球槽,多个球槽绕调节环周向排布;壳体开设有放置腔,壳体通过放置腔套设于激光模组;调节组件包括多个调节球,多个调节球沿调节环周向排布,调节球的部分伸入球槽中,调节球远离球槽的部分位于壳体的内腔壁中。该激光发射器调轴机构提高了激光发射器光轴精度以及稳定性。The laser transmitter axis adjustment mechanism provided according to the embodiment of the present application includes a laser module, a housing and an adjustment assembly. The laser module is provided with two ends along its own length direction, one end is a laser emission end, and the laser module is provided with a Adjustment ring, the side of the adjustment ring away from the laser module is arranged in an arc shape. The adjustment ring is provided with a plurality of ball grooves, and the plurality of ball grooves are arranged circumferentially around the adjustment ring; the shell is provided with a placement cavity, and the shell is sleeved through the placement cavity. In the laser module; the adjustment assembly includes a plurality of adjustment balls, the plurality of adjustment balls are arranged along the circumference of the adjustment ring, the part of the adjustment ball extends into the ball groove, and the part of the adjustment ball away from the ball groove is located in the inner cavity wall of the shell . The laser transmitter axis adjustment mechanism improves the accuracy and stability of the laser transmitter's optical axis.
附图说明Description of drawings
为了更清楚地说明本申请实施例或现有技术中的技术方案,下面将对实施例或现有技术描述中所需要使用的附图作一简单地介绍,显而易见地,下面描述中的附图是本申请的一些实施例,对于本领域普通技术人员来讲,在不付出创造性劳动的前提下,还可以根据这些附图获得其他的附图。另外,在附图中,相同的部件使用相同的附图标记,且附图并未按照实际的比例绘制。In order to more clearly illustrate the embodiments of the present application or the technical solutions in the prior art, the following will briefly introduce the accompanying drawings used in the description of the embodiments or the prior art. Obviously, the accompanying drawings in the following description These are some embodiments of the present application. For those of ordinary skill in the art, other drawings can also be obtained based on these drawings without any creative effort. In addition, in the drawings, the same reference numerals are used for the same components, and the drawings are not drawn to actual scale.
图1示出本申请实施例提供的一种激光发射器调轴机构的结构示意图;1 shows a schematic structural diagram of a laser transmitter axis adjustment mechanism provided by an embodiment of the present application;
图2示出本申请实施例提供的一种激光发射器调轴机构的正面剖视图;2 shows a front cross-sectional view of a laser transmitter axis adjustment mechanism provided by an embodiment of the present application;
图3示出本申请实施例提供的一种激光发射器调轴机构的端面剖视图。FIG. 3 shows an end cross-sectional view of a laser transmitter axis adjustment mechanism provided by an embodiment of the present application.
附图标记说明:Description of reference numbers:
1、激光模组;11、调节环;2、壳体;3、调节球;4、外筒;5、微调旋钮;6、弹性件。1. Laser module; 11. Adjusting ring; 2. Housing; 3. Adjusting ball; 4. Outer cylinder; 5. Fine-tuning knob; 6. Elastic part.
具体实施方式Detailed ways
为使本申请实施例的目的、技术方案和优点更加清楚,下面将结合本申请实施例中的附图,对本申请实施例中的技术方案进行清楚、完整地描述,显然,所描述的实施例是本申请的一部分实施例,而不是全部的实施例。基于本申请中的实施例,本领域普通技术人员在没有做出创造性劳动的前提下所获得的所有其他实施例,都属于本申请保护的范围。In order to make the purposes, technical solutions and advantages of the embodiments of the present application clearer, the technical solutions in the embodiments of the present application will be described clearly and completely below with reference to the drawings in the embodiments of the present application. Obviously, the described embodiments It is a part of the embodiments of the present application, but not all of the embodiments. Based on the embodiments in the present application, all other embodiments obtained by those of ordinary skill in the art without creative work shall fall within the protection scope of the present application.
如图1至图3所示,图1示出本申请实施例提供的一种激光发射器调轴机构的结构示意图,图2示出本申请实施例提供的一种激光发射器调轴机构的正面剖视图,图3示出本申请实施例提供的一种激光发射器调轴机构的端面剖视图。As shown in FIGS. 1 to 3 , FIG. 1 shows a schematic structural diagram of a laser transmitter axis adjustment mechanism provided by an embodiment of the present application, and FIG. 2 shows a laser transmitter axis adjustment mechanism provided by an embodiment of the present application. Front cross-sectional view, FIG. 3 shows an end cross-sectional view of a laser transmitter axis adjustment mechanism provided by an embodiment of the present application.
