CN212738516U

CN212738516U - Aircraft passenger isolation cabin

Info

Publication number: CN212738516U
Application number: CN202021747204.9U
Authority: CN
Inventors: 王学东
Original assignee: Individual
Current assignee: Individual
Priority date: 2020-08-19
Filing date: 2020-08-19
Publication date: 2021-03-19
Anticipated expiration: 2030-08-19

Abstract

The utility model discloses an aircraft passenger isolation cabin. The aircraft comprises an aircraft cabin, wherein one or more isolation cabin areas are arranged in the aircraft cabin, one or more sealed isolation cabins are arranged in the isolation cabin areas, a sealing door is arranged in each isolation cabin, the isolation cabins are isolated through an isolation plate, and the isolation plates extend from the floor of the local layer of the aircraft to the ceiling of the local layer of the aircraft. The utility model is used for the aircraft passenger keeps apart, prevents because of the bacterium cross infection that the circulation of air caused.

Description

Aircraft passenger isolation cabin

Technical Field

The utility model belongs to the technical field of aircraft equipment, concretely relates to aircraft passenger isolation cabin.

Background

The passengers in the common cabin of the existing aircraft cabin are not isolated from the isolation area, and the mutual air circulation is easy to cause bacterial cross infection, so that the design of a new aircraft passenger isolation cabin is very necessary.

SUMMERY OF THE UTILITY MODEL

The utility model aims at providing an aircraft passenger isolation cabin in order to solve the deficiencies of the prior art.

The utility model adopts the technical proposal that: the utility model provides an aircraft passenger isolation cabin, includes the cabin, be equipped with one or more isolation cabin regions in the cabin, be equipped with one or more sealed isolation cabin in the isolation cabin region, the sealed door is seted up to the isolation cabin, the isolation cabin passes through the division board and keeps apart, the division board extends to this layer of ceiling of aircraft from this layer of floor of aircraft.

In a further preferable structure, an air supply outlet and an air suction opening are arranged inside each isolation cabin, and the air supply outlet is connected with an air supply system through an air supply pipeline; the air suction opening is connected with an air suction system through an air suction pipeline; the air supply system is not communicated with the air exhaust system.

In a further preferred structure, an isolation cabin seat is arranged in the isolation cabin.

In a further preferred construction, the sealing door is embedded in a front partition plate facing the cabin seat.

The utility model is used for the aircraft passenger keeps apart, prevents because of the bacterium cross infection that the circulation of air caused.

Drawings

Fig. 1 is a schematic plan view of the present invention;

FIG. 2 is a plan view of the pod;

FIG. 3 is an elevational view of the front bulkhead and the sealing door;

FIG. 4 is an elevational view of the front spacer;

FIG. 5 is an elevational view of the rear spacer;

fig. 6 is the utility model discloses connect air supply system and exhaust system structure sketch map.

Wherein, 1-cab, 2-common cabin, 3-isolation cabin area, 4-isolation board (4-1-front isolation board, 4-2-rear isolation board), 5-sealing door, 6-channel, 7-isolation cabin seat, 8-aircraft floor, 9-aircraft floor, 10-air supply pipeline, 11-air supply outlet, 12-air extraction pipeline and 13-air extraction outlet.

Detailed Description

The invention will be further described in detail with reference to the drawings and the following detailed description, which are provided for the purpose of clearly understanding the invention and are not intended to limit the invention.

As shown in fig. 1-5, the utility model discloses a cabin establishes driver's cabin 1 and ordinary cabin 2 in, be equipped with one or more isolation cabin region 3 in the cabin, be equipped with a plurality of sealed isolation cabins in the isolation cabin region 3, sealing door 5 is seted up to the isolation cabin, the isolation cabin passes through division board 4 and keeps apart, division board 4 extends to this layer of ceiling 8 of aircraft from this layer of floor 9 of aircraft.

An air supply outlet 11 and an air suction opening 13 are arranged inside each isolation cabin, and the air supply outlet 11 is connected with an air supply system through an air supply pipeline 10; the air suction opening 13 is connected with an air suction system through an air suction pipeline 12; the air supply system is not communicated with the air exhaust system.

An isolation cabin seat 7 is arranged in the isolation cabin.

The sealing door 5 is embedded in the front partition plate 4-1 facing the cabin seat 7.

As shown in fig. 1, in an embodiment of the present invention, A, B, C, D, E, F six isolation cabins (shown in fig. 6), six air supply ports and six air suction ports are provided, and the air supply system and the air suction system are completely independent, so as to ensure that the passengers in each isolation cabin breathe fresh air supplied from the air supply system, and no cross infection due to air circulation occurs.

The isolation plate 4 is made of aluminum alloy plates, is isolated from the floor to the ceiling of the floor, and is sealed by sealant at the periphery. The sealing door is made of transparent organic glass, and rubber sealing rings are arranged around the sealing door.

The utility model discloses set up one or several regions on the aircraft, cancel original cabin position for establish one or several isolation cabin regions, in this region, construct a plurality of isolation cabins. Each isolation cabin is sealed by sealing materials, only goes in and out through a sealing door, the isolation materials are from the floor of the airplane to the ceiling of the airplane, when the sealing door is closed, the isolation cabin is not communicated with the outside, and an air supply opening and an air suction opening are arranged in the isolation cabin to keep fresh air fed and waste gas pumped away. The air supply system and the air suction system are completely independent and do not mix air. No air circulation exists between the inside of the isolation cabin seat and the public walkway (the channel 6) and other isolation cabin seats, air is only supplied in through the air supply system, and air is exhausted through the air exhaust system.

Those not described in detail in this specification are within the skill of the art.

Claims

1. An aircraft passenger isolation capsule comprising a cabin, characterized in that: the aircraft is characterized in that one or more isolation cabin areas are arranged in the cabin, one or more sealed isolation cabins are arranged in the isolation cabin areas, the isolation cabins are provided with sealing doors and are isolated by isolation plates, and the isolation plates extend from the floor of the local layer of the aircraft to the ceiling of the local layer of the aircraft.

2. An aircraft passenger isolation capsule as claimed in claim 1, wherein: an air supply outlet and an air suction opening are arranged in each isolation cabin, and the air supply outlet is connected with an air supply system through an air supply pipeline; the air suction opening is connected with an air suction system through an air suction pipeline; the air supply system is not communicated with the air exhaust system.

3. An aircraft passenger isolation capsule according to claim 1 or 2, wherein: and an isolation cabin seat is arranged in the isolation cabin.

4. An aircraft passenger isolation capsule according to claim 3, wherein: the sealing door is embedded in a front partition plate facing the cabin seat.