阅读说明：本技术 一种航空铝合金停机坪及安装方法 (Aviation aluminum alloy parking apron and installation method ) 是由 鲍海鸥 于 2020-12-08 设计创作，主要内容包括：本发明公开了一种航空铝合金停机坪及安装方法,包括底板、铝合金型材、扣板和紧固螺栓,所述底板的顶部安装有铝合金型材,铝合金型材底部支脚的左右两侧均卡接有扣板,扣板上螺纹连接有紧固螺栓,紧固螺栓的表面位于扣板的上方和底板的下方均螺纹连接有螺母,所述铝合金型材的顶部固定连接有用于防滑的防滑凸条,所述铝合金型材的顶部左侧开设有不规则的卡槽,所述铝合金型材的顶部右侧固定连接有卡块。本发明通过Y字型材构成的铝合金停机坪结构轻便,稳定,节省了材料,同时整体停机坪重量变轻,降低了大楼整体承载要求,节省了大量资源,安装过程中扣板的使用,使得现场工作尽量的减少复杂的钻孔和反转搬移,节省了大量施工时间。(The invention discloses an aviation aluminum alloy parking apron and an installation method thereof, and the aviation aluminum alloy parking apron comprises a bottom plate, aluminum alloy sections, a buckle plate and fastening bolts, wherein the aluminum alloy sections are installed at the top of the bottom plate, the buckle plate is clamped at the left side and the right side of a support leg at the bottom of the aluminum alloy sections, the fastening bolts are in threaded connection with the buckle plate, nuts are in threaded connection with the surfaces of the fastening bolts above the buckle plate and below the bottom plate, anti-skid convex strips for skid resistance are fixedly connected to the top of the aluminum alloy sections, irregular clamping grooves are formed in the left side of the top of the aluminum alloy sections, and clamping blocks are fixedly connected to the. The aluminum alloy parking apron formed by the Y-shaped section is light and stable in structure, materials are saved, meanwhile, the whole parking apron is light in weight, the whole bearing requirement of a building is lowered, a large number of resources are saved, the buckle plate is used in the installation process, complex drilling and reverse moving are reduced as much as possible in field work, and a large amount of construction time is saved.)

1. The utility model provides an aviation aluminum alloy air park, its characterized in that, includes bottom plate, aluminum alloy ex-trusions, buckle and fastening bolt, aluminum alloy ex-trusions is installed at the top of bottom plate, and the equal joint in the left and right sides of aluminum alloy ex-trusions bottom stabilizer blade has the buckle, and threaded connection has fastening bolt on the buckle, and fastening bolt's the equal threaded connection in below of the top that is located the buckle and bottom plate in surface has the nut, aluminum alloy ex-trusions's top fixedly connected with is used for skid-proof anti-skidding sand grip, irregular draw-in groove has been seted up on aluminum alloy ex-trusions's top left side, aluminum alloy ex-trusions's top right.

2. The aviation aluminum alloy air park according to claim 1, wherein a damping plate is arranged on the top of the bottom plate below the aluminum alloy section, and the thickness of the damping plate is not less than two centimeters.

3. The aviation aluminum alloy tarmac as claimed in claim 1, wherein the aluminum alloy profile is of a Y-shaped structure, so that structural stability is ensured, the bearable weight is increased, and the material usage amount is reduced.

4. The aviation aluminum alloy parking apron according to claim 1, wherein waterproof glue is coated on the surface of the aluminum alloy section bar, so that the waterproof function can be achieved.

5. The aviation aluminum alloy parking apron according to claim 1, wherein a protruding clamping block is arranged at a bottom supporting leg of the aluminum alloy section, and the protruding clamping block is clamped with the buckling plate.

6. The aviation aluminum alloy air park according to claim 1, wherein the aluminum alloy section is wide in upper surface and narrow in lower surface, and after the upper surface is embedded, extruded and assembled, a wider gap is formed between the lower surfaces.

7. The mounting method of the aviation aluminum alloy parking apron is characterized by comprising the following steps of,

101, marking and aligning an aluminum alloy deck, and hoisting the aluminum alloy deck by using hoisting equipment;

102, paving a steel structure on the site, and drilling a steel structure secondary beam by using a magnetic electric drill;

103, installing the upper aluminum alloy deck and the lower aluminum alloy deck which are hoisted in pairs, and extruding the aluminum alloy decks by using a hydraulic jack for fixed assembly;

104, after the aluminum alloy deck is matched, fixedly mounting the aluminum alloy deck and the steel structure secondary beam through bolts;

and 105, sequentially combining a plurality of aluminum alloy decks to form the complete parking apron.