本申请实施例提供一种激光发射器调轴机构,包括激光模组1、壳体2以及调节组件。The embodiment of the present application provides an axis adjustment mechanism of a laser transmitter, which includes a
调节组件设置于激光模组1与壳体2之间,用于调节激光模组1与壳体2的相对位置,从而对激光发射器调轴机构的精度以及稳定性进行调节,真实模拟武器的射击精度,保障战场训练的效果。The adjustment component is arranged between the
其中,激光模组1沿自身长度方向设置有两端,一端为激光发射端,激光模组1远离发射端设置有调节环11,调节环11远离激光模组1的一面呈圆弧设置,调节环11开设有多个球槽,多个球槽绕调节环11周向排布,壳体2开设有放置腔,壳体2通过放置腔套设于激光模组1;调节组件包括多个适配于球槽的调节球3,多个调节球3沿调节环11周向排布,调节球3的部分伸入球槽中,调节球3远离球槽的部分位于壳体2的内腔壁中。Among them, the
需要理解的是,激光模组1是发散角可调的独立发光组件,呈圆柱状,激光模组1沿自身长度方向设置有两端,一端为激光发射端,可用于发射激光,另一端设置有调节环11,调节环11的位置远离发射端。It should be understood that the
壳体2开设有放置腔,壳体2通过放置腔套设激光模组1,壳体2的放置腔呈圆孔状,激光模组1位于放置腔中。调节环11的外径小于壳体2的内径,因此调节环11与壳体2的内壁间隔设置,调节组件包括多个调节球3,多个调节球3沿调节环11周向排布,调节环11处开设有多个球槽,多个球槽与多个调节球3相适配,调节球3的部分位于球槽中,部分位于壳体2的内腔壁中,且调节球3可在壳体2的内腔壁转动。The
使用时,使用者转动激光模组1,以调节环11为界,激光模组1的两端绕调节环11进行转动或摆动,多个调节球3发生转动,从而降低调节环11与壳体2的内腔壁的摩擦力,使得调节环11与壳体2的相对转动更加容易。When in use, the user rotates the
其中调节环11远离激光模组1的一面呈圆弧设置,从而使得激光模组1的两端可绕调节环11进行转动。The side of the
参照图2和图3,以激光模组1的轴向设置为Z向,在垂直于Z向的平面设置有X向与Y向,其中X向、Y向以及Z向两两相互垂直。调节环11与调节球3的设置使得激光模组1在调节环11处不能沿调节环11径向移动,同时调节球3使得激光模组1不能绕Z相转动,从而使得激光模组1的激光发射端只具有X向以及Y向的转动自由度,从而对激光模组1发射端的俯仰以及侧摆位置进行精准调节。2 and 3 , the axial direction of the
调节球3的数量可以为两个、三个以及四个等多个数量,根据激光模组1的半径大小进行调节,调节球3的设置,提高了调节环11与壳体2之间安装的稳定性,同时提高了激光模组1绕调节环11转动的效果。The number of the
在一个示例中,调节球3体积的三分之一位于球槽中,调节球3体积的三分之一位于壳体2的内腔壁中。调节球3在球槽中的体积占比为整体体积的三分之一,调节球3体积的三分之一位于壳体2的内腔壁中,从而使得调节球3的体积的三分之一位于调节环11与壳体2的内腔壁中,本申请调节球3的体积划分设置,不仅确保了调节球3与壳体2的内腔壁以及调节环11连接的稳定性,同时还确保了激光模组1发生转动的顺畅性。In one example, one third of the volume of the
进一步的,沿壳体2径向贯穿有用于放置调节球3的球孔,还包括外筒4,外筒4套设于壳体2的外周侧且与壳体2可拆卸连接,球孔位于外筒4内腔。Further, a ball hole for placing the adjusting
可以理解的是,球孔适配于调节球3,球孔贯穿于壳体2。外筒4套设于壳体2,即外筒4的内壁与壳体2的外壁抵接,外筒4与壳体2可拆卸连接,即外筒4与壳体2可选择螺纹连接、插接或隼接等方式连接。It can be understood that the ball hole is adapted to the adjusting
安装时,先将激光模组1放入放置腔中,然后将调节球3从壳体2外壁放入球孔中,使得调节球3部分位于球槽中,部分位于球孔中,然后将外筒4套接于壳体2,将外筒4与壳体2进行连接。When installing, first put the
在一个示例中,调节组件还包括微调旋钮5以及弹性件6,微调旋钮5位于发射端,壳体2开设有适配微调旋钮5的旋钮孔,微调旋钮5的一端伸入放置腔与激光模组1抵接,微调旋钮5伸入放置腔的长度可调节设置;壳体2开设有放置孔,弹性件6位于放置孔中且一端伸入放置腔中与激光模组1抵接。In one example, the adjustment assembly further includes a fine-
使用时,将微调旋钮5伸入放置腔中,调节微调旋钮5的伸入的长度,从而使得激光模组1发生移动,激光模组1绕调节环11发生摆动或转动,调整激光模组1的俯仰或侧摆的位置,使得激光模组1的激光发射的精度,然后通过微调旋钮5与弹性件6对激光模组1进行抵接,从而对激光模组1进行稳定固定。When in use, the fine-
在一个示例中,微调旋钮5包括调节部以及第一抵接部:调节部设置于旋钮孔内可在旋钮孔中沿激光模组1的径向移动;第一抵接部位于放置腔中,第一抵接部的一面与调节部连接且另一面与激光模组1抵接,第一抵接部的外沿朝向调节部弯折设置。In one example, the
