Container type emergency helicopter parking apron

文档序号:1857288 发布日期:2021-11-19 浏览:39次 中文

阅读说明:本技术 一种集装箱式应急直升机停机坪 (Container type emergency helicopter parking apron ) 是由 黄洪田 张兆国 于 2021-08-18 设计创作,主要内容包括:本发明属于直升机停机坪技术领域,尤其为一种集装箱式应急直升机停机坪,包括集装箱框架,其特征在于,集装箱框架的顶端面固定设置有支撑板组件,集装箱框架的两侧对称设置有用于拓宽宽度的侧翼展开机构,且展开后的侧翼展开机构的顶端面与支撑板组件的顶端面位于同一水平面上,支撑板组件的顶端面设置有停机坪标识;通过将侧翼展开机构展开构成一个完整的直升机停机坪,进而可以通过改造现有的集装箱形成应急停机坪,可以供紧急救援的直升机临时停靠,较停靠在道路街区空旷地带更加安全可靠。(The invention belongs to the technical field of helicopter parking aprons, and particularly relates to a container type emergency helicopter parking apron which comprises a container frame and is characterized in that a supporting plate assembly is fixedly arranged on the top end surface of the container frame, side wing unfolding mechanisms for widening the width are symmetrically arranged on two sides of the container frame, the top end surface of each unfolded side wing unfolding mechanism and the top end surface of the supporting plate assembly are positioned on the same horizontal plane, and a parking apron mark is arranged on the top end surface of the supporting plate assembly; the side wing unfolding mechanism is unfolded to form a complete helicopter apron, so that an emergency apron can be formed by reforming the existing container, a helicopter for emergency rescue can be temporarily parked, and the emergency apron is safer and more reliable than the helicopter parked in an open area of a road block.)

1. The utility model provides an emergent helicopter air park of container formula, includes container frame (1), its characterized in that, the fixed supporting plate subassembly (2) that is provided with of top face of container frame (1), the bilateral symmetry of container frame (1) is provided with flank deployment mechanism (3) that are used for widening the width, and after expanding the top face of flank deployment mechanism (3) with the top face of supporting plate subassembly (2) is located same horizontal plane, the top face of supporting plate subassembly (2) is provided with air park sign (4).

2. The container-type emergency helicopter apron of claim 1, characterized in that: container frame (1) includes bottom plate (11), corner support column (12), horizontal back timber (13), two divisions of doors (14) and curb plate (15), the top end symmetry of bottom plate (11) is provided with a plurality of corner support column (12) is located bottom plate (11) length direction's two pass through between corner support column (12) curb plate (15) fixed connection is located bottom plate (11) width direction's two pass through between corner support column (12) horizontal back timber (13) fixed connection is located two of bottom plate (11) one end be provided with between corner support column (12) two divisions of doors (14).

3. The container-type emergency helicopter apron of claim 2, characterized in that: the top of corner support post (12) all is provided with mounting hole (121), corner support post (12) orientation equal fixed mounting in one side in the container frame (1) outside has fixing base (122).

4. The container-type emergency helicopter apron of claim 3, characterized in that: the side plates (15) and the cross top beams (13) face the inner side of the container frame (1) and are provided with a plurality of process grooves (151) in the vertical direction.

5. The container-type emergency helicopter apron of claim 4, characterized in that: the supporting plate assembly (2) comprises a top supporting plate (21) and a top plate (22), the top supporting plate (21) is installed at the top of the container frame (1), the top end of the top supporting plate (21) is welded with the top plate (22), and the top end face of the top plate (22) is provided with the parking apron mark (4).

6. The container-type emergency helicopter apron of claim 5, characterized in that: the top support plate (21) is of a hollow structure, and a plurality of V-shaped frameworks (211) are arranged in the top support plate (21) at equal intervals.

7. The container-type emergency helicopter apron of claim 6, characterized in that: the fixed a plurality of installing pins (212) that are provided with of bottom face of top backup pad (21), the bilateral symmetry of top backup pad (21) is provided with a plurality of articulated seats (213), the top surface of top backup pad (21) evenly is provided with a plurality of longerons (214) along length direction, the top face of top backup pad (21) evenly is provided with a plurality of crossbeams (215) along width direction.

