US1154609A - Method of increasing the energy of a fluid-motor in motor-driven torpedoes. - Google Patents
Method of increasing the energy of a fluid-motor in motor-driven torpedoes. Download PDFInfo
- Publication number
- US1154609A US1154609A US85221814A US1914852218A US1154609A US 1154609 A US1154609 A US 1154609A US 85221814 A US85221814 A US 85221814A US 1914852218 A US1914852218 A US 1914852218A US 1154609 A US1154609 A US 1154609A
- Authority
- US
- United States
- Prior art keywords
- motor
- energy
- fluid
- increasing
- driven
- 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 - Lifetime
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Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C6/00—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use
- F02C6/18—Plural gas-turbine plants; Combinations of gas-turbine plants with other apparatus; Adaptations of gas-turbine plants for special use using the waste heat of gas-turbine plants outside the plants themselves, e.g. gas-turbine power heat plants
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- 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
- Y02E—REDUCTION OF GREENHOUSE GAS [GHG] EMISSIONS, RELATED TO ENERGY GENERATION, TRANSMISSION OR DISTRIBUTION
- Y02E20/00—Combustion technologies with mitigation potential
- Y02E20/16—Combined cycle power plant [CCPP], or combined cycle gas turbine [CCGT]
Definitions
- a superheater In motor driven torpedoes operated by means of compressed air, a superheater is employed for increasing the energy available for the propulsion, and consequently increasing the speed and power of these engines.
- This superheater is inserted in the pipe which connects the air reservoir with the motor, and in it is ignited a preferably liquid combustible, such as petrol, spirit or the like, conveyed automatically under pressure.
- a combustible such as petrol, spirit or the like
- This invention has for its object a process which enables the quantity of gaseous fluid I released in the combustion chamber'to be increased in a certain proportion according to requirements, and which consequently allows the energy of the fluid motor to be notably increased.
- This process consists in injecting into the superheater, oxygenated water (hydrogen peroxid) of suitable strength (to be determmed for each particular case), which being vaporized will pro- Speciflcation of Letters Patent.
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- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Description
MICHEL BRUNIQUEL, OF PARIS, FRANCE.
METHOD OF INCREASING THE ENERGY OF A FLUID-MOTOR IN MOTOR-DRIVEN TORIEDOES.
No Drawing.
To all whom it may concern:
Be it known that I, MICHEL BRUNIQUEL, engineer, residing at 43 Rue de la Federation, Paris, in the Republic of France, have invented certain new and useful Improvements in Methods of Increasing the Energy of a Fluid-Motor in Motor-Driven Torpedoes; and I do hereby declare the following to be a full, clear, and exact description of the invention, such as will enable others skilled in the art to which it appertains to make and use the same.
In motor driven torpedoes operated by means of compressed air, a superheater is employed for increasing the energy available for the propulsion, and consequently increasing the speed and power of these engines. This superheater is inserted in the pipe which connects the air reservoir with the motor, and in it is ignited a preferably liquid combustible, such as petrol, spirit or the like, conveyed automatically under pressure. The energy produced by this combustion is added to that of the compressed air. This increase'of energy is limited by considerations of the strength of the constructional materials at high temperatures. Also in certain of these superheaters in order further to increase the available energy without reaching-too high temperatures, a portion of the heat evolved by the combustion of the liquid combustible or the like is employedfor vaporizing water conveyed also under pressure into the superheater.
This invention has for its object a process which enables the quantity of gaseous fluid I released in the combustion chamber'to be increased in a certain proportion according to requirements, and which consequently allows the energy of the fluid motor to be notably increased. This process consists in injecting into the superheater, oxygenated water (hydrogen peroxid) of suitable strength (to be determmed for each particular case), which being vaporized will pro- Speciflcation of Letters Patent.
Patented Sept. 28, 1915.
Application filed July 21, 1914. Serial No. 852,218.
duce oxygen and steam, while releasing a certain quantity of heat. The oxygen insures a more complete combustion of the combustible, and. if the strength is suitably selected will .enable a larger quantity of the latter to be burnt. For this reason the energy available in the motor will be increased in a proportion dependent on the strength of the hydrogen peroxid employed, more particularly by employinga peroxid, which is sufliciently rich in oxygen, air might be dispensed with and the mixture of peroxid and combustible burnt in a combustion motor. Further as the peroxid only solidifies at low temperatures, it has a great advantage over the ordinary water at present employed for torpedoes which are required to work in winter or in cold countries.
Having now particularly described and ascertained the nature of my said invention and in what manner the same is to be performed, I declare that what I claim is:
1. The process of increasing the energy supplied to a motor driven by compressed fluid which consists in subjecting such fluid while on its Way to the motor, to the heat of a suitable fuel in combustion while injecting hydrogen peroxid into the sphere of combustion.
2. The process of increasing the energy supplied to a motor driven by compressed fluid which consists in burning a'suitable fuel in such fluid while on its way to the motor, and simultaneously mingling hydrogen peroxid with the same, whereby the temperature is suitably controlled while a suitable proportion of oxygen is supplied to prevent resultant impairment of combustion.
In testimony whereof, I have afiixedmy signature, in presence of two witnesses.
MICHEL BRUNIQUEL.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US85221814A US1154609A (en) | 1914-07-21 | 1914-07-21 | Method of increasing the energy of a fluid-motor in motor-driven torpedoes. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US85221814A US1154609A (en) | 1914-07-21 | 1914-07-21 | Method of increasing the energy of a fluid-motor in motor-driven torpedoes. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1154609A true US1154609A (en) | 1915-09-28 |
Family
ID=3222673
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US85221814A Expired - Lifetime US1154609A (en) | 1914-07-21 | 1914-07-21 | Method of increasing the energy of a fluid-motor in motor-driven torpedoes. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1154609A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2631426A (en) * | 1948-07-07 | 1953-03-17 | Curtiss Wright Corp | Engine starting turbine having combustion element supplied thereto in response to speed and combustion chamber pressure |
| US2746249A (en) * | 1936-09-14 | 1956-05-22 | Francis R Bichowsky | Spaced wall combustion apparatus |
| US2775961A (en) * | 1954-10-22 | 1957-01-01 | Fairchild Engine & Airplane | Fuel supply system |
| US2862482A (en) * | 1949-09-07 | 1958-12-02 | Hart David Kennedy | Internal combustion engine |
| US2992638A (en) * | 1953-04-01 | 1961-07-18 | Fmc Corp | Internal combustion engine and method of operating same |
-
1914
- 1914-07-21 US US85221814A patent/US1154609A/en not_active Expired - Lifetime
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2746249A (en) * | 1936-09-14 | 1956-05-22 | Francis R Bichowsky | Spaced wall combustion apparatus |
| US2631426A (en) * | 1948-07-07 | 1953-03-17 | Curtiss Wright Corp | Engine starting turbine having combustion element supplied thereto in response to speed and combustion chamber pressure |
| US2862482A (en) * | 1949-09-07 | 1958-12-02 | Hart David Kennedy | Internal combustion engine |
| US2992638A (en) * | 1953-04-01 | 1961-07-18 | Fmc Corp | Internal combustion engine and method of operating same |
| US2775961A (en) * | 1954-10-22 | 1957-01-01 | Fairchild Engine & Airplane | Fuel supply system |
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