可以理解的是,调节部呈柱状设置,调节部可通过旋钮孔与壳体2连接,当需要调节微调旋钮5时,可对调节部进行旋转使得调节部沿激光模组1径向移动。调节部可以与壳体2螺纹连接的,可直接控制调节部的伸入长度,当调节部伸入放置腔的长度调节好后,再将调节部与壳体2进行固定。It can be understood that the adjustment part is arranged in a column shape, and the adjustment part can be connected to the
第一抵接部与调节部连接,第一连接部朝向激光模组1的一面呈平面设置。第一抵接部的外沿背离激光模组1弯折设置,当微调旋钮5对激光模组1进行调节时,第一抵接部的外沿弯折设置可降低对激光模组1移动的干扰。The first abutting part is connected with the adjusting part, and the side of the first connecting part facing the
在一个示例中,弹性件6包括弹簧和第二抵接部,弹簧位于放置孔中;第二抵接部位于放置腔中,第二抵接部一面与弹簧连接且另一面与激光模组1抵接,第二抵接部的外沿朝向弹簧弯折设置。In one example, the
可以理解的是放置孔为盲孔设置,弹簧位于放置孔中,且一端与放置孔的孔底抵接,另一端伸入放置腔中与第二抵接部连接。第二连接部朝向激光模组1的一面呈平面设置。第二抵接部的外沿背离激光模组1弯折设置,当微调旋钮5对激光模组1进行调节时,第二抵接部的外沿弯折设置可降低对激光模组1移动的干扰。It can be understood that the placement hole is provided as a blind hole, the spring is located in the placement hole, one end abuts against the bottom of the placement hole, and the other end extends into the placement cavity to connect with the second abutting portion. The side of the second connecting portion facing the
进一步的,微调旋钮5设置有两个,两个微调旋钮5与弹性件6绕激光模组1呈圆周设置,两个微调旋钮5呈90°夹角,弹性件6与任意一个微调旋钮5的夹角呈135°设置。Further, there are two fine-
微调旋钮5设置有两个,两个微调旋钮5相邻设置,一个微调旋钮5与激光模组1中轴线的连线为A连线,另一个微调旋钮5与激光模组1中轴线的连线为B连线,其中A连线与B连线之间的内夹角为90°夹角。There are two fine-
弹性件6只设置一个,弹性件6与激光模组1中连线为C连线,A连线与C连线之间的内夹角为135°夹角,B连线与C连线之间的内夹角为135°夹角。Only one
微调旋钮5的两个设置以及角度设置,使用时,使用者可通过两个微调旋钮5进行调节,从而提高调节的精确性。弹性件6与两个微调旋钮5之间的夹角设置,使得弹性件6与两个微调旋钮5对激光模组1的支撑更加稳定。The two settings and the angle setting of the fine-
进一步的,调节环11设置于激光模组1远离激光发射的一端。即调节环11与微调旋钮5分别设置于激光模组1的两端,调节环11与调节球3控制激光模组1远离发射端的位置调节,微调旋钮5以及弹性件6用于精准调节激光模组1发射端的位置调节。调节环11、调节球3、微调旋钮5以及弹性件6对激光模组1与壳体2的相对位置进行配合调节,从而提高激光模组的光轴校准精度,提高稳定性。Further, the adjusting
应当指出,在说明书中提到的“一个实施例”、“实施例”、“示例性实施例”、“一些实施例”等表示所述的实施例可以包括特定特征、结构或特性,但未必每个实施例都包括该特定特征、结构或特性。此外,这样的短语未必是指同一实施例。此外,在结合实施例描述特定特征、结构或特性时,结合明确或未明确描述的其他实施例实现这样的特征、结构或特性处于本领域技术人员的知识范围之内。It should be noted that references in the specification to "one embodiment," "an embodiment," "exemplary embodiment," "some embodiments," etc. mean that the described embodiment may include a particular feature, structure, or characteristic, but not necessarily Each embodiment includes the particular feature, structure or characteristic. Moreover, such phrases are not necessarily referring to the same embodiment. Furthermore, when a particular feature, structure or characteristic is described in conjunction with one embodiment, it is within the knowledge of those skilled in the art to implement such feature, structure or characteristic in conjunction with other embodiments, expressly or not expressly described.