8. The method for installing the aviation aluminum alloy parking apron according to claim 7, wherein the aluminum alloy decks which are hoisted are installed in pairs, and the aluminum alloy deck is fixedly assembled by extruding the aluminum alloy decks through a hydraulic jack, wherein the aluminum alloy decks and the aluminum alloy decks are sealed through 3M adhesive tapes.

9. The method for installing the aviation aluminum alloy parking apron according to claim 7, wherein the steel structure is laid on the site, and the steel structure secondary beam is drilled by using a magnetic electric drill, and the step of fixing the aluminum alloy section by a buckle plate and then drilling is carried out.

Technical Field

The invention relates to the technical field of air park, in particular to an aviation aluminum alloy air park and an installation method.

Background

The parking apron is a place for parking the airplane and various maintenance activities, and the arrangement of the parking (maintenance) apron needs to consider the blowing influence of airflow during the test of the airplane besides the different requirements of maintenance equipment so as to provide the place for parking the airplane and carrying out various business activities. It can pose a threat to parked, taxiing aircraft, ground equipment and personnel.

The traditional air park is mostly of a concrete structure, cracks and peels after long time, the service life is about five years, the weight of the concrete structure is large, if the air park is built on a roof and needs to be reinforced, the damping effect is poor, the air park is complex in field work, and multiple times of drilling and reverse moving are needed, so that the problem is solved by the aid of the aviation aluminum alloy air park and the installation method.

Disclosure of Invention

In order to overcome the problems in the related art, the embodiment of the invention provides an aviation aluminum alloy parking apron and an installation method thereof, and solves the problems of complex installation and poor bearing effect of the existing parking apron.

The embodiment of the invention provides an aviation aluminum alloy parking apron which comprises a bottom plate, aluminum alloy sections, a buckle plate and fastening bolts, wherein the aluminum alloy sections are installed at the top of the bottom plate, the buckle plate is clamped on the left side and the right side of supporting legs at the bottom of the aluminum alloy sections, the fastening bolts are connected onto the buckle plate in a threaded mode, nuts are connected onto the surfaces of the fastening bolts, the surfaces of the fastening bolts are located above the buckle plate and below the bottom plate in a threaded mode, anti-skid convex strips used for skid resistance are fixedly connected onto the top of the aluminum alloy sections, irregular clamping grooves are formed in the left side of the top of the aluminum alloy sections, clamping blocks are fixedly connected onto the right side of the.

Further, the top of bottom plate is located the below of aluminum alloy ex-trusions and is provided with the damper plate, and the damper plate thickness is no less than two centimeters.

Furthermore, the aluminum alloy section bar is of a Y-shaped structure, so that the structural stability is ensured, the bearable weight is improved, and the material usage amount is reduced.

Furthermore, waterproof glue is coated on the surface of the aluminum alloy section, so that the waterproof effect can be achieved.

Furthermore, a protruding clamping block is arranged at the bottom supporting leg of the aluminum alloy section, and the protruding clamping block is clamped with the buckling plate.

Furthermore, the upper surface of the aluminum alloy section is wide, the lower surface of the aluminum alloy section is narrow, and after the aluminum alloy section is embedded, extruded and assembled on the upper surface, a wide gap is formed between the lower surfaces.

An installation method of an aviation aluminum alloy parking apron comprises the following steps,

101, marking and aligning an aluminum alloy deck, and hoisting the aluminum alloy deck by using hoisting equipment;

102, paving a steel structure on the site, and drilling a steel structure secondary beam by using a magnetic electric drill;

103, installing the upper aluminum alloy deck and the lower aluminum alloy deck which are hoisted in pairs, and extruding the aluminum alloy decks by using a hydraulic jack for fixed assembly;

104, after the aluminum alloy deck is matched, fixedly mounting the aluminum alloy deck and the steel structure secondary beam through bolts;

and 105, sequentially combining a plurality of aluminum alloy decks to form the complete parking apron.

Further, the aluminum alloy deck and the aluminum alloy deck are sealed through a 3M adhesive tape.

Further, the aluminum alloy section is fixed through the pinch plate, and then drilling is conducted.

The technical scheme provided by the embodiment of the invention has the following beneficial effects: the aluminum alloy parking apron formed by the Y-shaped section is light and stable in structure, materials are saved, meanwhile, the weight of the whole parking apron is light, the integral bearing requirement of a building is lowered, a large number of resources are saved, the buckle plate is used in the installation process, complex drilling and reverse moving are reduced as far as possible in field work, and a large amount of construction time is saved.

It is to be understood that both the foregoing general description and the following detailed description are exemplary and explanatory only and are not restrictive of the invention, as claimed.

Drawings

The accompanying drawings, which are incorporated in and constitute a part of this specification, illustrate embodiments consistent with the invention and together with the description, serve to explain the principles of the invention.

FIG. 1 is a schematic structural diagram of an aviation aluminum alloy air park in an embodiment of the invention.

