A spherical expandable multi-chamber inflatable target

The spherical expandable multi-chamber inflatable target addresses inefficiencies in traditional targets by providing a durable, rapidly deployable design with improved radar reflection and multiple-use capabilities, enhancing training effectiveness and resource utilization.

CN111637799BActive Publication Date: 2024-12-24MAANSHAN HUAQIVIA TECH DEV CO LTD
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Patent Information

Application Number
CN202010621871.0
Authority / Receiving Office
CN · China
Patent Type
Patents(China)
Current Assignee / Owner
Filing Date
2020-06-30
Publication Date
2024-12-24
Estimated Expiration
2040-06-30

AI Technical Summary

Technical Problem

Traditional maritime targets are costly, slow to deploy, difficult to recover, and inefficient, with inflatable targets failing upon damage, wasting resources and disrupting training exercises.

Method used

A spherical expandable multi-chamber inflatable target with a four-independent cabin design, featuring flexible radar reflectors and a deployable airbag structure, allowing multiple uses and rapid deployment with improved radar reflection capabilities.

Benefits of technology

Enhances shooting accuracy and efficiency by enabling multiple deployments, rapid setup, and extended service life through a durable design that maintains functionality even after partial damage.

✦ Generated by Eureka AI based on patent content.

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Abstract

The invention discloses a spherical deployable multi-chamber inflatable target, comprising a flexible spherical deployable multi-chamber inflatable airbag, a sealable operating port is arranged on the flexible spherical deployable multi-chamber inflatable airbag, a plurality of flexible cabin isolation layers are arranged on the inner side of the flexible spherical deployable multi-chamber inflatable airbag, a plurality of inflation valves and a plurality of pressure relief valves are fixedly installed on the flexible spherical deployable multi-chamber inflatable airbag, and six flexible deployable radar reflectors are installed in independent cabins; the twenty-four flexible deployable radar reflectors arranged inside the target can ensure that radar signals can be reflected at any direction and angle, the target has high shooting accuracy, is convenient for storage and preservation, can be quickly assembled when in use, can arrange multiple shooting targets at the same time, the target has a long service life, can continue to work even if one cabin is hit, thus improving training efficiency, and can be repeatedly used through simple maintenance.
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Description

Technical Field

[0001] The invention relates to a target, in particular to a spherical expandable multi-chamber inflatable target. Background Art

[0002] Targets provide maritime targets for naval artillery, missile live-fire shooting or simulation training, and are important maritime equipment for maritime target shooting training and exercises, as well as for testing and evaluating the strike effect. Therefore, the development, product iteration and deployment of targets are of great significance to the development of naval weapon equipment technology and the improvement of combat capabilities. Traditional targets generally use abandoned ships, requisitioned civilian fishing boats and special steel-structured target ships, which are costly, slow to deploy at sea, slow to recover, difficult to tow, pollute the ocean, and cannot be deployed on a large scale. The existing inflatable ball targets are simple and fast to deploy, but once they are damaged or scratched by external forces, the internal air pressure of the entire inflatable ball target is insufficient, and the inflatable ball target immediately fails and must be re-deployed, wasting personnel, time, financial resources, and seriously affecting the progress of training or exercise subjects. Summary of the invention

[0003] In order to solve the above-mentioned technical problems, the present invention provides a spherical expandable multi-chamber inflatable target. The present invention adopts a four-independent cabin design, that is, when one part is hit or damaged, it will not affect the appearance and use of other independent cabins, and it can be deployed once and used multiple times. It is more convenient and efficient than traditional offshore floating targets. The twenty-four flexible and deployable radar reflectors arranged inside the target have a total of seventy-two reflecting surfaces, which can ensure that radar signals can be reflected at any direction and angle, greatly improving the shooting accuracy; the present invention adopts an inflatable airbag as a target, which is convenient to store and keep, and can be quickly assembled when used. Multiple shooting targets can be deployed at the same time. The target has a long service life and can be reused many times through simple maintenance. The existing inflatable ball airbag floating target has a simple and fast deployment method, but once it is damaged or hit once due to external force, the air pressure in the entire inflatable ball airbag target body is insufficient, and the target body immediately fails and must be re-deployed, wasting personnel, time, financial resources and other resources, and seriously affecting the technical problems of the progress of training or exercise subjects.

