CN201934430U - Transitional connecting device - Google Patents
Transitional connecting device Download PDFInfo
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- CN201934430U CN201934430U CN 201120041471 CN201120041471U CN201934430U CN 201934430 U CN201934430 U CN 201934430U CN 201120041471 CN201120041471 CN 201120041471 CN 201120041471 U CN201120041471 U CN 201120041471U CN 201934430 U CN201934430 U CN 201934430U
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Abstract
本实用新型涉及一种过渡连接装置,特别是关于一种应用于飞机与飞机保障设备过渡的连接装置。本实用新型最大的特点是单耳耳片的底座一侧开“U”型槽、另一侧开斜圆孔(现有技术过渡连接装置两侧均为圆柱孔),斜圆孔中心线方向向下延长将远离耳片。本实用新型过渡连接装置结构形式巧妙、连接安全可靠,并且可以有效实现飞机保障设备与飞机预留连接孔小空间间距且中心线异面的过渡连接问题。所以,具有较大的实用价值。
The utility model relates to a transition connection device, in particular to a connection device used in the transition between aircraft and aircraft support equipment. The biggest feature of the utility model is that one side of the base of the single-ear lug has a "U"-shaped groove, and the other side has an oblique round hole (both sides of the transition connection device in the prior art are cylindrical holes), and the direction of the centerline of the oblique round hole Extending down will move away from the tabs. The transitional connection device of the utility model has ingenious structural form, safe and reliable connection, and can effectively realize the transitional connection problem of the small space distance between the aircraft support equipment and the reserved connection hole of the aircraft and the centerlines are different planes. Therefore, it has great practical value.
Description
技术领域technical field
本实用新型涉及一种过渡连接装置,特别是关于一种应用于飞机与飞机保障设备过渡的连接装置。The utility model relates to a transition connection device, in particular to a connection device used in the transition between aircraft and aircraft support equipment.
背景技术Background technique
为了安全稳定,飞机保障设备使用时经常需要与飞机经连接,连接需要用到过渡连接装置。现有飞机保障设备的过渡连接装置主要有单耳连接和双耳连接。由于飞机预留的连接孔的间距一般相对较大,且连接孔的中心线基本平行,所以与之配合的单耳或双耳底座的连接孔间距也相对较大,且连接孔中心线也基本平行。For the sake of safety and stability, aircraft support equipment often needs to be connected to the aircraft when in use, and a transition connection device is required for the connection. The transition connection devices of existing aircraft support equipment mainly include single-ear connection and binaural connection. Since the spacing of the connection holes reserved by the aircraft is generally relatively large, and the centerlines of the connection holes are basically parallel, the spacing of the connection holes of the matching single-ear or double-ear base is also relatively large, and the centerline of the connection holes is also basically parallel.
然而,在实际工程应用中,由于飞机结构限制,有时飞机上预留的连接孔位置的间距很小且孔中心线不平行,有较大的空间异面夹角。如果使用常规单耳或双耳过渡连接装置,会出现螺栓连接时与耳片干涉而无法穿过连接孔。所以,现有过渡连接装置不能实现飞机保障设备与飞机预留小空间间距且中心线异面的连接孔的过渡连接要求。因此急需一种过渡连接装置,以满足上述小空间内飞机与飞机保障设备的连接要求。However, in practical engineering applications, due to the limitations of the aircraft structure, sometimes the spacing between the reserved connection holes on the aircraft is very small and the centerlines of the holes are not parallel, resulting in a large angle between different planes in space. If a conventional one-ear or two-ear transition connection device is used, the bolts will interfere with the lugs during connection and cannot pass through the connection hole. Therefore, the existing transitional connection device cannot meet the transitional connection requirements of the aircraft support equipment and the aircraft with a small space reserved for the connection hole with a different plane of the center line. Therefore, there is an urgent need for a transition connection device to meet the connection requirements between the aircraft and the aircraft support equipment in the above-mentioned small space.
发明内容Contents of the invention
本实用新型的目的:为了解决现有技术过渡连接装置无法实现小空间内飞机与飞机保障设备的过渡连接,本实用新型提供了一种安全可靠的且可以在小空间内实现飞机与飞机保障设备过渡连接的过渡连接装置。The purpose of this utility model: in order to solve the problem that the existing transition connection device cannot realize the transition connection between the aircraft and the aircraft support equipment in a small space, the utility model provides a safe and reliable and can realize the aircraft and aircraft support equipment in a small space A transition connection for a transition connection.
本实用新型的技术方案:Technical scheme of the utility model:
一种过渡连接装置,包括单耳耳片1、底座6、第一斜垫片2、第一螺栓3、第二垫片4、第二螺栓5;其中,所述底座6一侧开“U”型槽,另一侧开斜圆孔,第一螺栓(3)依次穿过第一斜垫片2、底座的“U”型槽,第二螺栓5依次穿过第二斜垫片4、底座的斜圆孔,第一螺栓(3)和第二螺栓5的直径相同,长度不同,底座的“U”型槽的宽度与斜圆孔的直径相等。A transitional connection device, including a single-ear lug 1, a
优选地,所述底座“U”型槽的中心线与斜圆孔的中心线有空间异面角。Preferably, the centerline of the "U"-shaped groove of the base and the centerline of the oblique circular hole have spatially different angles.