FIG. 2 is a flow chart of an installation method of an aviation aluminum alloy tarmac in the embodiment of the invention.

Detailed Description

Reference will now be made in detail to the exemplary embodiments, examples of which are illustrated in the accompanying drawings. When the following description refers to the accompanying drawings, like numbers in different drawings represent the same or similar elements unless otherwise indicated. The embodiments described in the following exemplary embodiments do not represent all embodiments consistent with the present invention. Rather, they are merely examples of apparatus, and associated applications, methods consistent with certain aspects of the invention, as detailed in the following claims.

FIG. 1 is a schematic structural diagram of an aviation aluminum alloy parking apron in an embodiment of the invention, as shown in FIG. 1, the aviation aluminum alloy parking apron comprises a bottom plate 1, an aluminum alloy section 3, a buckle plate 4 and a fastening bolt 5, the aluminum alloy section is mounted at the top of the bottom plate, a damping plate 2 is arranged at the top of the bottom plate and below the aluminum alloy section, the thickness of the damping plate is not less than two centimeters, the aluminum alloy section is in a Y-shaped structure, the stable structure is ensured, the borne weight is improved, and the material usage amount is reduced, compared with the traditional trapezoid structure, the borne weight of the Y-shaped structure is higher, so that a heavier parking apron can be built by using less materials, a large amount of materials are saved, a large amount of weight is saved, the requirement on the integral structure of a building is also reduced, a large amount of construction cost is saved additionally, the buckle plates are clamped at the left side and the right side, the bottom stand bar of the aluminum alloy section is provided with a raised clamping block which is clamped with the pinch plate.

The buckle plate is in threaded connection with a fastening bolt, the surface of the fastening bolt is positioned above the buckle plate and below the bottom plate and is in threaded connection with a nut 6, the top of the aluminum alloy section is fixedly connected with an anti-skid raised strip 7 for skid resistance, the left side of the top of the aluminum alloy section is provided with an irregular clamping groove 8, the right side of the top of the aluminum alloy section is fixedly connected with a clamping block 9, and two adjacent clamping grooves and clamping blocks are clamped and connected, so that the aluminum alloy section can be tightly connected after being assembled, the surface of the aluminum alloy section is coated with waterproof glue and can play a waterproof role, the upper surface of the aluminum alloy section is wide, the lower surface of the aluminum alloy section is narrow, after the aluminum alloy section is embedded, extruded and assembled on the upper surface, a wider gap is formed between the lower surfaces, the aluminum alloy section can be conveniently installed on a steel structure in a larger space, a plurality of materials are saved, therefore, the requirement on the integral bearing of the building is reduced, the integral structure of the building does not need to be reinforced, and a large amount of construction cost is saved.

Fig. 2 is a flow chart of an aviation aluminum alloy tarmac installation method in an embodiment of the invention, and as shown in fig. 2, the aviation aluminum alloy tarmac installation method includes the following steps,

101, marking and aligning an aluminum alloy deck, and hoisting the aluminum alloy deck by using hoisting equipment.

102, paving a steel structure on the site, drilling the steel structure secondary beam by using a magnetic electric drill, fixing the aluminum alloy section through a buckle plate, and then drilling.

The installation method is innovated, the difficulty of drilling on the aluminum alloy section bar in a construction site is high, the section bar needs to be reversed, then the hole is drilled through an electric drill, the section bar is reversed and installed after the hole is drilled, the steps are troublesome, the clamp plate is fixed through the illustration buckle plate, the hole can be drilled in a factory in advance, the hole does not need to be drilled on the section bar in the site, and therefore a large amount of construction time is saved.

103, installing the upper aluminum alloy deck and the lower aluminum alloy deck which are hoisted in pairs, extruding the aluminum alloy decks by using hydraulic jacks to fixedly assemble, and sealing the aluminum alloy decks by using a 3M adhesive tape.

And step 104, after the aluminum alloy deck is matched, fixedly mounting the aluminum alloy deck and the steel structure secondary beam through bolts.

And 105, sequentially combining a plurality of aluminum alloy decks to form the complete parking apron.

The field installation mode is that single installation concatenation is carried it to the secondary beam through electric hoist or manual work on, with the steel construction match brill and assembly, the installation order is installed by the right side left side direction.

Other embodiments of the invention will be apparent to those skilled in the art from consideration of the specification and practice of the invention disclosed herein. This application is intended to cover any variations, uses, or adaptations of the invention following, in general, the principles of the invention and including such departures from the present disclosure as come within known or customary practice within the art to which the invention pertains.

It will be understood that the invention is not limited to the precise arrangements described above and shown in the drawings and that various modifications and changes may be made without departing from the scope thereof. The scope of the invention is limited only by the appended claims.