GB669008A - Improvements relating to jet-propelled missiles - Google Patents
Improvements relating to jet-propelled missilesInfo
- Publication number
- GB669008A GB669008A GB14592/50A GB1459250A GB669008A GB 669008 A GB669008 A GB 669008A GB 14592/50 A GB14592/50 A GB 14592/50A GB 1459250 A GB1459250 A GB 1459250A GB 669008 A GB669008 A GB 669008A
- Authority
- GB
- United Kingdom
- Prior art keywords
- jet
- nozzle
- chamber
- june
- diffusor
- 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.)
- Expired
Links
- 238000002485 combustion reaction Methods 0.000 abstract 2
- 230000006835 compression Effects 0.000 abstract 2
- 238000007906 compression Methods 0.000 abstract 2
- 239000000567 combustion gas Substances 0.000 abstract 1
- 238000010304 firing Methods 0.000 abstract 1
- 239000000446 fuel Substances 0.000 abstract 1
- 239000007788 liquid Substances 0.000 abstract 1
- 239000004449 solid propellant Substances 0.000 abstract 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/105—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines using a solid fuel
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
- F02K7/10—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
- F02K7/18—Composite ram-jet/rocket engines
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
-
- H—ELECTRICITY
- H10—SEMICONDUCTOR DEVICES; ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N—ELECTRIC SOLID-STATE DEVICES NOT OTHERWISE PROVIDED FOR
- H10N60/00—Superconducting devices
- H10N60/01—Manufacture or treatment
- H10N60/0912—Manufacture or treatment of Josephson-effect devices
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10S—TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10S60/00—Power plants
- Y10S60/917—Solid fuel ramjet using pulverized fuel
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Manufacturing & Machinery (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Nozzles For Spraying Of Liquid Fuel (AREA)
Abstract
669,008. Jet propulsion plant. AKTIEBOLAGET BOFORS. June 12, 1950. [June 16, 1949] No. 14592/50. Class 110(iii). [Also in Group XXI] Relates to jet-propelled mis siles fired from a gun or similar device and comprising an outer shell and an inner co-axial body between which is an annular cavity for a ram-jet motor consisting of a compression nozzle, a diffusor, a combustion chamber and an exhaust nozzle. Before firing the com pression nozzle is closed by the inner body 2 which, after launching, is retarded relatively to the shell 1 to expose ar annular passage 5 througl which air compressed against the surface 4 of the inner body enters to become further com pressed in the diffusor chamber 6. From the chamber 6 the air passes into the combustion chamber 7 where the fuel 8 is ignited, the combustion gases escaping through the exhaust nozzle 9. Liquid, gaseous or solid fuels or a combination of these may be used.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
SE286895X | 1949-06-16 | ||
SE669014X | 1949-07-07 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB669008A true GB669008A (en) | 1952-03-26 |
Family
ID=26656214
Family Applications (2)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB14592/50A Expired GB669008A (en) | 1949-06-16 | 1950-06-12 | Improvements relating to jet-propelled missiles |
GB16535/50A Expired GB669014A (en) | 1949-06-16 | 1950-07-03 | Improvements relating to jet-propelled missiles |
Family Applications After (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB16535/50A Expired GB669014A (en) | 1949-06-16 | 1950-07-03 | Improvements relating to jet-propelled missiles |
