Universal engine nozzle
Universal engine nozzle, Total:168 items.
The international standard classification for "Universal engine nozzle" includes: Aerospace engines and propulsion systems , Military engineering. Military affairs. Weapons .
The Chinese standard classification for "Universal engine nozzle" includes: Engine , Spacecraft power system , Engine auxiliary system and its accessories , Highway vehicle servicing installation .
Professional Standard - Aerospace
- QJ 1016A-1998 General Requirements for Pipeline System of Liquid Rocket Engine
- QJ 1783A-1996 General Specifications for Cavitation Venturi of Liquid Rocket Engine
- QJ 2140A-1997 QJ A 2140-1997 High Altitude Simulation Test for Missile Used Turbojet
- QJ 3284-2006 General specification for solid rocket motor nozzles
- QJ 3032-1998 Equilibrium Method for Turbojet Rotor for Bomb
- QJ 3192-2004 General specification for turbojet engines of missile
- QJ 3193-2004 Structure design criterion for turbojet and turbofan engine of missile
- QJ 2744-1995 Ground Static Test Method of Turbojet Engine for Missile
- QJ 1016-1986 General technical requirements for engine piping system
- QJ 2610-1994 Test Method for Nozzle Deflection Angle of Solid Rocket Motor
- QJ 2746-1995 General Specification for Rack Manufacture, Acceptance and Preservation of Liquid Rocket Engine (LRE)
- QJ 1409-1988 Calculation method and computer program for temperature field of solid rocket motor nozzle
- QJ 2903-1997 Measurement Method of Controlling Moment of Movable Nozzle for Solid Rocket Solid Rocket Engine
- QJ 20032-2011 General specification for metallic hose assemblies of liquid rocket engine
- QJ 2139-1991 General technical requirements for the manufacture and acceptance of solid rocket motor nozzles
- QJ 2273-1992 Measurement method of opening time of solid rocket motor nozzle blockage cover
Military Standard of the People's Republic of China-Commission of Science,Technology and Industry for National Defence
- GJB 5100-2002 Engines,unmanned aircraft,turbojet and turbofan,general specification for
Military Standard of the People's Republic of China-General Armament Department
- GJB 3465-1998 General specification for fuel pumps and controls for aerospace turbojet and turbofan engines
- GJB 3816-1999 General technical requirements for aircraft engine piping systems
- GJB 241-1987 General specifications for aero turbine jet and turbofan engine
- GJB 8968-2017 High-altitude simulation test method of missile turbojet turbofan engine
- GJB 3740-1999 Routine testing of aviation turbojet engines
- GJB 3465A-2015 General specification for fuel pumps and controls for aerospace turbojet and turbofan engines
- GJB/Z 216-2004 Guide to the use of general specifications for aerospace turbojet and turbofan engines
- GJB 4735-1996*GJBz 20339-1996 General specification for air turbine starters for aircraft engines
- GJB 1417-1992 General specifications for ramjet engines
- GJB 8967-2017 Distortion test method of missile turbojet turbofan engine
- GJB 6538-2008 General requirements for aircraft turbojet and aircraft turbofan engines overhaul
- GJB 241A-2010 General specifications for aero turbine jet and turbofan engine
Group Standards of the People's Republic of China
- T/CSF 0086-2024 Portable blower-spray for fire-fighting powered by turbojet engines
- T/ZZB 1796-2020 Engines-Piston cooling jets
Association Standard-China Association for Standardization
- CAS 163-2008 Cleaning agent of the EFI (electronic Fuel Injection) system of gasoline engine
Professional Standard-Ships
- CB 1240-1995 General Specification for Torpedo Engine
Professional Standard - Aviation
- HB 7806-2006 General requirements for digital mock-up of areoengine
- HB 7667-2000 Performance Test of Fuel Nozzle on Aero-Engine
Professional Standard - Civil Aviation
- MH/T 3021-2011 Gas turbine engine fuel nozzle test procedures
Professional Standard - Traffic
- JT/T 638-2005 Cleaning and detecting instrument for spray nozzles of vehicle engine
Society of Automotive Engineers (SAE)
