GB1413845A - Marine propulsion - Google Patents
Marine propulsionInfo
- Publication number
- GB1413845A GB1413845A GB647572A GB647572A GB1413845A GB 1413845 A GB1413845 A GB 1413845A GB 647572 A GB647572 A GB 647572A GB 647572 A GB647572 A GB 647572A GB 1413845 A GB1413845 A GB 1413845A
- Authority
- GB
- United Kingdom
- Prior art keywords
- turbine
- driven
- compressed air
- combustion device
- feb
- 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
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B60—VEHICLES IN GENERAL
- B60V—AIR-CUSHION VEHICLES
- B60V1/00—Air-cushion
- B60V1/14—Propulsion; Control thereof
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B63—SHIPS OR OTHER WATERBORNE VESSELS; RELATED EQUIPMENT
- B63H—MARINE PROPULSION OR STEERING
- B63H11/00—Marine propulsion by water jets
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- Aviation & Aerospace Engineering (AREA)
- Transportation (AREA)
- Ocean & Marine Engineering (AREA)
- Supercharger (AREA)
- Structures Of Non-Positive Displacement Pumps (AREA)
- Jet Pumps And Other Pumps (AREA)
Abstract
1413845 Marine propulsion ROLLS-ROYCE (1971) Ltd 13 Feb 1973 [11 Feb 1972] 6475/72 Heading B7V A water jet propulsion unit includes a turbine 22 which drives an impulse rotor 18 at the downstream end of a divergent/convergent portion 16 of the units' water flow duet. The turbine 22 is driven by gases from a combustion device 20 and the turbine exhaust gases are discharged through slots 36 into the water stream. The turbine and combustion device are contained in a body which is located within the water flow duct and which is fed with fuel and compressed air through a hollow strut 12. The source of compressed air may be a compressor driven by a gas generator, Fig. 5 (not shown). Alternatively, Figs. 6 and 7 (not shown), the source may be a gas turbine engine which may feed gas from an extra compression stage through a combustion device and a turbine. As a further alternative, Fig. 8 (not shown), compressed air is supplied by a pair of compressors connected in series with an intercooler. The compressors are driven by series connected turbines driven in turn by a gas generator.
Priority Applications (6)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB647572A GB1413845A (en) | 1972-02-11 | 1972-02-11 | Marine propulsion |
US00329334A US3808804A (en) | 1972-02-11 | 1973-02-05 | Marine propulsion |
DE19732306513 DE2306513C3 (en) | 1972-02-11 | 1973-02-09 | Thrust tube water jet drive with propellant gas admixture for watercraft |
JP48016361A JPS4919588A (en) | 1972-02-11 | 1973-02-09 | |
IT20242/73A IT978983B (en) | 1972-02-11 | 1973-02-09 | IMPROVEMENTS RELATING TO PRO MARINE PULSERS |
FR7304630A FR2171351B1 (en) | 1972-02-11 | 1973-02-09 |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB647572A GB1413845A (en) | 1972-02-11 | 1972-02-11 | Marine propulsion |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1413845A true GB1413845A (en) | 1975-11-12 |
Family
ID=9815163
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB647572A Expired GB1413845A (en) | 1972-02-11 | 1972-02-11 | Marine propulsion |
Country Status (5)
Country | Link |
---|---|
US (1) | US3808804A (en) |
JP (1) | JPS4919588A (en) |
FR (1) | FR2171351B1 (en) |
GB (1) | GB1413845A (en) |
IT (1) | IT978983B (en) |
Families Citing this family (20)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4343611A (en) * | 1979-01-05 | 1982-08-10 | Rolls-Royce Limited | Marine propulsion |
DE3009671A1 (en) * | 1980-03-13 | 1981-09-24 | Schottel-Werft Josef Becker Gmbh & Co Kg, 5401 Spay | WATERJET DRIVE DEVICE FOR DRIVING WATER VEHICLES |
US4578943A (en) * | 1984-11-19 | 1986-04-01 | Scampini Daniel C | Hydro-vapor free turbine engine |
FR2623161B1 (en) * | 1987-11-16 | 1990-04-06 | Moteur Moderne Le | VESSEL PROVIDED WITH AT LEAST ONE REACTION PROPELLER |
US4974539A (en) * | 1989-06-21 | 1990-12-04 | Fmc Corporation | Integrated propulsion and hydrofoil system |
JPH0464811A (en) * | 1990-07-03 | 1992-02-28 | Saamaru:Kk | Refuse incinerator |
US5598700A (en) * | 1994-06-30 | 1997-02-04 | Dimotech Ltd. | Underwater two phase ramjet engine |
US6161374A (en) * | 1999-11-01 | 2000-12-19 | Sverdlin; Anatoly | Transportation propulsion system |
US20110070782A1 (en) * | 2008-05-16 | 2011-03-24 | The Ohio State University | Marine propulsion system |
US8408155B2 (en) * | 2008-06-16 | 2013-04-02 | Juliet Marine Systems, Inc. | Fleet protection attack craft |