Country Status (5)
Country | Link |
---|---|
US (2) | US2684570A (en) |
BE (2) | BE496372A (en) |
CH (2) | CH286895A (en) |
FR (2) | FR1020175A (en) |
GB (2) | GB669008A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2906094A (en) * | 1954-04-14 | 1959-09-29 | Glenn H Damon | Fuel and rapid ignition apparatus for ignition of fuel in ram jets and rockets |
US2948112A (en) * | 1953-12-14 | 1960-08-09 | Kenneth W Smith | Combined rocket and ram-jet engine |
US2989922A (en) * | 1953-02-17 | 1961-06-27 | Marvin H Greenwood | Ramjet propulsion device |
DE1213760B (en) * | 1962-06-30 | 1966-03-31 | Rheinmetall Gmbh | Self-propelled hollow charge projectile |
Families Citing this family (32)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2990682A (en) * | 1951-11-07 | 1961-07-04 | Gen Electric | Fuel charge |
US2840322A (en) * | 1952-09-23 | 1958-06-24 | Rolls Royce | Air intake for aircraft power plant installations |
US2811829A (en) * | 1952-12-04 | 1957-11-05 | Alfred A Topinka | Ram jet employing carbon layer of insulation for solid carbon propellant |
US2799987A (en) * | 1952-12-31 | 1957-07-23 | Edward F Chandler | Solid fuel ramjet projectiles |
US2912820A (en) * | 1953-07-31 | 1959-11-17 | Quentin R Whitmore | Combined ram jet and rocket engine |
US3069300A (en) * | 1954-12-30 | 1962-12-18 | Glenn H Damon | Boron containing fuel and fuel igniter for ram jet and rocket |
US2883829A (en) * | 1955-01-24 | 1959-04-28 | Curtiss Wright Corp | Rocket engine convertible to a ramjet engine |
US2926613A (en) * | 1955-05-23 | 1960-03-01 | Phillips Petroleum Co | Composite rocket-ram jet fuel |
US3903802A (en) * | 1955-08-26 | 1975-09-09 | Us Army | Shell construction sealing washer |
DE1025215B (en) * | 1955-11-07 | 1958-02-27 | Max Koppe Dr Rer Pol Dr Rer Na | Jet engine for unmanned and manned missiles of all types |
US2936710A (en) * | 1956-01-03 | 1960-05-17 | Curtiss Wright Corp | High mach deceleration device |
US3048009A (en) * | 1956-06-21 | 1962-08-07 | Phillips Petroleum Co | Rocket motor |
US2977879A (en) * | 1957-09-18 | 1961-04-04 | Atlantic Res Corp | Rocket projectile |
US3115008A (en) * | 1959-02-03 | 1963-12-24 | Cohen William | Integral rocket ramjet missile propulsion system |
DE1144060B (en) * | 1960-08-04 | 1963-02-21 | Daimler Benz Ag | Compound engine for aircraft |
US3220181A (en) * | 1962-11-08 | 1965-11-30 | Texaco Experiment Inc | Split-flow solid fuel ramjet |
US3218974A (en) * | 1964-03-24 | 1965-11-23 | Samms Adolphus | Air breathing booster |
US3974648A (en) * | 1968-08-19 | 1976-08-17 | United Technologies Corporation | Variable geometry ramjet engine |
US3726219A (en) * | 1970-03-24 | 1973-04-10 | Us Navy | Integral propellant case ramjet projectile |
US4135449A (en) * | 1975-06-20 | 1979-01-23 | Rheinmetall Gmbh | Projectile for attacking small targets |
US4338783A (en) * | 1975-09-04 | 1982-07-13 | The United States Of America As Represented By The Secretary Of The Air Force | Two-stage hypersonic ramjet |
US4052846A (en) * | 1976-01-08 | 1977-10-11 | The United States Of America As Represented By The Secretary Of The Navy | Baffled combustion chamber |
FR2666850B1 (en) * | 1978-08-04 | 1994-09-09 | Onera (Off Nat Aerospatiale) | IMPROVEMENTS RELATING TO STATOREACTOR TYPE PROPELLERS. |
US4745740A (en) * | 1982-09-30 | 1988-05-24 | The Boeing Company | Velocity controller for ramjet missile and method therefor |
GB2165338B (en) * | 1984-10-06 | 1988-11-02 | Rolls Royce | Integral rocket and ramjet engine |