8. The container-type emergency helicopter apron of claim 7, characterized in that: the cross beams (215) and the longitudinal beams (214) are arranged in a staggered mode, the top plates (22) are welded to the top end faces of the cross beams (215) and the longitudinal beams (214), the number of the cross beams (215) is five, and the number of the longitudinal beams (214) is three.

9. The container-type emergency helicopter apron of claim 8, characterized in that: flank deployment mechanism (3) include electric hydraulic cylinder (31) and flank board (32), electric hydraulic cylinder (31) with fixing base (122) are connected through the round pin axle rotation, electric hydraulic cylinder (31) are kept away from the one end of fixing base (122) with flank board (32) rotate to be connected, flank board (32) with articulated seat (213) are connected through the round pin axle rotation.

10. The container-type emergency helicopter apron of claim 9, characterized in that: the middle position of one side of flank board (32) is provided with rotates seat (321), flank board (32) orientation one side of container frame (1) is provided with fillet (322), flank board (32) are close to one side symmetry of fillet (322) is provided with roating seat (323).

Technical Field

The invention belongs to the technical field of helicopter parking aprons, and particularly relates to a container type emergency helicopter parking apron.

Background

The apron plays an important role as the main activity area of the helicopter. The helicopter landing pad is a field for taking off and landing the helicopter. Generally, the emergency rescue helicopter is fixedly built on the ground or the top layer of a building, and for the emergency rescue helicopter, the environment such as urban traffic, residential buildings and the like is not suitable for the parking of the helicopter, so that a suitable emergency shutdown place is difficult to find.

Therefore, a container type emergency helicopter apron is designed to solve the problems.

Disclosure of Invention

To solve the problems set forth in the background art described above. The invention provides a container type emergency helicopter parking apron which can be used for temporarily parking a helicopter for emergency rescue and has the characteristics of safety and reliability.

In order to achieve the purpose, the invention provides the following technical scheme: the utility model provides an emergent helicopter air park of container formula, includes container frame, its characterized in that, container frame's the fixed supporting plate subassembly that is provided with of top face, container frame's bilateral symmetry is provided with the flank deployment mechanism that is used for widening the width, and the top face of the flank deployment mechanism after the expansion is located same horizontal plane with supporting plate subassembly's top face, and supporting plate subassembly's top face is provided with the air park sign.

Preferably, the container type emergency helicopter apron comprises a bottom plate, corner support columns, a cross top beam, a double door and side plates, wherein the top end face of the bottom plate is symmetrically provided with the corner support columns, the two corner support columns in the length direction of the bottom plate are fixedly connected through the side plates, the two corner support columns in the width direction of the bottom plate are fixedly connected through the cross top beam, and the double door is arranged between the two corner support columns at one end of the bottom plate.

Preferably, the top ends of the corner support columns are provided with mounting holes, and one sides of the corner support columns facing the outer side of the container frame are fixedly provided with fixing seats.

As the preferable preference of the container type emergency helicopter apron, a plurality of process grooves are formed in the vertical direction on the side plates and the surfaces, facing the inner side of the container frame, of the cross beams.

The support plate assembly comprises a top support plate and a top plate, the top support plate is installed at the top of the container frame, the top of the top support plate is welded with the top plate, and the top end face of the top plate is provided with an apron mark.

Preferably, the container type emergency helicopter apron is of a hollow structure, and a plurality of V-shaped frameworks are arranged in the top supporting plate at equal intervals.

Preferably, the bottom end face of the top supporting plate is fixedly provided with a plurality of mounting pins, the two sides of the top supporting plate are symmetrically provided with a plurality of hinged seats, the top face of the top supporting plate is uniformly provided with a plurality of longitudinal beams along the length direction, and the top end face of the top supporting plate is uniformly provided with a plurality of cross beams along the width direction.

Preferably, the cross beams and the longitudinal beams are arranged in a staggered mode, top plates are welded to the top end faces of the cross beams and the longitudinal beams, the number of the cross beams is five, and the number of the longitudinal beams is three.

Preferably, the side wing unfolding mechanism comprises an electric hydraulic cylinder and a side wing plate, the electric hydraulic cylinder is rotatably connected with the fixed seat through a pin shaft, one end of the electric hydraulic cylinder, far away from the fixed seat, is rotatably connected with the side wing plate, and the side wing plate is rotatably connected with the hinged seat through a pin shaft.