[0004] The purpose of the present invention can be achieved through the following technical solutions:

[0005] A spherical deployable multi-chamber inflatable target, comprising a flexible spherical deployable multi-chamber inflatable airbag, the outer surface of which is provided with two reinforcing ropes, the flexible spherical deployable multi-chamber inflatable airbag is provided with a sealable operating port, a plurality of D-shaped pull rings are fixedly installed on the outer surface of the flexible spherical deployable multi-chamber inflatable airbag, and a towing cable is fixedly installed on one of the D-shaped pull rings;

[0006] A plurality of flexible cabin isolation layers are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag, and an independent cabin is enclosed between two adjacent flexible cabin isolation layers and the flexible spherical expandable multi-chamber inflatable airbag. A plurality of inflation valves and a plurality of pressure relief valves are fixedly installed on the outer surface of the flexible spherical expandable multi-chamber inflatable airbag, and each independent cabin corresponds to an inflation valve and a pressure relief valve. Six flexible deployable radar reflectors are installed in the independent cabin, and a weighted water bag is arranged on the outer side of the flexible spherical expandable multi-chamber inflatable airbag, and the weighted water bag is connected to one of the D-type pull rings.

[0007] Furthermore, the flexible deployable radar reflector includes a radar reflective bottom plate and two radar reflective side plates, the radar reflective bottom plate is an isosceles triangle structure, the radar reflective side plates are triangular structures, the two radar reflective side plates are respectively located at two isosceles edge positions on one side surface of the radar reflective bottom plate, and the three adjacent surfaces of the radar reflective bottom plate and the two radar reflective side plates are reflective surfaces.

[0008] Furthermore, four of the six flexible deployable radar reflectors are located in the middle of the independent cabin, the four flexible deployable radar reflectors are distributed in an equidistant circular array, the other two flexible deployable radar reflectors are respectively located in the upper and lower parts of the independent cabin, the outer edges of the radar reflective bottom plates in the four flexible deployable radar reflectors are enclosed to form a square structure, the tops of the radar reflective side plates in the four flexible deployable radar reflectors are concentrated to the same place, the hypotenuses of two adjacent radar reflective side plates in the four flexible deployable radar reflectors are connected, and the four flexible deployable radars are arranged in a rectangular shape. One end of the radar reflection bottom plate on both sides of the reflector is fixedly connected to one side of the two flexible cabin isolation layers respectively, the top end of the upper radar reflection bottom plate among the four flexible deployable radar reflectors is connected to the upper radar reflection bottom plate of the independent cabin, the bottom end of the lower radar reflection bottom plate among the four flexible deployable radar reflectors is connected to one end of the lower radar reflection bottom plate of the independent cabin, the top end of the radar reflection side plate in the flexible deployable radar reflector in the upper part of the independent cabin is connected to the flexible cabin isolation layer, and the bottom end of the radar reflection side plate in the flexible deployable radar reflector in the lower part of the independent cabin is connected to the flexible cabin isolation layer.

[0009] Furthermore, four flexible cabin isolation layers are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag, and the four flexible cabin isolation layers are distributed in an equidistant circular array. Four independent cabins are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag.

[0010] Furthermore, the independent cabin is a quarter-spherical structure.

[0011] Furthermore, the flexible cabin isolation layer is a semicircular structure, and the straight sides of four flexible cabin isolation layers are connected to the same place.

[0012] Furthermore, the two reinforcement ropes are both annular structures, and the two reinforcement ropes are respectively arranged in the radial direction and the latitudinal direction of the outer surface of the flexible spherical expandable multi-chamber inflatable airbag.