- SAE J1958-1995 DIESEL ENGINES—STEEL TUBES FOR HIGH-PRESSURE FUEL INJECTION PIPES (TUBING)
- SAE J1958-2002 Diesel Engines - Steel Tubes for High-Pressure Fuel Injection Pipes (Tubing)
- SAE ARP458-2002 Universal Maintenance & Overhaul Stand for Turbo-Jet (10,000 Lbs. Thrust Class) and Turbo-Prop Engines
- SAE ARP246-1949 NUMBERING POSITIONS FOR NOZZLES, BURNERS, ETC. FOR TURBO-JET AND TURBO-PROP ENGINES
- SAE ARP741B-2002 Turbofan and Turbojet Gas Turbine Engine Test Cell Correlation
- SAE AS1606-1992 Gas Turbine Starter (Jet Fuel Starter) Specification
- SAE J1668-1999 Diesel Engines Fuel Injection Pump Testing
- SAE AS8181A-2002 Detector, Ice, Air Intake Duct, Aircraft Engines and Airframe Systems, General Specification For
- SAE AIR1147B-2022 Electromagnetic Interference on Aircraft from Jet Engine Charging
- SAE AIR1147A-2013 Electromagnetic Interference on Aircraft from Jet Engine Charging
- SAE ARP4865-2007 GAS TURBINE ENGINE FUEL NOZZLE TEST PROCEDURES
- SAE AIR1191A-1999 Performance of Low Pressure Ratio Ejectors for Engine Nacelle Cooling
- SAE AIR1147-1991 ELECTROMAGNETIC INTERFERENCE ON AIRCRAFT FROM JET ENGINE CHARGING
British Standards Institution (BSI)
- BS ISO 4093:2000 Diesel engines - Fuel injection pumps - High-pressure pipes for testing
- BS ISO 22561:2020 Gasoline engines with direct fuel injection (GDI engines). Installation of the injectors to the engine
- BS ISO 13296:2012 Diesel engines. High-pressure fuel injection pipe assemblies. General requirements and dimensions
- BS ISO 8535-2:2003 Compression ignition engines. Steel tubes for high pressure fuel injection pipes - Requirements for composite tubes
- BS ISO 4093:1999 Diesel engines. Fuel injection pumps. High-pressure pipes for testing
- BS ISO 8535-2:2004 Compression ignition engines - Steel tubes for high pressure fuel injection pipes - Requirements for composite tubes
- 20/30421344 DC BS ISO 22561. Gasoline engines with direct fuel injection (GDI engines). Installation of the injectors to the engine
- 24/30470350 DC Draft ISO 13296 Diesel engines — High-pressure fuel injection pipe assemblies — General requirements and dimensions
- 19/30361639 DC BS ISO 22561. Gasoline engines with direct fuel injection (GDI engines). Installation of the injectors to the engine
- BS ISO 8535-1:2016 Diesel engines. Steel tubes for high-pressure fuel injection pipes - Requirements for seamless cold-drawn single-wall tubes
- BS ISO 21042:2018 Gasoline engines with direct fuel injection (GDI engines). Installation of the high pressure fuel pump to the engine
- BS ISO 2697:2000 Diesel engines - Fuel nozzles - Size "S"
- BS ISO 2697:1999 Diesel engines - Fuel nozzles - Size "S"
- BS ISO 19724:2016 Gasoline engines with direct injection. Cleanliness assessment of fuel injection equipment
- 17/30332768 DC BS ISO 21042. Gasoline engines with direct fuel injection (GDI engines). Installation of the high pressure fuel pump to the engine
- BS ISO 7299:1997 Diesel engines - End-mounting flanges for fuel injection pumps
- BS ISO 13296:2016 Diesel engines. High-pressure fuel injection pipe assemblies. General requirements and dimensions
SCC
- MIL MIL-E-5007D-1973 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR (SUPERSEDING MIL-E-5007C)
- BS ISO 8535-1:2006 Diesel engines. Steel tubes for high-pressure fuel injection pipes-Requirements for seamless cold-drawn single-wall tubes
- BS ISO 8535-1:1996 Compression ignition engines. Steel tubes for high pressure fuel injection pipes-Requirements for seamless cold drawn single wall tubes
- MIL MIL-T-83431-1974 TEST STAND, JET ENGINE ACCESSORY OVERHAUL GENERAL SPECIFICATION FOR (NO S/S DOCUMENT)
- MIL MIL-I-22027-1959 IGNITER, JET ENGINE, MK 243 MOD 2
- MIL MIL-DTL-82068D-2012 Sprayers, Pesticide; Trailer-Mounted, Gasoline-Engine-Driven
- BS ISO 13296:1997 Diesel engines. High pressure fuel injection pipe assemblies. General requirements and dimensions
- UNE 26492-2:2001 Road vehicles. Compression ignition engines. Steel tubes for high pressure fuel inyection. Part 2: Requirements for composite tubes.