Preferably, the container type emergency helicopter apron is characterized in that a rotating seat is arranged in the middle of one side of a side wing plate, a round angle is arranged on one side of the side wing plate, which faces a container frame, and rotating seats are symmetrically arranged on one side of the side wing plate, which is close to the round angle.

Compared with the prior art, the invention has the beneficial effects that:

through the both sides installation flank deployment mechanism at container body, and install supporting plate subassembly on the roof of container body, constitute a complete helicopter air park through launching flank deployment mechanism, and then can form emergent air park through reforming transform current container, the helicopter that can supply emergency rescue berths temporarily, it is safe and reliable more in road block spacious area to berth, in addition through the roof repacking into the supporting plate subassembly with the container, and then increased the holistic intensity of this container, make it to bear helicopter's weight.

Drawings

The accompanying drawings, which are included to provide a further understanding of the invention and are incorporated in and constitute a part of this specification, illustrate embodiments of the invention and together with the description serve to explain the principles of the invention and not to limit the invention. In the drawings:

FIG. 1 is a schematic structural view of the present invention;

FIG. 2 is a side view of FIG. 1 of the present invention;

FIG. 3 is a top view of FIG. 1 of the present invention;

FIG. 4 is a schematic view of the construction of the container frame of the present invention;

FIG. 5 is a schematic view of the top support plate of the present invention;

FIG. 6 is a cross-sectional view of FIG. 5 in accordance with the present invention;

FIG. 7 is a schematic structural view of a side wing panel according to the present invention;

FIG. 8 is a schematic structural view of a top plate according to the present invention;

in the figure:

1. a container frame; 11. a base plate;

12. corner support columns; 121. mounting holes; 122. a fixed seat;

13. a cross-top beam; 14. double doors are opened;

15. a side plate; 151. a process tank;

2. a support plate assembly; 21. a top support plate; 211. a V-shaped framework; 212. mounting a pin; 213. a hinged seat; 214. a stringer; 215. a cross beam;

22. a top plate;

3. a side wing unfolding mechanism; 31. an electric hydraulic cylinder;

32. a side wing panel; 321. a rotating seat; 322. round corners; 323. a rotating base;

4. and identifying the parking apron.

Detailed Description

The technical solutions in the embodiments of the present invention will be clearly and completely described below with reference to the drawings in the embodiments of the present invention, and it is obvious that the described embodiments are only a part of the embodiments of the present invention, and not all of the embodiments. All other embodiments, which can be derived by a person skilled in the art from the embodiments given herein without making any creative effort, shall fall within the protection scope of the present invention.

As shown in fig. 1;

the utility model provides an emergent helicopter air park of container formula, includes container frame 1, its characterized in that, container frame 1's the fixed supporting plate subassembly 2 that is provided with of top face, container frame 1's both sides symmetry is provided with the flank deployment mechanism 3 that is used for widening the width, and the top face of the flank deployment mechanism 3 after the expansion is located same horizontal plane with the top face of backup pad subassembly 2, and the top face of backup pad subassembly 2 is provided with air park sign 4.

In this embodiment: through the both sides installation flank deployment mechanism 3 at the container body, and install backup pad subassembly 2 on the roof of container body, constitute a complete helicopter air park through launching flank deployment mechanism 3, and then can form emergent air park through reforming transform current container, the helicopter that can supply emergency rescue berths temporarily, it is safe and reliable more in the spacious area in road block to berth, in addition through the roof repacking into backup pad subassembly 2 with the container, and then increased the holistic intensity of this container, make it to bear helicopter's weight.

It should be noted that: and the top end surface of the supporting plate component 2 is provided with an apron mark 4, so that a helicopter pilot can conveniently observe the helicopter when the helicopter stops.