[0013] Furthermore, the working steps of the spherical multi-chamber inflatable target are:

[0014] Step 1: fix six flexible deployable radar reflectors between two flexible cabin isolation layers, and fill air into the flexible spherical deployable multi-cabin inflatable airbag to a set pressure value through an inflation valve using a dedicated inflation device, so that the flexible spherical deployable multi-cabin inflatable airbag is rapidly deployed, and the flexible spherical deployable multi-cabin inflatable airbag is in a tensioned state, forming a spherical overall force system with a certain rigidity and the ability to withstand deadweight and external loads. As the flexible spherical deployable multi-cabin inflatable airbag is deployed, the flexible deployable radar reflectors installed in the independent cabins are deployed under the tensioning action of the flexible spherical deployable multi-cabin inflatable airbag;

[0015] Step 2: Fix the towing cable on one of the D-shaped pull rings, throw the target into the sea and drag it to the designated area to complete the target deployment. During maintenance, first deflate the flexible spherical expandable multi-chamber inflatable airbag through the pressure relief valve, and open the sealable operating port to maintain the inside of the flexible spherical expandable multi-chamber inflatable airbag.

[0016] Beneficial effects of the present invention:

[0017] The present invention adopts a four-independent cabin design, that is, when one part is hit or damaged, it will not affect the appearance and use of other independent cabins, so it can be deployed once and used multiple times. It is more convenient and efficient than traditional offshore floating targets. The twenty-four flexible and deployable radar reflectors arranged inside the target have a total of seventy-two reflecting surfaces, a small folding space, and can be deployed to achieve large space, which can ensure that radar signals can be reflected in any direction and angle, greatly improving shooting accuracy; the present invention adopts an inflatable airbag as a target, which can be folded and stored after exhaust, and can be quickly inflated and unfolded when used. When deployed, multiple can be carried for rapid and multi-directional deployment at sea, thereby improving the effectiveness of the mission and greatly increasing the service life of the target. It can also be reused multiple times through simple maintenance. BRIEF DESCRIPTION OF THE DRAWINGS

[0018] The present invention will be further described below in conjunction with the accompanying drawings.

[0019] Figure 1 It is a structural schematic diagram of a spherical expandable multi-chamber inflatable target of the present invention;

[0020] Figure 2 It is an assembly diagram of the flexible spherical deployable multi-chamber inflatable airbag and the flexible cabin isolation layer in the present invention;

[0021] Figure 3 It is a perspective view of a spherical expandable multi-chamber inflatable target of the present invention;

[0022] Figure 4 It is an assembly stereogram of the flexible cabin isolation layer and the flexible deployable radar reflector in the present invention;

[0023] Figure 5 It is a schematic diagram of the structure of the flexible deployable radar reflector in the present invention;

[0024] Figure 6 It is an assembly cross-sectional view of the flexible cabin isolation layer, the flexible deployable radar reflector, and the counterweight water bag in the present invention.

[0025] In the figure: 1. Flexible spherical deployable multi-chamber inflatable airbag; 101. Independent cabin; 2. Flexible cabin isolation layer; 3. Flexible deployable radar reflector; 31. Radar reflective bottom plate; 32. Radar reflective side plate; 4. Towing cable; 5. Inflating valve; 6. Sealable operating port; 7. D-type pull ring; 8. Counterweight water bag; 9. Reinforcement rope; 10. Pressure relief valve. DETAILED DESCRIPTION

[0026] The following will be combined with the drawings in the embodiments of the present invention to clearly and completely describe the technical solutions in the embodiments of the present invention. Obviously, the described embodiments are only part of the embodiments of the present invention, not all of the embodiments. Based on the embodiments of the present invention, all other embodiments obtained by ordinary technicians in this field without creative work are within the scope of protection of the present invention.

[0027] like Figure 1-6 As shown, a spherical deployable multi-chamber inflatable target comprises a flexible spherical deployable multi-chamber inflatable airbag 1, the outer surface of the flexible spherical deployable multi-chamber inflatable airbag 1 is provided with two reinforcing ropes 9, the flexible spherical deployable multi-chamber inflatable airbag 1 is provided with a sealable operating port 6, the sealable operating port 6 is opened and closed by a waterproof and airtight zipper, and a plurality of D-shaped pull rings 7 are fixedly installed on the outer surface of the flexible spherical deployable multi-chamber inflatable airbag 1, and a towing cable 4 is fixedly installed on one of the D-shaped pull rings 7;

[0028] A plurality of flexible cabin isolation layers 2 are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag 1, and an independent cabin 101 is enclosed between two adjacent flexible cabin isolation layers 2 and the flexible spherical expandable multi-chamber inflatable airbag 1. A plurality of inflation valves 5 and a plurality of pressure relief valves 10 are fixedly installed on the outer surface of the flexible spherical expandable multi-chamber inflatable airbag 1, and each independent cabin 101 corresponds to an inflation valve 5 and a pressure relief valve 10. Six flexible deployable radar reflectors 3 are installed in the independent cabin 101, and a weighted water bag 8 is arranged on the outer side of the flexible spherical expandable multi-chamber inflatable airbag 1, and the weighted water bag 8 is connected to one of the D-type pull rings 7.