- BS ISO 13296:2005 Diesel engines. High-pressure fuel injection pipe assemblies. General requirements and dimensions
- MIL MIL-PRF-6081E-2014 LUBRICATING OIL, JET ENGINE (SUPERSEDING MIL-L-6081D)
- MIL MIL-PRF-6081D-1997 LUBRICATING OIL, JET ENGINE (SUPERSEDING MIL-L-6081C)
International Organization for Standardization (ISO)
- ISO 13296:2016 Diesel engines - High-pressure fuel injection pipe assemblies - General requirements and dimensions
- ISO 13296:2012 Diesel engines - High-pressure fuel injection pipe assemblies - General requirements and dimensions
- ISO 22561:2020 Gasoline engines with direct fuel injection (GDI engines) - Installation of the injectors to the engine
- ISO 8535-2:2003 Compression-ignition engines - Steel tubes for high-pressure fuel injection pipes - Part 2: Requirements for composite tubes
- ISO 8535-2:1993 Compression-ignition engines — Steel tubes for high-pressure fuel injection pipes — Part 2: Requirements for composite tubes
- ISO 21042:2018 Gasoline engines with direct fuel injection (GDI engines) - Installation of the high pressure fuel pump to the engine
- ISO 8535-1:1996 Compression-ignition engines - Steel tubes for high-pressure fuel injection pipes - Part 1: Requirements for seamless cold-drawn single-wall tubes
- ISO 2698:1974 Diesel engines — Injection nozzle holder — Type 7
- ISO 19724:2016 Gasoline engines with direct injection - Cleanliness assessment of fuel injection equipment
- ISO 8535-1:2011 Diesel engines - Steel tubes for high-pressure fuel injection pipes - Part 1: Requirements for seamless cold-drawn single-wall tubes
- ISO 13296:2005 Diesel engines - High-pressure fuel injection pipe assemblies - General requirements and dimensions
- ISO 8535-1:2006 Diesel engines - Steel tubes for high-pressure fuel injection pipes - Part 1: Requirements for seamless cold-drawn single-wall tubes
- ISO 8535-1:1989 Compression-ignition engines — Steel tubes for high-pressure fuel injection pipes — Part 1: Requirements for seamless cold-drawn single-wall steel tubes
Korean Agency for Technology and Standards (KATS)
- KS W 4611-2013 GENERAL SPECIFICATION OF TURBOJET ENGINES AND TURBOFAN ENGINES FOR AIRCRAFT
- KS W 4611-1978 General specification of turbojet engines and turbofan engines for aircraft
- KS W 4611-1996 General specification of turbojet engines and turbofan engines for aircraft
- KS V 4332-2013 Fuel injector of marine small diesel engine
- KS R ISO 14681-2022 Diesel engines-Fuel injection pump testing-Calibrating fuel injectors
- KS R 3048-2009 Diesel engines-Tapers for shaft ends of fuel injection pumps and hubs
- KS W 4611-1996(2011) GENERAL SPECIFICATION OF TURBOJET ENGINES AND TURBOFAN ENGINES FOR AIRCRAFT
- KS R 3009-2013 In-line fuel injection pumps for automobile diesel engines
- KS R ISO 2697-2007(2017) Diesel engines-Fuel nozzles-Size “S”
- KS R ISO 13296:2020 Diesel engines — High-pressure fuel injection pipe assemblies — General requirements and dimensions
- KS R ISO 14681-2007(2017) Diesel engines-Fuel injection pump testing-Calibrating fuel injectors
U.S. Air Force
- AIR FORCE MIL-PRF-6081 D (1)-2009 LUBRICATING OIL, JET ENGINE
- AIR FORCE QPL-6081-QPD-2010 Lubricating Oil, Jet Engine
