CN109533347B - Automatic connection type quick-release connector - Google Patents
Automatic connection type quick-release connector Download PDFInfo
- Publication number
- CN109533347B CN109533347B CN201811322616.5A CN201811322616A CN109533347B CN 109533347 B CN109533347 B CN 109533347B CN 201811322616 A CN201811322616 A CN 201811322616A CN 109533347 B CN109533347 B CN 109533347B
- Authority
- CN
- China
- Prior art keywords
- support
- sealing ring
- cover plate
- holes
- semicircular
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Active
Links
- 238000007789 sealing Methods 0.000 claims abstract description 34
- 230000008878 coupling Effects 0.000 claims description 13
- 238000010168 coupling process Methods 0.000 claims description 13
- 238000005859 coupling reaction Methods 0.000 claims description 13
- 238000012423 maintenance Methods 0.000 abstract description 5
- 230000005540 biological transmission Effects 0.000 abstract description 4
- 238000007667 floating Methods 0.000 abstract description 2
- 210000001503 joint Anatomy 0.000 description 6
- 239000002737 fuel gas Substances 0.000 description 3
- 230000009286 beneficial effect Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 239000007789 gas Substances 0.000 description 1
- 238000009434 installation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
Images
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D25/00—Emergency apparatus or devices, not otherwise provided for
- B64D25/08—Ejecting or escaping means
- B64D25/10—Ejector seats
Landscapes
- Business, Economics & Management (AREA)
- Emergency Management (AREA)
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Quick-Acting Or Multi-Walled Pipe Joints (AREA)
Abstract
The invention belongs to the technical field of protection and lifesaving, and relates to an automatic connection type quick-release connector. The device comprises a support assembly (2), an upper joint (3), a top sealing ring (4), a bottom sealing ring (5) and a lower joint (6); the top sealing ring (4) and the bottom sealing ring (5) are respectively arranged in a sealing ring groove of the upper joint (3), the upper joint (3) is fixedly arranged on the ejection seat, and the 2 lower joints (6) are arranged on the ejection cylinder supporting arm (1) through the support assembly (2). The invention adopts a floating connection structure form to realize gas transmission. The automatic connection type quick-release connector has the advantages of simple structure, convenience in use and maintenance and the like, is suitable for an active ejection life-saving device, and has wider application prospect.
Description
The technical field is as follows:
the invention belongs to the technical field of protection and lifesaving, and relates to an automatic connection type quick-release connector.
Background art:
the quick-release connector is used for connecting the ejection seat with the instruction ejection system, and fuel gas transmission between the ejection seat and the instruction ejection system is realized. When the seat is detached and ejected, the quick-release connector can be automatically disconnected, so that the ejection seat and the cabin are separated.
At present, the upper joint of the domestic quick-release joint is arranged on a seat, and the lower joint is arranged in a cabin. The seat hangs into the passenger cabin, when keeping a certain distance from the floor of the passenger cabin, is not convenient for install by the ground service personnel manual with lower clutch and top connection butt joint. Particularly, for the ejection seat adopting the seat back rocket as the secondary power, the installation space of the quick release connector is limited by the seat back rocket, and the quick release connector is more difficult to install.
When the quick release connector is maintained regularly, the upper connector needs to be detached from the seat, and the quick release connector still needs to be installed on the seat after the regular maintenance is finished, so that the maintenance operation is more.
With the continuous improvement of the performance of fighters in all countries at present, users put higher demands on the operability and maintainability of the seats. When the seat is hung into the cabin, the automatic connection type quick-release connector can realize automatic butt joint of an upper connector on the seat and a lower connector of the command ejection system. And during regular maintenance, the upper joint and the lower joint do not need to be detached, so that the maintainability is greatly improved.
The technical scheme is as follows:
the purpose of the invention is as follows: a quick-release connector for automatically connecting an ejection seat with a command ejection system is provided.
The technical scheme of the invention is as follows: an automatic connection type quick-release connector is characterized by comprising a support assembly 2, an upper connector 3, a top sealing ring 4, a bottom sealing ring 5 and a lower connector 6; the top sealing ring 4 and the bottom sealing ring 5 are respectively arranged in a sealing ring groove of the upper joint 3, the upper joint 3 is fixedly arranged on the ejection seat, and the 2 lower joints 6 are arranged on the ejection cylinder support arm 1 through the support component 2.