[0029] The flexible deployable radar reflector 3 includes a radar reflection bottom plate 31 and two radar reflection side plates 32, wherein the radar reflection bottom plate 31 is an isosceles triangle structure, and the radar reflection side plates 32 are triangular structures. The two radar reflection side plates 32 are respectively located at two isosceles sides of a side surface of the radar reflection bottom plate 31, and the three adjacent surfaces of the radar reflection bottom plate 31 and the two radar reflection side plates 32 are reflection surfaces.

[0030] Four of the six flexible deployable radar reflectors 3 are located in the middle of the independent cabin 101, and the four flexible deployable radar reflectors 3 are distributed in an equidistant circular array. The other two flexible deployable radar reflectors 3 are respectively located at the upper and lower parts of the independent cabin 101. The outer edges of the radar reflective bottom plates 31 in the four flexible deployable radar reflectors 3 are enclosed to form a square structure. The tops of the radar reflective side panels 32 in the four flexible deployable radar reflectors 3 are concentrated at the same place. The hypotenuses of two adjacent radar reflective side panels 32 in the four flexible deployable radar reflectors 3 are connected. The radar reflective panels 32 on both sides of the four flexible deployable radar reflectors 3 are connected to the same place. One end of the radar reflection bottom plate 31 is fixedly connected to one side of the two flexible cabin isolation layers 2 respectively, the top end of the upper radar reflection bottom plate 31 among the four flexible deployable radar reflectors 3 is connected to one end of the upper radar reflection bottom plate 31 of the independent cabin 101, the bottom end of the lower radar reflection bottom plate 31 among the four flexible deployable radar reflectors 3 is connected to one end of the lower radar reflection bottom plate 31 of the independent cabin 101, the top end of the radar reflection side panel 32 in the flexible deployable radar reflector 3 at the upper part of the independent cabin 101 is connected to the flexible cabin isolation layer 2, and the bottom end of the radar reflection side panel 32 in the flexible deployable radar reflector 3 at the lower part of the independent cabin 101 is connected to the flexible cabin isolation layer 2.

[0031] Four flexible cabin isolation layers 2 are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag 1. The four flexible cabin isolation layers 2 are distributed in an equidistant circular array. Four independent cabins 101 are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag 1.

[0032] The independent chamber 101 is a quarter spherical structure.

[0033] The flexible cabin isolation layer 2 is a semicircular structure, and the flexible cabin isolation layer 2 is made of PVC mesh cloth material. The straight edges of four flexible cabin isolation layers 2 are connected to the same place.

[0034] The two reinforcing ropes 9 are both annular structures, and the two reinforcing ropes 9 are respectively arranged in the radial direction and the latitudinal direction of the outer surface of the flexible spherical deployable multi-chamber inflatable airbag 1.

[0035] The working steps of the spherical multi-chamber inflatable target are:

[0036] Step 1, fix six flexible deployable radar reflectors 3 between two flexible cabin isolation layers 2, and fill air into the flexible spherical deployable multi-cabin inflatable airbag 1 through the inflation valve 5 to a set air pressure value by means of a dedicated inflation device, so that the flexible spherical deployable multi-cabin inflatable airbag 1 is rapidly deployed, and the flexible spherical deployable multi-cabin inflatable airbag 1 is in a tensioned state, forming a spherical overall force system with a certain rigidity and the ability to withstand deadweight and external loads. As the flexible spherical deployable multi-cabin inflatable airbag 1 is deployed, the flexible deployable radar reflector 3 installed in the independent cabin 101 is deployed under the tension of the flexible spherical deployable multi-cabin inflatable airbag 1;

[0037] Step 2: Fix the towing cable 4 on one of the D-shaped pull rings 7, throw the target into the sea and drag it to the designated area to complete the target deployment. During maintenance, first deflate the flexible spherical expandable multi-chamber inflatable airbag 1 through the pressure relief valve 10, and open the sealable operating port 6 to maintain the interior of the flexible spherical expandable multi-chamber inflatable airbag 1.