应当容易地理解,应当按照最宽的方式解释本公开中的“在……上”、“在……以上”和“在……之上”,以使得“在……上”不仅意味着“直接处于某物上”,还包括“在某物上”且其间具有中间特征或层的含义,并且“在……以上”或者“在……之上”不仅包括“在某物以上”或“之上”的含义,还可以包括“在某物以上”或“之上”且其间没有中间特征或层(即,直接处于某物上)的含义。It should be readily understood that "on", "over" and "on" in this disclosure should be interpreted in the broadest possible manner, such that "on" does not only mean "on" Directly on something" also includes the meaning of "on something" with intervening features or layers, and "above" or "over" includes not only "above something" or " The meaning of "over" can also include "above" or "over" without intervening features or layers (ie, directly on something).
此外,文中为了便于说明可以使用空间相对术语,例如,“下面”、“以下”、“下方”、“以上”、“上方”等,以描述一个元件或特征相对于其他元件或特征的如图所示的关系。空间相对术语意在包含除了附图所示的取向之外的处于使用或操作中的器件的不同取向。装置可以具有其他取向(旋转90度或者处于其他取向上),并且文中使用的空间相对描述词可以同样被相应地解释。In addition, spatially relative terms such as "below," "below," "below," "above," "above," etc. may be used herein for ease of description, to describe one element or feature relative to other elements or features as shown in the drawings. relationship shown. The spatially relative terms are intended to encompass different orientations of the device in use or operation in addition to the orientation shown in the figures. The device may be otherwise oriented (rotated 90 degrees or at other orientations) and the spatially relative descriptors used herein may likewise be interpreted accordingly.
需要说明的是,在本文中,诸如“第一”和“第二”等之类的关系术语仅仅用来将一个实体或者操作与另一个实体或操作区分开来,而不一定要求或者暗示这些实体或操作之间存在任何这种实际的关系或者顺序。而且,术语“包括”、“包含”或者其任何其他变体意在涵盖非排他性的包含,从而使得包括一系列要素的过程、方法、物品或者设备不仅包括那些要素,而且还包括没有明确列出的其他要素,或者是还包括为这种过程、方法、物品或者设备所固有的要素。在没有更多限制的情况下,由语句“包括一个……”限定的要素,并不排除在包括所述要素的过程、方法、物品或者设备中还存在另外的相同要素。It should be noted that, in this document, relational terms such as "first" and "second" etc. are only used to distinguish one entity or operation from another entity or operation, and do not necessarily require or imply these There is no such actual relationship or sequence between entities or operations. Moreover, the terms "comprising", "comprising" or any other variation thereof are intended to encompass a non-exclusive inclusion such that a process, method, article or device comprising a list of elements includes not only those elements, but also includes not explicitly listed or other elements inherent to such a process, method, article or apparatus. Without further limitation, an element qualified by the phrase "comprising a..." does not preclude the presence of additional identical elements in a process, method, article or apparatus that includes the element.
最后应说明的是:以上各实施例仅用以说明本申请的技术方案,而非对其限制;尽管参照前述各实施例对本申请进行了详细的说明,本领域的普通技术人员应当理解:其依然可以对前述各实施例所记载的技术方案进行修改,或者对其中部分或者全部技术特征进行等同替换;而这些修改或者替换,并不使相应技术方案的本质脱离本申请各实施例技术方案的范围。Finally, it should be noted that the above embodiments are only used to illustrate the technical solutions of the present application, but not to limit them; although the present application has been described in detail with reference to the foregoing embodiments, those of ordinary skill in the art should understand that: It is still possible to modify the technical solutions recorded in the foregoing embodiments, or perform equivalent replacements on some or all of the technical features; and these modifications or replacements do not make the essence of the corresponding technical solutions deviate from the technical solutions of the embodiments of the present application. scope.
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