CN108194231A - A kind of small-scale solid rocket motor jet pipe blanking cover - Google Patents

A kind of small-scale solid rocket motor jet pipe blanking cover Download PDF

Info

Publication number
CN108194231A
CN108194231A CN201711357894.XA CN201711357894A CN108194231A CN 108194231 A CN108194231 A CN 108194231A CN 201711357894 A CN201711357894 A CN 201711357894A CN 108194231 A CN108194231 A CN 108194231A
Authority
CN
China
Prior art keywords
blanking cover
jet pipe
small
rocket motor
solid rocket
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.)
Pending
Application number
CN201711357894.XA
Other languages
Chinese (zh)
Inventor
靳向往
王峰
李先聚
刘国斌
边国军
李恒
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Inner Mongolia Power Machinery Research Institute
Original Assignee
Inner Mongolia Power Machinery Research Institute
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Inner Mongolia Power Machinery Research Institute filed Critical Inner Mongolia Power Machinery Research Institute
Priority to CN201711357894.XA priority Critical patent/CN108194231A/en
Publication of CN108194231A publication Critical patent/CN108194231A/en
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/97Rocket nozzles
    • F02K9/978Closures for nozzles; Nozzles comprising ejectable or discardable elements

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Gasket Seals (AREA)

Abstract

The present invention relates to a kind of jet pipe blanking cover more particularly to a kind of small-scale solid rocket motor blanking covers.Blanking cover connection screw thread and cut groove are provided on jet pipe blanking cover, jet pipe blanking cover is connect by blanking cover connection screw thread with jet pipe housing sidewall, and cut groove is set on blanking cover and jet pipe contact surface.Solid propellant rocket blanking cover provided by the present invention improves the reliability of solid propellant rocket work, suitable for most of small-scale solid rocket motor, it can be achieved that blanking cover is reliably connected.

Description

A kind of small-scale solid rocket motor jet pipe blanking cover
Technical field
The present invention relates to a kind of jet pipe blanking cover more particularly to a kind of small-scale solid rocket motor blanking covers.
Background technology
Jet pipe blanking cover is one of critical component of solid propellant rocket, and major function has two aspects:First, sealing is anti- Tide prevents outside air from entering combustion chamber, influences solid propellant rocket storage life;Second is that provide wink in engine ignition When closed container, combustion gas is made to stay for some time in the combustion chamber, engine is helped to build pressure rapidly, shortening ignition delay time, Realize reliable ignition.Existing jet pipe blanking cover use is bonded or welded mode and is fixed in jet pipe other parts.Bonding way is by viscous The influence of the factors such as surface treatment situation, specific technique for sticking and condition of cure is connect, adhesive property is unstable, and long term storage In, aging or embrittlement under cryogenic due to bonding agent so that gas leak phenomenon occurs for bonding site part unsticking.Welding Mode is suitable for jet pipe blanking cover and is same metal material to pipe fitting, and application range is narrow.
Invention content
The technical problems to be solved by the invention:
The present invention provides a kind of small-scale solid rocket motor blanking cover, realizes being reliably connected for blanking cover, improves solid-rocket and starts The reliability of machine work, suitable for most of small-scale solid rocket motor.
The technical solution adopted in the present invention:
A kind of small-scale solid rocket motor jet pipe blanking cover, the blanking cover 3 are equipped with blanking cover connection screw thread 4, and jet pipe blanking cover leads to It crosses blanking cover connection screw thread 4 to connect with jet pipe housing sidewall, is provided with cut groove 5 on the jet pipe blanking cover, cut groove is set to stifled On lid and jet pipe contact surface.
Preferably, the blanking cover connection screw thread 4 is connect by sealing ring 2 with jet pipe side wall.
Beneficial effects of the present invention:
The present invention provides a kind of small-scale solid rocket motor blanking cover, realizes being reliably connected for blanking cover, improves solid-rocket and starts The reliability of machine work, suitable for most of small-scale solid rocket motor.
Description of the drawings
Fig. 1:Jet pipe blanking cover and jet pipe housing connection diagram.
Fig. 2:Jet pipe blocking cover structure schematic diagram.
Fig. 3:Jet pipe housing and jet pipe blanking cover connecting portion structure diagram.
Specific embodiment
Below in conjunction with the accompanying drawings and specific embodiment the present invention is described in further detail.
As illustrated in fig. 1 and 2, a kind of small-scale solid rocket motor jet pipe blanking cover, the blanking cover 3 are connected equipped with blanking cover Screw thread 4, jet pipe blanking cover are connect by blanking cover connection screw thread 4 with jet pipe housing sidewall, and cut groove is provided on the jet pipe blanking cover, Cut groove is set on blanking cover and jet pipe contact surface.The blanking cover connection screw thread 4 is connect by sealing ring 2 with jet pipe side wall. When it is implemented, being required according to nozzle closure opening pressure, cut groove 5 and connection screw thread 4,7 sizes are calculated.2 side of sealing ring Seal compression selects 15%.Jet pipe blanking cover of the present invention by sealing ring 2 in use, be installed to jet pipe housing seal slot 6, in sealing ring 2 Surface applies a small amount of lubricating grease, and jet pipe blanking cover 3 is installed to jet pipe housing 1, completes the installation of jet pipe blanking cover.