As shown in fig. 4;

in an alternative embodiment: container frame 1 includes bottom plate 11, corner support column 12, horizontal top beam 13, two divisions of doors 14 and curb plate 15, bottom plate 11's top end face symmetry is provided with a plurality of corner support columns 12, be located through curb plate 15 fixed connection between 11 length direction's of bottom plate two corner support columns 12, be located through horizontal top beam 13 fixed connection between 11 width direction's of bottom plate two corner support columns 12, be located and be provided with two divisions of doors 14 between 11 one end of bottom plate two corner support columns 12, the top of corner support column 12 all is provided with mounting hole 121, there is fixing base 122 corner support column 12 towards the equal fixed mounting in one side in the container frame 1 outside.

In this embodiment: through mounting hole 121 and then can install supporting plate subassembly 2 on container frame 1's top, cooperate through corner support column 12 and crossbeam 13 and curb plate 15 to make container frame 1's structure more firm, through setting up crossbeam 13 and then can increase container frame 1's bearing capacity.

It should be noted that: the side plates 15 and the side faces of the cross beams 13 facing the inner side of the container frame 1 are both provided with a plurality of process grooves 151 in the vertical direction.

As shown in fig. 2 and 5 and 6;

in an alternative embodiment: the support plate assembly 2 comprises a top support plate 21 and a top plate 22, the top support plate 21 is installed at the top of the container frame 1, the top of the top support plate 21 is welded with the top plate 22, the top end face of the top plate 22 is provided with an apron mark 4, the bottom end face of the top support plate 21 is fixedly provided with a plurality of installation pins 212, the bilateral symmetry of the top support plate 21 is provided with a plurality of hinged seats 213, the top face of the top support plate 21 is evenly provided with a plurality of longitudinal beams 214 along the length direction, and the top end face of the top support plate 21 is evenly provided with a plurality of cross beams 215 along the width direction.

It should be noted that: the top support plate 21 is of a hollow structure, a plurality of V-shaped frameworks 211 are arranged in the top support plate 21 at equal intervals, transverse beams 215 and longitudinal beams 214 are arranged in a staggered mode, top plates 22 are welded to the top end faces of the transverse beams 215 and the longitudinal beams 214, the number of the transverse beams 215 is five, and the number of the longitudinal beams 214 is three.

In this embodiment: by welding the top plate 22 to the top support plate 21 and alternately arranging the cross beam 215 and the longitudinal beam 214 between the top plate 22 and the top support plate 21, the structural strength of the support plate assembly 2 is increased, and the weight of the top support plate 21 is reduced to a certain extent by adopting a hollow structure.

As shown in fig. 2 and 7;

in an alternative embodiment: flank deployment mechanism 3 includes electric hydraulic cylinder 31 and flank board 32, and electric hydraulic cylinder 31 is connected through the round pin axle rotation with fixing base 122, and electric hydraulic cylinder 31 is kept away from the one end of fixing base 122 and is connected with the flank board 32 rotation, and the flank board 32 is connected through the round pin axle rotation with articulated seat 213.

It should be noted that: the one side middle part position of flank board 32 is provided with rotates seat 321, it is connected through the round pin rotation with electric hydraulic cylinder 31's top to rotate seat 321, flank board 32 is provided with fillet 322 towards one side of container frame 1, a side symmetry that flank board 32 is close to fillet 322 is provided with roating seat 323, roating seat 323 is connected through the round pin rotation with articulated seat 213, one side that flank board 32 is close to the roof simultaneously sets up the fillet, and then can make that flank board 32 can be smooth and easy rotate around articulated seat 213, roof 22 all is provided with the frosting with the top surface of flank board 32, in order to increase frictional force.

In this embodiment: the electric hydraulic cylinder 31 can be controlled to start through the vehicle-mounted control end, so that the side wing plates 32 are unfolded until the side wing plates 32 are level with the top plate 22, and the two side wing plates 32 are unfolded to be matched with the top plate 32 to form a complete parking apron.

In addition, one side of the container frame 1 can be additionally provided with navigation aid equipment, such as: navigation management communication equipment, meteorological facilities, fire rescue equipment and the like, so that the helicopter safety take-off and landing requirements can be met.

Finally, it should be noted that: although the present invention has been described in detail with reference to the foregoing embodiments, it will be apparent to those skilled in the art that changes may be made in the embodiments and/or equivalents thereof without departing from the spirit and scope of the invention. Any modification, equivalent replacement, or improvement made within the spirit and principle of the present invention should be included in the protection scope of the present invention.

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