GB578263A - Improvements in or relating to jet propulsion apparatus - Google Patents
Improvements in or relating to jet propulsion apparatusInfo
- Publication number
- GB578263A GB578263A GB1440541A GB1440541A GB578263A GB 578263 A GB578263 A GB 578263A GB 1440541 A GB1440541 A GB 1440541A GB 1440541 A GB1440541 A GB 1440541A GB 578263 A GB578263 A GB 578263A
- Authority
- GB
- United Kingdom
- Prior art keywords
- combustion chamber
- supplied
- jet propulsion
- fuel
- combustion
- 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
-
- 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
- F02K9/60—Constructional parts; Details not otherwise provided for
- F02K9/62—Combustion or thrust chambers
- F02K9/64—Combustion or thrust chambers having cooling arrangements
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Liquid Carbonaceous Fuels (AREA)
Abstract
578,263. Jet propulsion apparatus. ASIATIC PETROLEUM CO., Ltd., LUBBOCK, I., and GOLLIN, G. J. Nov. 7, 1941, No. 14405. [Class 114] In apparatus for effecting jet propulsion by the products of the combustion of a liquid fuel and a liquid oxidant in a combustion chamber, water or other liquid diluent is introduced into the combustion chamber so as to reduce the temperature of combustion. In the form shown, the fuel and oxidant are supplied to a combustion chamber 1 by a nozzle 4, and the water &c. is supplied at 8 to a cooling-coil 7 surrounding the expansion nozzle 6, and then by a pipe 9 to one or more jets 10. The nozzle 4 may be constructed and surrounded by a cooling-chamber 5, as described in Specification 578,293, [Group XXVII], and the water &c. supplied to the chamber 5 may also have access to the combustion chamber. The liquids may be supplied by the pressure of a propellant gas as described in Specification 578,262, and the combustion chamber 1 has a refractory lining 2 which may be subdivided into rings as described in- Specification 578,007, [Group XII]. The liquid diluent may be emulsified with the liquid fuel, the emulsified fuel being then used as the cooling-medium.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1440541A GB578263A (en) | 1941-11-07 | 1941-11-07 | Improvements in or relating to jet propulsion apparatus |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1440541A GB578263A (en) | 1941-11-07 | 1941-11-07 | Improvements in or relating to jet propulsion apparatus |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB578263A true GB578263A (en) | 1946-06-21 |
Family
ID=10040619
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1440541A Expired GB578263A (en) | 1941-11-07 | 1941-11-07 | Improvements in or relating to jet propulsion apparatus |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB578263A (en) |
Cited By (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1164753B (en) * | 1959-12-12 | 1964-03-05 | Boelkow Entwicklungen Kg | Rocket engine for liquid fuels |
| US3313488A (en) * | 1964-10-02 | 1967-04-11 | Thiokol Chemical Corp | Rocket thrust chamber |
| GB2272025A (en) * | 1992-10-28 | 1994-05-04 | Snecma | Air heating system for turbojet bypass engines. |
| WO2010042095A2 (en) * | 2007-07-24 | 2010-04-15 | Thomas Clayton Pavia | Systems, methods and apparatus for propulsion |
-
1941
- 1941-11-07 GB GB1440541A patent/GB578263A/en not_active Expired
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| DE1164753B (en) * | 1959-12-12 | 1964-03-05 | Boelkow Entwicklungen Kg | Rocket engine for liquid fuels |
| US3313488A (en) * | 1964-10-02 | 1967-04-11 | Thiokol Chemical Corp | Rocket thrust chamber |
| GB2272025A (en) * | 1992-10-28 | 1994-05-04 | Snecma | Air heating system for turbojet bypass engines. |
| WO2010042095A2 (en) * | 2007-07-24 | 2010-04-15 | Thomas Clayton Pavia | Systems, methods and apparatus for propulsion |
| WO2010042095A3 (en) * | 2007-07-24 | 2015-01-08 | Thomas Clayton Pavia | Method of cooling a rocket engine and rocket engine |
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