US9327811B2 (en) | 2008-06-16 | 2016-05-03 | Juliet Marine Systems, Inc. | High speed surface craft and submersible craft |
US8857365B2 (en) | 2008-06-16 | 2014-10-14 | Juliet Marine Systems, Inc. | Fleet protection attack craft and underwater vehicles |
AU2012236188B2 (en) | 2011-03-30 | 2016-10-20 | Juliet Marine Systems, Inc. | High speed surface craft and submersible vehicle |
GB2489521B (en) * | 2011-04-01 | 2013-05-08 | Rolls Royce Plc | A water jet propulsion device having fluid injection nozzles |
CN102251880A (en) * | 2011-06-02 | 2011-11-23 | 西北工业大学 | Underwater gas-liquid two-phase engine |
WO2014098962A1 (en) * | 2012-12-17 | 2014-06-26 | United Technologies Corporation | Two spool gas generator to create family of gas turbine engines |
CN106985991B (en) * | 2017-04-01 | 2018-11-13 | 徐斌 | A kind of type of respiration power plant peculiar to vessel |
RU2728937C1 (en) * | 2019-06-13 | 2020-08-03 | Петр Викторович Соловьёв | Method of using internal energy of thermal jet of air-jet engine |
WO2021164775A1 (en) * | 2020-02-21 | 2021-08-26 | 曾德润 | Ship propulsion method and structure device using air working medium for propulsion |
WO2023091052A1 (en) * | 2021-11-16 | 2023-05-25 | Liber Vladislav Yuryevich | Direct flow air-and-hydraulic propulsion unit |
Family Cites Families (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US2447100A (en) * | 1946-06-17 | 1948-08-17 | Edward A Stalker | Propulsion and boundary layer control for aircraft |
US3153905A (en) * | 1962-01-10 | 1964-10-27 | Robert J Sutherlin | Jet engine |
US3365891A (en) * | 1966-08-22 | 1968-01-30 | John M Peterson | Gas thrustor marine engine |
-
1972
- 1972-02-11 GB GB647572A patent/GB1413845A/en not_active Expired
-
1973
- 1973-02-05 US US00329334A patent/US3808804A/en not_active Expired - Lifetime
- 1973-02-09 FR FR7304630A patent/FR2171351B1/fr not_active Expired
- 1973-02-09 IT IT20242/73A patent/IT978983B/en active
- 1973-02-09 JP JP48016361A patent/JPS4919588A/ja active Pending
Also Published As
Publication number | Publication date |
---|---|
US3808804A (en) | 1974-05-07 |
DE2306513B2 (en) | 1975-05-22 |
FR2171351B1 (en) | 1977-08-19 |
DE2306513A1 (en) | 1973-08-23 |
IT978983B (en) | 1974-09-20 |
JPS4919588A (en) | 1974-02-21 |
FR2171351A1 (en) | 1973-09-21 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
GB1413845A (en) | Marine propulsion | |
GB1273673A (en) | Improvements relating to jet engines | |
GB1151177A (en) | Improvements in and relating to Gas Turbine Engines | |
GB1270434A (en) | Turbofan engines | |
JPS61197724A (en) | Gas turbine engine for turbo propella airplane | |
GB513751A (en) | Improvements in power plants for aircraft | |
GB795651A (en) | Improvements in or relating to aircraft power plant installations incorporating gas-turbine engines | |
JPS5756623A (en) | Acceleration time auxiliary device in internal combustion engine with exhaust gas turbine supercharger | |
FR2284040A1 (en) | Diesel engine turbocharger pressure control - injects compressor bleed air obliquely into drive turbine flow to increase speed | |
GB881967A (en) | Improved propulsion unit for use in vertical take-off aircraft | |
FR2389772A1 (en) | Jet engine for subsonic aircraft - has hollow rotor with internal blades to produce secondary stream of air within annular primary stream | |
SU1270389A1 (en) | Combination gas-turbine plant | |
RU2125659C1 (en) | Turboramjet engine | |
GB839925A (en) | Improvements in or relating to starting arrangements for gas turbine engines | |
GB672660A (en) | Improvements relating to internal combustion power plants | |
GB1473542A (en) | Mobile power units | |
GB919113A (en) | Improvements in or relating to aircraft propulsive means | |
GB784531A (en) | The combination of a helicoptor-supporting rotor and a two-stroke fuel-injection compression-ignition engine serving as a gas generator | |
GB992931A (en) | Gas turbine jet propulsion engine | |
GB862560A (en) | Improvements in or relating to the silencing of the exhaust jet from combustion engines | |
GB847868A (en) | Improvements relating to vertical take-off aircraft | |
SU144346A1 (en) | Turbodiesel | |
GB789800A (en) | Jet propelled aircraft | |
GB869587A (en) | Improvements in or relating to jet lift gas turbine engines | |
GB920253A (en) | Improvements in or relating to gas-turbine jet-propulsion engines |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed [section 19, patents act 1949] | ||
PLNP | Patent lapsed through nonpayment of renewal fees |