The support assembly 2 comprises a support 7, a cover plate 8 and a fastener 9; the longitudinal section of the support 7 is of an L-shaped structure, 2 semicircular holes with the same diameter are arranged on one side below the support, mounting holes are distributed around the 2 semicircular holes, 2 square holes are arranged on one side above the support, and mounting holes are distributed above the square holes; the cover plate 8 is of a cuboid structure, wherein one side of the cover plate is provided with 2 semicircular holes with the same diameter, and the other side of the cover plate is distributed with mounting holes corresponding to the mounting holes distributed around the 2 semicircular holes on the support 7; one side of the support 7 with the semicircular hole is attached to one side of the cover plate 8 with the semicircular hole and then fixed by a fastening piece 9.
The lower joint 6 is an L-shaped joint, both ends of the joint are respectively provided with a 60-degree chamfer, one longer end of the joint is provided with an annular groove, the annular groove of the lower joint 6 is arranged in semicircular holes of the support 7 and the cover plate 8, and the lower joint is fixedly arranged on the support component 2.
The two lower joints 6 have different lengths at the longer ends.
The annular groove of lower clutch 6 is installed in the support 7 of support subassembly 2 and the semicircle orifice of apron 8, and the annular groove diameter of lower clutch 6 is less than the semicircle orifice diameter of support 7 and apron 8, and the height of annular groove is greater than the semicircle orifice height of support 7 and apron 8.
The invention has the beneficial effects that: the automatic connection type quick-release connector adopts a floating connection structure form to realize gas transmission. The automatic connection type quick-release connector has the advantages of simple structure, convenience in use and maintenance and the like, is suitable for an active ejection life-saving device, and has wider application prospect.
Description of the drawings:
FIG. 1 is a schematic structural view of the present invention;
wherein, 1-ejection cylinder support arm, 2-support component, 3-upper joint, 4-top sealing ring, 5-bottom sealing ring, and 6-lower joint.
FIG. 2 is a schematic structural view of the seat assembly of the present invention;
wherein, 7-support, 8-cover plate and 9-fastener.
FIG. 3 is a schematic view of the construction of the lower joint of the present invention;
Detailed Description
The present invention will be described in further detail below by way of specific embodiments:
referring to fig. 1, an automatic connection type quick release coupling comprises a support assembly 2, an upper coupling 3, a top seal ring 4, a bottom seal ring 5 and a lower coupling 6; the top sealing ring 4 and the bottom sealing ring 5 are respectively arranged in a sealing ring groove of the upper joint 3, the upper joint 3 is fixedly arranged on the ejection seat, and the lower joint 6 is arranged on the ejection cylinder support arm 1 through the support component 2.
When the seat is hung into the cabin, the 60-degree chamfer angle at the nozzle of the upper joint 3 and the lower joint 6 is contacted, the lower joint 6 is provided with lateral guiding force along with the downward placement of the seat, and the lower joint 6 moves horizontally along the radial direction in the support assembly 2, so that the automatic butt joint of the upper joint 3 and the lower joint 6 is realized.
Referring to fig. 2, the seat assembly 2 includes a seat 7, a cover plate 8 and a fastener 9; the longitudinal section of the support 7 is of an L-shaped structure, 2 semicircular holes with the same diameter are arranged on one side below the support, mounting holes are distributed around the 2 semicircular holes, 2 square holes are arranged on one side above the support, and mounting holes are distributed above the square holes; the cover plate 8 is of a cuboid structure, wherein one side of the cover plate is provided with 2 semicircular holes with the same diameter, and the other side of the cover plate is distributed with mounting holes corresponding to the mounting holes distributed around the 2 semicircular holes on the support 7; one side of the support 7 with the semicircular hole is attached to one side of the cover plate 8 with the semicircular hole and then fixed by a fastening piece 9. The lower joint 6 can flexibly move on the support assembly 2, so that the space is saved, and the weight is reduced.
Referring to fig. 3, the lower joint 6 is an L-shaped joint, two ends of the joint are respectively provided with a chamfer of 60 degrees, one longer end of the joint is provided with an annular groove, and the annular groove of the lower joint 6 is arranged in semicircular holes of the support 7 and the cover plate 8 and is fixedly arranged on the support component 2.
The two lower joints 6 have different lengths at the longer ends. The distance between the semicircular holes of the support 7 and the cover plate 8 can be minimized, the space is saved, and the weight is reduced.
The ring channel of lower clutch 6 is installed in the semicircle orifice of support 7 and apron 8 of support subassembly 2, and the ring channel diameter of lower clutch 6 is less than the semicircle orifice diameter of support 7 and apron 8, and the height that highly is greater than support 7 and the semicircle orifice height of apron 8 of ring channel guarantees that lower clutch 6 has certain clearance in support subassembly 2, can float along axial and radial on support subassembly 2.