[0038] Working principle of the present invention:

[0039] The flexible spherical deployable multi-chamber inflatable airbag 1 of the spherical multi-chamber inflatable target is divided into four independent chambers 101 by a flexible chamber isolation layer 2. Six flexible deployable radar reflectors 3 are arranged in each independent chamber 101, that is, twenty-four flexible deployable radar reflectors 3 are evenly arranged in the entire target. Each reflector has three reflecting surfaces, that is, the reflectors have a total of seventy-two reflecting surfaces, which can reflect radar waves in all directions for rapid capture and recovery. The outer side of the spherical airbag is respectively radially and latitudely arranged. Two circles of reinforcing ropes 9 are arranged to prevent the target from being deformed or damaged when the ship is towed at high speed. Several D-type pull rings 7 are also arranged on the flexible spherical expandable multi-chamber inflatable airbag 1, which serve as limiters for the reinforcing rope 9 and mooring devices for the towing cable 4. Each cabin of the inflatable airbag is provided with an inflation valve 5 and a pressure relief valve 10, and a sealable operating port 6 is provided for easy maintenance. Air is flushed into the target body to the set air pressure value through the dedicated floating target inflation equipment, and the target can be thrown and laid.

[0040] The present invention adopts a four-independent cabin 101 design, that is, when one part is hit or damaged, it will not affect the appearance and use of other independent cabins, so it can be deployed once and used multiple times. It is more convenient and efficient than traditional offshore floating targets. The twenty-four flexible and deployable radar reflectors arranged inside the target have a total of seventy-two reflecting surfaces, a small folding space, and can be deployed to achieve large space, which can ensure that radar signals can be reflected in any direction and angle, greatly improving the shooting accuracy; the present invention adopts an inflatable airbag as a target, which can be folded and stored after exhaust, and can be quickly inflated and unfolded when used. When deployed, multiple can be carried for rapid multi-directional deployment at sea, thereby improving the effectiveness of the mission and greatly increasing the service life of the target. It can also be reused multiple times through simple maintenance.

[0041] The above description is only a preferred embodiment of the present invention and does not limit the present invention in any form. Although the present invention has been disclosed as a preferred embodiment as above, it is not used to limit the present invention. Any technician familiar with this profession can make some changes or modify the technical contents disclosed above into equivalent embodiments without departing from the scope of the technical solution of the present invention. However, any simple modification, equivalent change and modification made to the above embodiments according to the technical essence of the present invention without departing from the content of the technical solution of the present invention still fall within the scope of the technical solution of the present invention.

