CN206582453U - A kind of unidirectional three-way connection of aircraft oxygen system - Google Patents

A kind of unidirectional three-way connection of aircraft oxygen system Download PDF

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Publication number
CN206582453U
CN206582453U CN201720199975.0U CN201720199975U CN206582453U CN 206582453 U CN206582453 U CN 206582453U CN 201720199975 U CN201720199975 U CN 201720199975U CN 206582453 U CN206582453 U CN 206582453U
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China
Prior art keywords
check valve
valve component
unidirectional
housing
oxygen
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Active
Application number
CN201720199975.0U
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Chinese (zh)
Inventor
谢磊
刘祚祺
白晓东
崔超
郑旭莹
刘益民
郭侨
王晓琪
何凯
常晓静
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Shaanxi Aircraft Industry Co Ltd
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AVIC Shaanxi Aircraft Industry Group Corp Ltd
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Priority to CN201720199975.0U priority Critical patent/CN206582453U/en
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Abstract

The utility model belongs to aircraft oxygen-supplying technology, is related to a kind of unidirectional three-way connection of aircraft oxygen system oxygen cylinder.It is characterized in that:It is made up of housing (1), branch pipe (2), the 1st filter screen (3), the 1st check valve component (4), the 2nd filter screen (5) and the 2nd check valve component (6).The utility model provides a kind of unidirectional three-way connection of aircraft oxygen system, to meet the development needs of certain domestic type transporter carbon fibre composite high-pressure oxygen cylinder.

Description

A kind of unidirectional three-way connection of aircraft oxygen system
Technical field
The utility model belongs to aircraft oxygen-supplying technology, is related to a kind of aircraft oxygen system oxygen cylinder and is connected with unidirectional three Head.
Background technology
The carbon fibre composite high-pressure oxygen cylinder that certain domestic type transporter is newly developed is, it is necessary to a kind of aircraft oxygen of supporting installation The special three-way connection of gas system carbon fiber oxygen cylinder.Because oxygen belongs to the explosive combustion-supporting gas of high energy, therefore oxygen in itself All strictly it must be controlled to flow to from oxygen dispenser to oxygen source, from oxygen source to oxygen terminal.When aircrew normally uses oxygen, It is in the same direction and irreversible to meet the oxygen flowed out from multiple high-pressure oxygen cylinders;When needing to be oxygenated to high-pressure oxygen cylinder, oxygen is met Gas is unidirectional and air tight during multiple oxygen cylinders are entered.Do not retrieve on carbon fiber oxygen cylinder special three-way joint Open source literature.
The content of the invention
The purpose of this utility model is:A kind of unidirectional three-way connection of aircraft oxygen system is provided, so as to meet it is domestic certain The development of type transporter carbon fibre composite high-pressure oxygen cylinder needs.
The technical solution of the utility model is:A kind of unidirectional three-way connection of aircraft oxygen system, it is characterised in that:It by Housing 1, branch pipe 2, the 1st filter screen 3, the 1st check valve component 4, the 2nd filter screen 5 and the 2nd check valve component 6 are constituted;In housing (1) there is the arrow of a horizontal direction outside, there is a horizontal hole and a upright opening, the inner of upright opening in housing 1 Mouth connection orthogonal with the middle part of horizontal hole, has internal thread in the left port of horizontal hole and the lower port of upright opening, The right-hand member of horizontal hole has external screw thread, has external screw thread outside the lower port of upright opening, unidirectional living with the female 1st Door component 4 is combined with the external screw thread of horizontal hole right-hand member, the right-hand member of the 1st check valve component 4 and housing 1 is connected as whole Body;Combined with externally threaded 2nd check valve component 6 with the internal thread of horizontal hole left end, by the 2nd check valve component 6 are connected as entirety with the left end of housing 1;1st filter screen 3 is arranged in the runner of the 1st check valve component 4, and the 2nd filter screen 5 is installed In the runner of the 2nd check valve component 6;Branch pipe 2 is that a upper end carries externally threaded pipe, the external screw thread of the upper end of branch pipe 2 In the internal thread for being screwed into upright opening lower port.
The beneficial effects of the utility model are:A kind of unidirectional three-way connection of aircraft oxygen system is provided, to meet state The development of certain interior type transporter carbon fibre composite high-pressure oxygen cylinder needs.
Brief description of the drawings
Fig. 1 is structural representation of the present utility model.
Embodiment
The utility model is described in further detail below.Referring to Fig. 1, a kind of aircraft oxygen system is connected with unidirectional three Head, it is characterised in that:It is by housing 1, branch pipe 2, the 1st filter screen 3, the 1st check valve component 4, the 2nd filter screen 5 and the 2nd check valve Component 6 is constituted;Have the arrow of a horizontal direction outside the housing (1), have in housing 1 horizontal hole and one it is vertical Hole, the inner port of upright opening connection orthogonal with the middle part of horizontal hole, under the left port and upright opening of horizontal hole There is internal thread port, has external screw thread in the right-hand member of horizontal hole, has external screw thread outside the lower port of upright opening, with interior 1st check valve component 4 of screw thread is combined with the external screw thread of horizontal hole right-hand member, by the 1st check valve component 4 and housing 1 Right-hand member be connected as entirety;Combined with externally threaded 2nd check valve component 6 with the internal thread of horizontal hole left end, will The left end of 2nd check valve component 6 and housing 1 is connected as entirety;1st filter screen 3 is arranged on the runner of the 1st check valve component 4 Interior, the 2nd filter screen 5 is arranged in the runner of the 2nd check valve component 6;Branch pipe 2 is that a upper end carries externally threaded pipe, branch The external screw thread of the upper end of pipe 2 is screwed into the internal thread of upright opening lower port.
In order to accelerate the speed that oxygen flows into oxygen cylinder, the horn mouth expanded outwardly is carried in the lower end of described branch pipe 2. In order to increase the circulation area between branch pipe 2 and oxygen cylinder inner chamber and prevent the problems such as single face is blocked, in described branch pipe 2 There is radial hole on tube wall.
Operation principle of the present utility model is:A kind of unidirectional three-way connection of aircraft oxygen system, it is characterised in that:It by Housing 1, branch pipe 2, the 1st filter screen 3, the 1st check valve component 4, the 2nd filter screen 5 and the 2nd check valve component 6 are constituted.Unidirectional threeway After joint is completed, the 1st check valve component 4 is connected with oxygen air induction conduit according to direction shown in the outer arrow of housing 1, will 2nd check valve component 6 is connected with oxygen exhaust manifolds, and the external screw thread of the upright opening lower port of housing 1 is connected with oxygen cylinder.When After source of the gas enters the 1st check valve component 4 through air induction conduit, the spring inside the 1st check valve component 4 occurs for bleed pressure Elastic deformation, valve is opened, and oxygen is flowed in oxygen cylinder or through the flow direction oxygen terminal of the 2nd check valve component 6 or next oxygen Gas cylinder, this is aerobic process;When occupant is opened with oxygen terminal on machine, source of the gas flows to the 2nd check valve component 6 by branch pipe 2, Bleed pressure makes the spring inside the 2nd check valve component 6 occur elastic deformation, and valve is opened, and oxygen flow direction uses oxygen terminal, this For oxygen supply process.