Claims (3)

1. a kind of small-scale solid rocket motor jet pipe blanking cover, it is characterised in that:The blanking cover(3)It is equipped with blanking cover and connects spiral shell Line(4), jet pipe blanking cover passes through blanking cover connection screw thread(4)It is connect with jet pipe housing sidewall, shearing is provided on the jet pipe blanking cover Slot(5), cut groove is set on blanking cover and jet pipe contact surface.
2. jet pipe blanking cover according to claim 1, it is characterised in that:The blanking cover connection screw thread(4)Pass through sealing ring (2)It is connect with jet pipe side wall.
3. jet pipe blanking cover according to claim 2, it is characterised in that:The sealing ring seal compression is 15%.
CN201711357894.XA 2017-12-17 2017-12-17 A kind of small-scale solid rocket motor jet pipe blanking cover Pending CN108194231A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
CN201711357894.XA CN108194231A (en) 2017-12-17 2017-12-17 A kind of small-scale solid rocket motor jet pipe blanking cover

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
CN201711357894.XA CN108194231A (en) 2017-12-17 2017-12-17 A kind of small-scale solid rocket motor jet pipe blanking cover

Publications (1)

Publication Number Publication Date
CN108194231A true CN108194231A (en) 2018-06-22

Family

ID=62574747

Family Applications (1)

Application Number Title Priority Date Filing Date
CN201711357894.XA Pending CN108194231A (en) 2017-12-17 2017-12-17 A kind of small-scale solid rocket motor jet pipe blanking cover

Country Status (1)

Country Link
CN (1) CN108194231A (en)

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109026445A (en) * 2018-07-12 2018-12-18 上海新力动力设备研究所 Multi nozzle solid attitude control engine blocking cover structure
CN110259608A (en) * 2019-06-19 2019-09-20 湖北三江航天红峰控制有限公司 A kind of solid rail control engine jet pipe blanking cover
CN110905686A (en) * 2019-10-30 2020-03-24 北京动力机械研究所 Multi-flow-path combined engine starting protection structure
CN111502862A (en) * 2020-04-29 2020-08-07 内蒙动力机械研究所 Plug-in type low pass filter
CN112523902A (en) * 2020-11-30 2021-03-19 内蒙动力机械研究所 3D printing-based composite material fixing shell for spray pipe

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204438928U (en) * 2014-12-09 2015-07-01 晋西工业集团有限责任公司 A kind of civil rocket bullet monoblock type projectile tail
CN106930866A (en) * 2017-01-26 2017-07-07 北京航空航天大学 A kind of solid-liquid rocket ground experiment jet pipe blocking cover structure

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN204438928U (en) * 2014-12-09 2015-07-01 晋西工业集团有限责任公司 A kind of civil rocket bullet monoblock type projectile tail
CN106930866A (en) * 2017-01-26 2017-07-07 北京航空航天大学 A kind of solid-liquid rocket ground experiment jet pipe blocking cover structure

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN109026445A (en) * 2018-07-12 2018-12-18 上海新力动力设备研究所 Multi nozzle solid attitude control engine blocking cover structure
CN110259608A (en) * 2019-06-19 2019-09-20 湖北三江航天红峰控制有限公司 A kind of solid rail control engine jet pipe blanking cover
CN110905686A (en) * 2019-10-30 2020-03-24 北京动力机械研究所 Multi-flow-path combined engine starting protection structure
CN111502862A (en) * 2020-04-29 2020-08-07 内蒙动力机械研究所 Plug-in type low pass filter
CN112523902A (en) * 2020-11-30 2021-03-19 内蒙动力机械研究所 3D printing-based composite material fixing shell for spray pipe

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Application publication date: 20180622