When the seat is transferred, the bottom sealing ring 5 is in contact with the chamfer angle of the lower joint 6, and the sealing principle of the sealing ring is that the sealing ring is extruded by an inner cavity of the lower joint 6, so that the sealing ring is elastically deformed, and contact pressure is generated on a sealing contact surface, thereby realizing sealing. Therefore, in order to avoid the failure of the bottom sealing ring 5 caused by the chamfer matching problem with the lower joint 6 in the lowering process, the top sealing ring 4 is added. Therefore, the upper joint 3 adopts a double-sealing ring structure, the bottom sealing ring 5 plays a role in protection, the seat is prevented from being quickly hung into the cabin to influence the sealing performance, and the top sealing ring 4 plays a main sealing role.
When the ejection seat starts ejection, the generated fuel gas is transmitted through the fuel gas transmission channels of the upper connector 3 and the lower connector 6.
Claims (4)
1. An automatic connection type quick-release connector is characterized by comprising a support assembly (2), an upper connector (3), a top sealing ring (4), a bottom sealing ring (5) and a lower connector (6); a top sealing ring (4) and a bottom sealing ring (5) are respectively arranged in a sealing ring groove of an upper joint (3), the upper joint (3) is fixedly arranged on an ejection seat, and two lower joints (6) are arranged on an ejection cylinder support arm (1) through a support assembly (2);
the support assembly (2) comprises a support (7), a cover plate (8) and a fastener (9); the longitudinal section of the support (7) is of an L-shaped structure, two semicircular holes with the same diameter are arranged on one side below the support, mounting holes are distributed around the two semicircular holes, two square holes are arranged on one side above the support, and mounting holes are distributed above the square holes; the cover plate (8) is of a cuboid structure, wherein one side of the cover plate is provided with two semicircular holes with the same diameter, and the other side of the cover plate is provided with mounting holes corresponding to the mounting holes distributed around the two semicircular holes on the support (7); one side of the support (7) with the semicircular hole is attached to one side of the cover plate (8) with the semicircular hole and then fixed by a fastener (9).
2. The automatic connection type quick release coupling as claimed in claim 1, wherein the lower coupling (6) is an L-shaped coupling, both ends of the coupling are chamfered at 60 °, the longer end is provided with an annular groove, and the annular groove of the lower coupling (6) is installed in the semicircular holes of the support (7) and the cover plate (8) and is installed and fixed on the support assembly (2).
3. An automatically connecting quick release coupling according to claim 1, wherein the two said lower couplings (6) differ in length at their longer ends.
4. An automatically connectable quick disconnect coupling according to claim 1, wherein the annular groove of the lower coupling (6) is received in the semi-circular holes of the base (7) and the cover plate (8) of the base assembly (2), the annular groove of the lower coupling (6) has a diameter smaller than the semi-circular holes of the base (7) and the cover plate (8), and the annular groove has a height greater than the semi-circular holes of the base (7) and the cover plate (8).
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811322616.5A CN109533347B (en) | 2018-11-07 | 2018-11-07 | Automatic connection type quick-release connector |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
CN201811322616.5A CN109533347B (en) | 2018-11-07 | 2018-11-07 | Automatic connection type quick-release connector |
Publications (2)
Publication Number | Publication Date |
---|---|
CN109533347A CN109533347A (en) | 2019-03-29 |
CN109533347B true CN109533347B (en) | 2021-10-15 |
Family
ID=65845332
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
CN201811322616.5A Active CN109533347B (en) | 2018-11-07 | 2018-11-07 | Automatic connection type quick-release connector |
Country Status (1)
Country | Link |
---|---|
CN (1) | CN109533347B (en) |
Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4303214A (en) * | 1978-05-30 | 1981-12-01 | Hughes Aircraft Company | Apparatus for gyroscopic ejection of shuttle launched spacecraft |