- AIR FORCE QPL-6081-QPD-2011 Lubricating Oil, Jet Engine
- AIR FORCE QPL-6081-2013 Lubricating Oil, Jet Engine
- AIR FORCE MIL-N-83158 A-1970 NOISE SUPPRESSOR SYSTEMS, ENGINE TEST STAND A/F32T-2 AND A/F32T-3; FOR TURBOJET AND TURBOFAN ENGINES
- AIR FORCE A-A-58038 VALID NOTICE 1-2012 Diesel Engine Fuel Injector Cleaner
Japanese Industrial Standards Committee (JISC)
- JIS D 3607:1993 Automotive diesel engines -- Steel tubes for high-pressure fuel injection pipes
- JIS D 3612:2023 Direct injection gasoline engines -- Installation of the high pressure fuel injector to the engine
- JIS W 4601:1996 General specification of turbojet engines and turbofan engines for aircraft
- JIS D 3603:1993 Automotive diesel engines -- Fuel injection pumps -- Shapes and dimensions
- JIS D 3607-2:2002 Diesel engines -- Steel tubes for high-pressure fuel injection pipes -- Part 2: Requirements for composite tubes
- JIS B 8035:1994 Testing method for fuel injection pump of diesel engine
- JIS D 0116-1:2001 Diesel engines -- Vocabulary of fuel injection equipment -- Part 1: Fuel injection pumps
- JIS D 0116-2:2001 Diesel engines -- Vocabulary of fuel injection equipment -- Part 2: Fuel injectors
United States Navy
- NAVY MIL-T-85630 VALID NOTICE 1-1991 TUBE, MOTOR, FOR 2.75 INCH ROCKET, MARK 66
- NAVY MIL-T-85630-1983 TUBE, MOTOR, FOR 2.75 INCH ROCKET, MARK 66
- NAVY MIL-E-005007 E-1983 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
- NAVY MIL-E-5007 D (3)-1995 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
- NAVY MIL-E-5007 D-1973 ENGINE, AIRCRAFT, TURBOJET AND TURBOFAN, GENERAL SPECIFICATION FOR
- NAVY MIL-I-22027 NOTICE 1-1996 IGNITER, JET ENGINE, MK 243 MOD 2
- NAVY QPL-22999-2012 STARTER, AIRCRAFT ENGINE, HYDRAULIC GENERAL SPECIFICATION FOR
- NAVY MIL-I-22027-1959 IGNITER, JET ENGINE, MK 243 MOD 2
ESDU - Engineering Sciences Data Unit
- ESDU 76034-1976 Estimation of take-off thrust using generalised data for turbo-jet and turbo-fan engines.
SAE - SAE International
- SAE J1958-2015 Diesel Engines - Steel Tubes for High-Pressure Fuel Injection Pipes (Tubing)
- SAE J1958-1989 Diesel Engines - Steel Tubes for High-Pressure Fuel Injection Pipes (Tubing)
- SAE ARP458-1954 UNIVERSAL MAINTENANCE AND OVERHAUL STAND FOR TURBO-JET (10@000 LBS. THRUST CLASS) AND TURBO-PROP ENGINES
- SAE J1668-2016 Diesel Engines - Fuel Injection Pump Testing
- SAE J1668-2021 Diesel Engines - Fuel Injection Pump Testing
- SAE J1668-1993 Diesel Engines - Fuel Injection Pump Testing
- SAE AS8181-1997 Detector@ Ice@ Air Intake Duct@ Aircraft Engines and Airframe Systems@ General Specification for
- SAE AS8181A-1997 Detector@ Ice@ Air Intake Duct@ Aircraft Engines and Airframe Systems@ General Specification for
- SAE AIR1147A-1998 Electromagnetic Interference on Aircraft from Jet Engine Charging
- SAE AIR1147-1970 Electromagnetic Interference on Aircraft from Jet Engine Charging
U.S. Military Regulations and Norms
- ARMY MIL-G-51491 A-1986 GENERATOR, SMOKE, MECHANICAL PULSE JET, M3A4
- ARMY MIL-G-51491 A (1)-1998 GENERATOR, SMOKE, MECHANICAL PULSE JET, M3A4
- ARMY MIL-G-51491 A VALID NOTICE 2-2004 GENERATOR, SMOKE, MECHANICAL PULSE JET, M3A4