US5363766A (en) * | 1990-02-08 | 1994-11-15 | The United States Of America As Represented By The Secretary Of The Army | Remjet powered, armor piercing, high explosive projectile |
US6058846A (en) * | 1998-06-03 | 2000-05-09 | Lockhead Martin Corporation | Rocket and ramjet powered hypersonic stealth missile having alterable radar cross section |
DE10158277A1 (en) * | 2001-11-20 | 2003-05-28 | Mieczyslaw Milewski | Device for adjusting the aerodynamics of a rocket comprises channels which guide the atmospheric air from the direction opposite the exit of the waste gas stream into the region of the jets of the propulsion system |
US7851733B2 (en) * | 2006-07-10 | 2010-12-14 | Raytheon Company | Methods and apparatus for missile air inlet |
US8117847B2 (en) * | 2008-03-07 | 2012-02-21 | Raytheon Company | Hybrid missile propulsion system with reconfigurable multinozzle grid |
US20110314791A1 (en) * | 2010-06-25 | 2011-12-29 | Haynes Jeffrey D | Method for combustion system |
FR3080912B1 (en) * | 2018-05-02 | 2020-04-03 | Nexter Munitions | PROJECTILE POWERED BY STATOREACTOR |
Family Cites Families (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB590177A (en) * | 1944-07-17 | 1947-07-10 | Hydran Products Ltd | Improvements in or relating to projectiles of the rocket type |
GB293594A (en) * | 1925-12-19 | 1928-08-16 | Benjamin Charles Carter | Improvements in or relating to apparatus for burning liquid or gaseous fuel and in the application thereof to internal combustion turbines, turbo-airscrews, projectiles, rockets and the like |
FR779655A (en) * | 1934-01-02 | 1935-04-10 | Process for transforming heat energy into kinetic or potential energy | |
FR47412E (en) * | 1938-07-05 | 1937-05-05 | Process for transforming heat energy into kinetic or potential energy | |
GB579807A (en) * | 1941-02-11 | 1946-08-16 | Walter Gordon Wilson | Improvements in and relating to the propulsion of aerial torpedoes |
US2446266A (en) * | 1946-02-23 | 1948-08-03 | Thomas L Cummings | Jet propelled helicopter rotor |
US2540594A (en) * | 1946-08-23 | 1951-02-06 | Lockheed Aircraft Corp | Ram jet engine having variable area inlets |
-
1950
- 1950-06-07 US US166594A patent/US2684570A/en not_active Expired - Lifetime
- 1950-06-07 US US166593A patent/US2684629A/en not_active Expired - Lifetime
- 1950-06-12 GB GB14592/50A patent/GB669008A/en not_active Expired
- 1950-06-14 FR FR1020175D patent/FR1020175A/en not_active Expired
- 1950-06-14 CH CH286895D patent/CH286895A/en unknown
- 1950-06-14 FR FR1020174D patent/FR1020174A/en not_active Expired
- 1950-06-15 BE BE496372D patent/BE496372A/xx unknown
- 1950-07-03 GB GB16535/50A patent/GB669014A/en not_active Expired
- 1950-07-04 BE BE496772D patent/BE496772A/xx unknown
- 1950-07-06 CH CH287258D patent/CH287258A/en unknown
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2989922A (en) * | 1953-02-17 | 1961-06-27 | Marvin H Greenwood | Ramjet propulsion device |
US2948112A (en) * | 1953-12-14 | 1960-08-09 | Kenneth W Smith | Combined rocket and ram-jet engine |
US2906094A (en) * | 1954-04-14 | 1959-09-29 | Glenn H Damon | Fuel and rapid ignition apparatus for ignition of fuel in ram jets and rockets |
DE1213760B (en) * | 1962-06-30 | 1966-03-31 | Rheinmetall Gmbh | Self-propelled hollow charge projectile |
Also Published As
Publication number | Publication date |
---|---|
FR1020174A (en) | 1953-02-03 |
BE496772A (en) | 1950-11-03 |
CH287258A (en) | 1952-11-30 |
US2684570A (en) | 1954-07-27 |
FR1020175A (en) | 1953-02-03 |
CH286895A (en) | 1952-11-15 |
BE496372A (en) | 1950-10-02 |
US2684629A (en) | 1954-07-27 |
GB669014A (en) | 1952-03-26 |
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