Claims

1. A spherical expandable multi-chamber inflatable target, characterized in that: The invention comprises a flexible spherical expandable multi-chamber inflatable airbag (1), wherein the outer surface of the flexible spherical expandable multi-chamber inflatable airbag (1) is provided with two reinforcing ropes (9), the flexible spherical expandable multi-chamber inflatable airbag (1) is provided with a sealable operating port (6), and a plurality of D-shaped pull rings (7) are fixedly mounted on the outer surface of the flexible spherical expandable multi-chamber inflatable airbag (1), wherein a towing cable (4) is fixedly mounted on one of the D-shaped pull rings (7); A plurality of flexible cabin isolation layers (2) are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag (1), and an independent cabin (101) is enclosed between two adjacent flexible cabin isolation layers (2) and the flexible spherical expandable multi-chamber inflatable airbag (1). A plurality of inflation valves (5) and a plurality of pressure relief valves (10) are fixedly installed on the outer surface of the flexible spherical expandable multi-chamber inflatable airbag (1), and each independent cabin (101) corresponds to an inflation valve (5) and a pressure relief valve (10). Six flexible deployable radar reflectors (3) are installed in the independent cabin (101). A weighted water bag (8) is arranged on the outer side of the flexible spherical expandable multi-chamber inflatable airbag (1), and the weighted water bag (8) is connected to one of the D-shaped pull rings (7); Four of the six flexible deployable radar reflectors (3) are located in the middle of the independent cabin (101), the four flexible deployable radar reflectors (3) are distributed in an equidistant circular array, the other two flexible deployable radar reflectors (3) are respectively located at the upper and lower parts of the independent cabin (101), the outer edges of the radar reflective bottom plates (31) in the four flexible deployable radar reflectors (3) are enclosed to form a square structure, the tops of the radar reflective side plates (32) in the four flexible deployable radar reflectors (3) are concentrated at the same place, the oblique edges of two adjacent radar reflective side plates (32) in the four flexible deployable radar reflectors (3) are connected, and the radar reflective bottom plates (31) on both sides of the four flexible deployable radar reflectors (3) are connected. 1) are respectively fixedly connected to one side of two flexible cabin insulation layers (2), the top end of the radar reflection bottom plate (31) at the top of the four flexible deployable radar reflectors (3) is connected to one end of the radar reflection bottom plate (31) at the top of the independent cabin (101), the bottom end of the radar reflection bottom plate (31) at the bottom of the four flexible deployable radar reflectors (3) is connected to one end of the radar reflection bottom plate (31) at the bottom of the independent cabin (101), the top end of the radar reflection side plate (32) in the flexible deployable radar reflector (3) at the top of the independent cabin (101) is connected to the flexible cabin insulation layer (2), and the bottom end of the radar reflection side plate (32) in the flexible deployable radar reflector (3) at the bottom of the independent cabin (101) is connected to the flexible cabin insulation layer (2); The independent chamber (101) is a quarter-spherical structure.

2. A spherical expandable multi-chamber inflatable target according to claim 1, characterized in that: The flexible deployable radar reflector (3) comprises a radar reflection bottom plate (31) and two radar reflection side plates (32); the radar reflection bottom plate (31) is an isosceles triangle structure; the radar reflection side plates (32) are triangular structures; the two radar reflection side plates (32) are respectively located at two isosceles sides of a side surface of the radar reflection bottom plate (31); and three adjacent surfaces of the radar reflection bottom plate (31) and the two radar reflection side plates (32) are reflection surfaces.

3. A spherical expandable multi-chamber inflatable target according to claim 1, characterized in that: Four flexible cabin isolation layers (2) are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag (1), and the four flexible cabin isolation layers (2) are distributed in a circular array at equal intervals. Four independent cabins (101) are arranged on the inner side of the flexible spherical expandable multi-chamber inflatable airbag (1).

4. The spherical expandable multi-chamber inflatable target according to claim 1, characterized in that: The flexible cabin insulation layer (2) is a semicircular structure, and the straight edges of four flexible cabin insulation layers (2) are connected to the same point.

5. The spherical expandable multi-chamber inflatable target according to claim 1, characterized in that: The two reinforcing ropes (9) are both annular structures, and the two reinforcing ropes (9) are respectively arranged in the radial direction and the latitudinal direction of the outer surface of the flexible spherical expandable multi-chamber inflatable airbag (1).

6. The spherical expandable multi-chamber inflatable target according to claim 1, characterized in that: The working steps of the spherical multi-chamber inflatable target are: Step 1: fix six flexible deployable radar reflectors (3) between two flexible cabin isolation layers (2), and use a dedicated inflation device to inflate air into the flexible spherical deployable multi-cabin inflatable airbag (1) through an inflation valve (5) to a set air pressure value, so that the flexible spherical deployable multi-cabin inflatable airbag (1) is rapidly deployed, and the flexible spherical deployable multi-cabin inflatable airbag (1) is in a tensioned state. As the flexible spherical deployable multi-cabin inflatable airbag (1) is deployed, the flexible deployable radar reflectors (3) installed in the independent cabins (101) are deployed under the tension of the flexible spherical deployable multi-cabin inflatable airbag (1); Step 2: Fix the towing cable (4) to one of the D-shaped pull rings (7), throw the target into the sea and tow it to the designated area to complete the target deployment. During maintenance, first deflate the flexible spherical deployable multi-chamber inflatable airbag (1) through the pressure relief valve (10), and open the sealable operating port (6) to perform maintenance on the inside of the flexible spherical deployable multi-chamber inflatable airbag (1).

Citation Information

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