优选地,所述底座的斜圆孔中心线方向向下延长将远离耳片。Preferably, the downward extension of the centerline of the oblique circular hole of the base will be away from the lugs.
优选地,第一螺栓(3)和第二螺栓5的直径比斜圆孔的直径小1mm。Preferably, the diameters of the first bolt (3) and the
本实用新型的优点:本实用新型过渡连接装置结构形式巧妙、连接安全可靠,并且可以有效实现飞机保障设备与飞机预留连接孔小空间间距且中心线异面的过渡连接问题。所以,具有较大的实用价值。The advantages of the utility model: the transition connection device of the utility model is ingenious in structure, safe and reliable in connection, and can effectively realize the transition connection problem of aircraft support equipment and aircraft reserved connection holes with small space spacing and different centerlines. Therefore, it has great practical value.
附图说明:Description of drawings:
图1是本实用新型过渡连接装置一较佳实施方式的结构示意图;Fig. 1 is a structural schematic diagram of a preferred embodiment of the utility model transition connection device;
图2是本实用新型过渡连接装置一较佳实施方式的侧向示意图。Fig. 2 is a schematic side view of a preferred embodiment of the transition connection device of the present invention.
其中,1耳片,2第一斜垫片,3第一螺栓,4第二斜垫片,5第二螺栓,6底座。Among them, 1 lug, 2 first slanted gasket, 3 first bolt, 4 second slanted gasket, 5 second bolt, 6 base.
具体实施方式:下面结合附图对本过渡连接装置做一详细说明。DETAILED DESCRIPTION OF THE PREFERRED EMBODIMENTS: The transition connection device will be described in detail below in conjunction with the accompanying drawings.
一种过渡连接装置,包括单耳耳片1、底座6、第一斜垫片2、第一螺栓3、第二垫片4、第二螺栓5;其中,所述底座6一侧开“U”型槽,另一侧开斜圆孔,第一螺栓(3)依次穿过第一斜垫片2、底座的“U”型槽,第二螺栓5依次穿过第二斜垫片4、底座的斜圆孔,第一螺栓(3)和第二螺栓5的直径相同,长度不同,底座的“U”型槽的宽度与斜圆孔的直径相等。A transitional connection device, including a single-ear lug 1, a
优选地,所述底座“U”型槽的中心线与斜圆孔的中心线有空间异面角。Preferably, the centerline of the "U"-shaped groove of the base and the centerline of the oblique circular hole have spatially different angles.
优选地,所述底座的斜圆孔中心线方向向下延长将远离耳片。Preferably, the downward extension of the centerline of the oblique circular hole of the base will be away from the lugs.
优选地,第一螺栓(3)和第二螺栓5的直径比斜圆孔的直径小1mm。Preferably, the diameters of the first bolt (3) and the
本实用新型最大的特点是单耳耳片1的底座6一侧开“U”型槽、另一侧开斜圆孔(现有技术过渡连接装置两侧均为圆柱孔),斜圆孔中心线方向向下延长将远离耳片。使用时,先将与耳片1有干涉的螺栓3带着第一斜垫片4初步拧入飞机内预留的托板螺母内(保留一定余量),再将耳片“U”型槽卡在第一螺栓3上,此时第一螺栓3已基本位于耳片1根部;将耳片1底座斜圆孔与飞机预留连接孔对齐,再将第二螺栓5带第二斜垫片4插入斜圆孔内直至完全拧入飞机预留的托板螺母里。最后,拧紧第一螺栓5。至此实现了飞机保障设备与飞机的过渡连接。The biggest feature of the utility model is that one side of the
本实用新型过渡连接装置结构形式巧妙、连接安全可靠,并且可以有效实现飞机保障设备与飞机预留连接孔小空间间距且中心线异面的过渡连接问题。所以,具有较大的实用价值。The transitional connection device of the utility model has ingenious structural form, safe and reliable connection, and can effectively realize the transitional connection problem of the small space distance between the aircraft support equipment and the reserved connection hole of the aircraft and the centerlines are different planes. Therefore, it has great practical value.
Claims (4)
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120041471 CN201934430U (en) | 2011-02-17 | 2011-02-17 | Transitional connecting device |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| CN 201120041471 CN201934430U (en) | 2011-02-17 | 2011-02-17 | Transitional connecting device |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| CN201934430U true CN201934430U (en) | 2011-08-17 |
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Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| CN 201120041471 Expired - Lifetime CN201934430U (en) | 2011-02-17 | 2011-02-17 | Transitional connecting device |
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| Country | Link |
|---|---|
| CN (1) | CN201934430U (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104864032A (en) * | 2015-05-08 | 2015-08-26 | 李理 | Damping shaft-fixing device for driving shaft of train |
| CN105020213A (en) * | 2015-07-14 | 2015-11-04 | 苏州柏德纳科技有限公司 | T-shaped connection seat |
-
2011
- 2011-02-17 CN CN 201120041471 patent/CN201934430U/en not_active Expired - Lifetime
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN104864032A (en) * | 2015-05-08 | 2015-08-26 | 李理 | Damping shaft-fixing device for driving shaft of train |
| CN105020213A (en) * | 2015-07-14 | 2015-11-04 | 苏州柏德纳科技有限公司 | T-shaped connection seat |
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| C14 | Grant of patent or utility model | ||
| GR01 | Patent grant | ||
| CX01 | Expiry of patent term |
Granted publication date: 20110817 |
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| CX01 | Expiry of patent term |