Claims (3)

1. a kind of unidirectional three-way connection of aircraft oxygen system, it is characterised in that:It is by housing (1), branch pipe (2), the 1st filter screen (3), the 1st check valve component (4), the 2nd filter screen (5) and the 2nd check valve component (6) composition;There is a water outside housing (1) Square to arrow, have a horizontal hole and a upright opening, the inner port of upright opening and horizontal insertion in the housing (1) The orthogonal connection in the middle part in hole, has internal thread, in horizontal hole in the left port of horizontal hole and the lower port of upright opening Right-hand member has external screw thread, has external screw thread outside the lower port of upright opening, with female 1st check valve component (4) with The external screw thread of horizontal hole right-hand member is combined, and the right-hand member of the 1st check valve component (4) and housing (1) is connected as into entirety;Carry Externally threaded 2nd check valve component (6) is combined with the internal thread of horizontal hole left end, by the 2nd check valve component (6) with The left end of housing (1) is connected as entirety;1st filter screen (3) is arranged in the runner of the 1st check valve component (4), the 2nd filter screen (5) In the runner of the 2nd check valve component (6);Branch pipe (2) is that a upper end is carried on externally threaded pipe, branch pipe (2) The external screw thread at end is screwed into the internal thread of upright opening lower port.
2. the unidirectional three-way connection of aircraft oxygen system according to claim 1, it is characterised in that:In described branch pipe (2) lower end carries the horn mouth expanded outwardly.
3. the unidirectional three-way connection of aircraft oxygen system according to claim 1 or 2, it is characterised in that:In described branch There is radial hole on the tube wall for managing (2).
CN201720199975.0U 2017-03-02 2017-03-02 A kind of unidirectional three-way connection of aircraft oxygen system Active CN206582453U (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201720199975.0U CN206582453U (en) 2017-03-02 2017-03-02 A kind of unidirectional three-way connection of aircraft oxygen system

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201720199975.0U CN206582453U (en) 2017-03-02 2017-03-02 A kind of unidirectional three-way connection of aircraft oxygen system

Publications (1)

Publication Number Publication Date
CN206582453U true CN206582453U (en) 2017-10-24

Family

ID=60112083

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201720199975.0U Active CN206582453U (en) 2017-03-02 2017-03-02 A kind of unidirectional three-way connection of aircraft oxygen system

Country Status (1)

Country Link
CN (1) CN206582453U (en)

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GR01 Patent grant
GR01 Patent grant
CP03 Change of name, title or address

Address after: 723213 Liulin Town, Chenggu County, Hanzhong City, Shaanxi Province

Patentee after: Shaanxi Aircraft Industry Co.,Ltd.

Address before: 723213 box 34, Hanzhoung, Shaanxi

Patentee before: Shaanxi Aircraft INDUSTRY(GROUP) Co.,Ltd.

CP03 Change of name, title or address