GB861735A - Improvements in or relating to mono-fuel self contained power unit - Google Patents
Improvements in or relating to mono-fuel self contained power unitInfo
- Publication number
- GB861735A GB861735A GB17701/57A GB1770157A GB861735A GB 861735 A GB861735 A GB 861735A GB 17701/57 A GB17701/57 A GB 17701/57A GB 1770157 A GB1770157 A GB 1770157A GB 861735 A GB861735 A GB 861735A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- pipe
- fuel
- exhaust gases
- duct
- 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
- 239000000446 fuel Substances 0.000 title abstract 6
- 239000007789 gas Substances 0.000 abstract 10
- 238000002485 combustion reaction Methods 0.000 abstract 3
- 230000003068 static effect Effects 0.000 abstract 2
- 238000001816 cooling Methods 0.000 abstract 1
- 238000000354 decomposition reaction Methods 0.000 abstract 1
- 239000002828 fuel tank Substances 0.000 abstract 1
- 238000011144 upstream manufacturing Methods 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
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/42—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
- F02K9/44—Feeding propellants
-
- 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
- B64D37/00—Arrangements in connection with fuel supply for power plant
- B64D37/02—Tanks
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/28—Continuous combustion chambers using liquid or gaseous fuel characterised by the fuel supply
-
- 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
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T90/00—Enabling technologies or technologies with a potential or indirect contribution to GHG emissions mitigation
- Y02T90/40—Application of hydrogen technology to transportation, e.g. using fuel cells
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
861,735. Combustion product plant. PLESSEY CO. Ltd. June 4, 1958, [June 4, 1957], No. 17701/57. Class 7(1). [Also in Group XXVI] A mono fuel power unit comprises a fuel tank container 1 which is divided into two chambers 3 and 2 by means of a flexible diaphragm 4 or a piston, monofuel contained in the chamber 3 being expelled therefrom by means of gas under pressure supplied to the chamber 2, the gas being tapped from the exhaust gases of the prime mover 13 which in the embodiment shown is a gas turbine. Fuel is supplied from the monofuel chamber 3 through duct 5 to fuel pump 6, thence to control valve 8 and combustion or decomposition chamber 11. The control valve 8 which may be as described in Specification 861,734 is also connected to the fuel chamber 3 by means of duct 9. Combustion products from the chamber 11 pass to the turbine 13 and exhaust gases therefrom discharge through the duct 14. The pressure of the exhaust gases is tapped off from the duct 14 and applied to the chamber 2 through the pipe 16. The inlet to the pipe 16 may be directed upstream so that the kinetic and static pressure of the gases is utilized or the inlet may be parallel to the flow of gases so that the static pressure only is utilized. A restriction 19 is disposed in the exhaust pipe so as to ensure a sufficiently high pressure of the exhaust gases. The fuel pump 6 is driven by the turbine 13 through connection 18. The exhaust gases passing through pipe 16 may be cooled for example by means of cooling fins or by making the pipe of considerable length.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB17701/57A GB861735A (en) | 1957-06-04 | 1957-06-04 | Improvements in or relating to mono-fuel self contained power unit |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB17701/57A GB861735A (en) | 1957-06-04 | 1957-06-04 | Improvements in or relating to mono-fuel self contained power unit |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB861735A true GB861735A (en) | 1961-02-22 |
Family
ID=10099696
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB17701/57A Expired GB861735A (en) | 1957-06-04 | 1957-06-04 | Improvements in or relating to mono-fuel self contained power unit |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB861735A (en) |
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3722217A (en) * | 1971-03-03 | 1973-03-27 | Sundstrand Corp | Auxiliary hydraulic power supply |
| WO2009136389A1 (en) * | 2008-05-05 | 2009-11-12 | Joshua Waldhorn | Turbine driven by predetermined deflagration of anaerobic fuel and method thereof |
-
1957
- 1957-06-04 GB GB17701/57A patent/GB861735A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3722217A (en) * | 1971-03-03 | 1973-03-27 | Sundstrand Corp | Auxiliary hydraulic power supply |
| WO2009136389A1 (en) * | 2008-05-05 | 2009-11-12 | Joshua Waldhorn | Turbine driven by predetermined deflagration of anaerobic fuel and method thereof |
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