US6217085B1 (en) * | 1997-11-28 | 2001-04-17 | Societe De Prospection Et D'inventions Techniques Spit | Connection for a compressed gas attachment device and compressed gas cartridge |
AU2004100775A4 (en) * | 2001-12-18 | 2004-11-04 | Societe De Prospection Et D'inventions Techniques Spit | Connector for a compressed-gas canister and a fastening appliance |
CN201284359Y (en) * | 2008-10-24 | 2009-08-05 | 江苏凯特尔工业炉有限公司 | Coal gas automatic butt joint for gas bell-type furnace |
CN104295891A (en) * | 2014-10-11 | 2015-01-21 | 凯迈(洛阳)气源有限公司 | Gas filling and gas supply joint for gas cylinder and high-pressure gas cylinder using same |
CN105180909A (en) * | 2015-09-02 | 2015-12-23 | 宁波舜宇测绘科技有限公司 | Connecting seat structure |
CN205469844U (en) * | 2016-03-28 | 2016-08-17 | 四川台风时代航空技术有限公司 | Draw fast and take off device |
CN106015211A (en) * | 2016-06-22 | 2016-10-12 | 浙江绿健胶囊有限公司 | Detachable fastener |
-
2018
- 2018-11-07 CN CN201811322616.5A patent/CN109533347B/en active Active
Patent Citations (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4303214A (en) * | 1978-05-30 | 1981-12-01 | Hughes Aircraft Company | Apparatus for gyroscopic ejection of shuttle launched spacecraft |
US6217085B1 (en) * | 1997-11-28 | 2001-04-17 | Societe De Prospection Et D'inventions Techniques Spit | Connection for a compressed gas attachment device and compressed gas cartridge |
AU2004100775A4 (en) * | 2001-12-18 | 2004-11-04 | Societe De Prospection Et D'inventions Techniques Spit | Connector for a compressed-gas canister and a fastening appliance |
CN201284359Y (en) * | 2008-10-24 | 2009-08-05 | 江苏凯特尔工业炉有限公司 | Coal gas automatic butt joint for gas bell-type furnace |
CN104295891A (en) * | 2014-10-11 | 2015-01-21 | 凯迈(洛阳)气源有限公司 | Gas filling and gas supply joint for gas cylinder and high-pressure gas cylinder using same |
CN105180909A (en) * | 2015-09-02 | 2015-12-23 | 宁波舜宇测绘科技有限公司 | Connecting seat structure |
CN205469844U (en) * | 2016-03-28 | 2016-08-17 | 四川台风时代航空技术有限公司 | Draw fast and take off device |
CN106015211A (en) * | 2016-06-22 | 2016-10-12 | 浙江绿健胶囊有限公司 | Detachable fastener |
Also Published As
Publication number | Publication date |
---|---|
CN109533347A (en) | 2019-03-29 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
RU2137014C1 (en) | Swivel for transfer of fluid medium | |
US20170113762A1 (en) | Disconnectable tower yoke assembly and method of using same | |
CN109533347B (en) | Automatic connection type quick-release connector | |
CN111895196B (en) | Connecting structure and construction method of municipal water supply pipeline | |
AU2013201770B2 (en) | Quick disconnect connector for subsea tubular members | |
CN117146088B (en) | Leakage-proof compensation device for thermal recovery wellhead | |
CN102287268B (en) | State transition valve and system | |
US11781529B2 (en) | Remote conduit de-coupling device | |
CN111306383B (en) | Argon pipeline butt joint structure of molten steel tank | |
CN212864833U (en) | Automatic male joint of tank seat suitable for argon blowing butt joint of molten steel tank | |
CN212868879U (en) | Argon pipe way butt-joint structure of molten steel tank | |
CN212361111U (en) | Easy-to-detach high-sealing-performance movable joint | |
CN212246202U (en) | Oil leak intelligence joint that drops is prevented dragging by filling station's oil gun | |
CN212249880U (en) | Blowout prevention connecting-tripping device | |
CN110005528B (en) | Oil supply method for lubricating oil tank of aircraft engine and flexible oil supply pipe | |
CN111286581B (en) | Tank seat automatic joint suitable for argon blowing butt joint of molten steel tank | |
CN203729904U (en) | Blowout prevention connecting-tripping device sealing and releasing mechanism | |
CN202300490U (en) | Cable transition interface of mining life-saving capsule | |
CN220298754U (en) | Frame is crossed to aerial refueling suspension and wing junction pipeline | |
CN205173782U (en) | A cooling water seal structure for space launch platform | |
CN211550815U (en) | Oil field gas transmission connecting equipment | |
CN221087870U (en) | Spring feeding assembly structure for pump body piston assembly | |
CN215806690U (en) | Valve group composed of pilot pipelines | |
CN216157998U (en) | Oil cylinder bottom assembly | |
CN211554407U (en) | Communication pipeline interfacing apparatus |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PB01 | Publication | ||
PB01 | Publication | ||
SE01 | Entry into force of request for substantive examination | ||
SE01 | Entry into force of request for substantive examination | ||
GR01 | Patent grant | ||
GR01 | Patent grant |