- ARMY MIL-G-51491 A NOTICE 1-1995 GENERATOR, SMOKE, MECHANICAL PULSE JET, M3A4
- ARMY A-A-52030-1991 NOZZLES, FUEL AND OIL SERVICING, NONAUTOMATIC SHUTOFF AND NOZZLES, FUEL SERVICING, AUTOMATIC SHUTOFF
ES-AENOR
- UNE 51-506-1985 JP-4 fuel for turbojet engines
- UNE 10-101-1990 Heat engine. Jet pump. Measuring diameter of high pressure pipe
- INTA 15 13 14 JP4 fuel turbojet engine
- INTA 15 33 12 Type 10 lubricating oil for aviation turbojet engines
GSO
- GSO ISO 8535-2:2013 Compression-ignition engines -- Steel tubes for high-pressure fuel injection pipes -- Part 2: Requirements for composite tubes
- BH GSO ISO 14681:2016 Diesel engines -- Fuel injection pump testing -- Calibrating fuel injectors
- GSO ISO 14681:2013 Diesel engines -- Fuel injection pump testing -- Calibrating fuel injectors
- BH GSO ISO 2697:2017 Diesel engines -- Fuel nozzles -- Size "S"
- OS GSO ISO 2697:2016 Diesel engines -- Fuel nozzles -- Size "S"
- GSO ISO 2697:2016 Diesel engines -- Fuel nozzles -- Size "S"
- GSO ISO 6519:2014 Diesel engines -- Fuel injection pumps -- Tapers for shaft ends and hubs
RO-ASRO
- STAS 7326-1974 INJECTION NOZZLES FOR COMPRESSION IGNITION ENGINES Rules and test methods
- STAS 9420-1987 Compression ignition engines SPRAY NOZZLES Dimensions
- STAS 6582-1987 INJECTION PUMPS ON LINE FOR COMPRESSION IGNITION ENGINES Numbering of pumping sections
- STAS 8611-1987 FUELS FOR TURBO-JET ENGINES Determination of mechanical impurities
RU-GOST R
- GOST 10227-1986 Jetfuels. Specifications
- GOST 17750-1972 Jet fuel. Method for the determination luminometric number on the PLCHT instrument
- GOST 13211-1980 Shell and tube water-oil and water-water type cooltrs of diesels engines and gas engines. General specifications
- GOST 5616-1989 Water-wheel type generators and motor-generators. General specifications
- GOST 12308-2013 Thermostable fuels T-6 and T-8B for jet engines. Specifications
AR-IRAM
- IRAM 6549-1959 Fuel for aviation turbojet engines
KR-KS
- KS R ISO 6519-2018(2023) Diesel engines — Fuel injection pumps — Tapers for shaft ends and hubs
- KS R ISO 13296-2020 Diesel engines — High-pressure fuel injection pipe assemblies — General requirements and dimensions
GB-REG
- REG NASA-LLIS-0105-1992 Lessons Learned - OMS Engine Nozzle Cover
German Institute for Standardization
- DIN ISO 2697:2002-05 Diesel engines - Fuel nozzles - Size "S" (ISO 2697:1999)
American Society for Testing and Materials (ASTM)
- ASTM D6894-08 Standard Test Method for Evaluation of Aeration Resistance of Engine Oils in Direct-Injected Turbocharged Automotive Diesel Engine
Underwriters Laboratories (UL)
- UL 401-2022 Portable spray hose nozzles for fire protection service
- UL 401-1993 Portable spray hose nozzles for fire protection service
General purpose for aviation turbojet and turbofan engines,General requirements for aero-engine ground test bench,General purpose aviation rotary engine for UAV,General requirements for field quality monitoring of aero-engines,General requirements for cleaning of helicopter turboshaft engines,Liquid rocket engine electropneumatic valve universal,Liquid Rocket Engine Cavitation Venturi Universal,engine common