GB572876A - Improvements in or relating to fluid reaction apparatus for propelling purposes - Google Patents
Improvements in or relating to fluid reaction apparatus for propelling purposesInfo
- Publication number
- GB572876A GB572876A GB1428243A GB1428243A GB572876A GB 572876 A GB572876 A GB 572876A GB 1428243 A GB1428243 A GB 1428243A GB 1428243 A GB1428243 A GB 1428243A GB 572876 A GB572876 A GB 572876A
- Authority
- GB
- United Kingdom
- Prior art keywords
- tube
- combustion chamber
- air
- valve
- fuel
- 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
- 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
- F02K7/02—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 the jet being intermittent, i.e. pulse-jet
Abstract
572,876. Jet propulsion of aircraft &c. STARK, F. H. Sept. 1, 1943, No. 14282. [Class 51 (i)] [Also in Group XXXIII] The jet propulsion of vehicles, ships and aircraft is effected by causing a column of fluid to be driven from the open end of a discharge tube at a velocity sufficient for it to set up a reactive effect for driving the vehicle &c. and in addition to set up a depression below atmospheric pressure in a combustion chamber at the other end of the tube so that after discharge of such column from the tube the ambient fluid is able to enter and set up a column of fluid moving through the tube in the reverse' direction and by its momentum exerting sufficient pressure for compressing a charge of air and fuel admitted for combustion into the combustion chamber. In the apparatus shown in Figs. 1 and 1a, fuel is sprayed into a combustion chamber 2 and ignited by a sparking plug 8. The explosion causes a column of gases to pass along the tube 1 to the open end la and also to cause a depression in the combustion chamber, whereupon a valve 3 opens against the action of a spring 5 and admits a mixture of fuel and air from a carburetter 6, 7 to the combustion chamber 2. The amount of mixture admitted to the combustion chamber is insufficient to restore atmospheric pressure so that a column of air from the atmosphere returns through the tube and compresses the charge and also closes the valve 3. The charge is ignited by the electric contacts 12 being closed by the motion of the rocker arm 4 of the valve 3. The exterior of the tube 1 may be cooled by an air or water jacket and where, as shown, an air jacket is employed, the tube 1 may be provided with fins 21. The interior of the tube may also be provided with partitions 20. Gases may be withdrawn from the tube 1 through a valve 23 and pipe 22 and used for auxiliary purposes. The combustion chamber 2 may be provided with an auxiliary air inlet 11. The valve 3 may be operated by a cam and instead of lift valve 3, sliding piston or reed valves may be used for the admission of air, fuel being injected into the combustion chamber under pressure. Two or more combustion chambers may discharge into a single tube 1 or a number of tubes 1 may receive the gases from a single combustion chamber. In the modification shown in Fig. 6, one or more annular ducts 50 are disposed along the tube 1 and supplied with fuel and air.from a carburetter 60, the inlet port 51 being controlled by a sleeve valve 52. Correction for atmospheric pressure and temperature may be provided by providing a duct 71 in communication with the air jacket 15 and a thermometer 70 arranged in the air jacket and connected to capsules 73, 72 adapted to influence the disc 74 of a governor 75 connected to the throttle lever 79. A number of propulsion units for aircraft may be grouped in a circle or arranged in a row ; in the latter case, the units may be mounted on the wing of an aeroplane. When the propulsion units are applied to marine vessels, the open ends of the tubes may be situated beneath the surface of the water in which the vessel is floated, in which case the water would be the ambient medium. Reference has been directed by the Comptroller to Specification 176,838, [Class 51 (i)].
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1428243A GB572876A (en) | 1943-09-01 | 1943-09-01 | Improvements in or relating to fluid reaction apparatus for propelling purposes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1428243A GB572876A (en) | 1943-09-01 | 1943-09-01 | Improvements in or relating to fluid reaction apparatus for propelling purposes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB572876A true GB572876A (en) | 1945-10-26 |
Family
ID=10038338
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1428243A Expired GB572876A (en) | 1943-09-01 | 1943-09-01 | Improvements in or relating to fluid reaction apparatus for propelling purposes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB572876A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE968328C (en) * | 1952-04-13 | 1958-02-06 | Schmidt Paul | Jet engine with intermittent combustion of fuel in air by shock wave ignition |
DE1045732B (en) * | 1952-12-19 | 1958-12-04 | Schmidt Paul | Device for generating thermal and mechanical energy by intermittently repeated combustion of ignitable mixture |
FR2853938A1 (en) * | 2003-04-17 | 2004-10-22 | Noel Gil | Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor |
-
1943
- 1943-09-01 GB GB1428243A patent/GB572876A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE968328C (en) * | 1952-04-13 | 1958-02-06 | Schmidt Paul | Jet engine with intermittent combustion of fuel in air by shock wave ignition |
DE1045732B (en) * | 1952-12-19 | 1958-12-04 | Schmidt Paul | Device for generating thermal and mechanical energy by intermittently repeated combustion of ignitable mixture |
FR2853938A1 (en) * | 2003-04-17 | 2004-10-22 | Noel Gil | Reactor has auxiliary engine turning electricity generator and compressor, and cam shaft opening or closing valve for providing multiple ram effects in second, where ram effects increase final force of reactor |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
US2427845A (en) | Periodically actuated jet motor | |
US1369672A (en) | Propelling device | |
GB669008A (en) | Improvements relating to jet-propelled missiles | |
US3133413A (en) | Control and cooling of rocket motors | |
GB716879A (en) | Improvements in or relating to outboard marine engines | |
GB572876A (en) | Improvements in or relating to fluid reaction apparatus for propelling purposes | |
US3230701A (en) | Two step reaction propulsion method | |
GB548898A (en) | Improvements in or relating to the propulsion of aircraft and other vehicles | |
US2397654A (en) | Propulsion means | |
US2799988A (en) | Catapult device | |
US2425121A (en) | Combustion jet propulsioned means | |
US2850872A (en) | Pulse jet convertible to ram jet engine | |
US3420053A (en) | Aircraft launching thrust augmentation system | |
US3112613A (en) | Positive power jet engine | |
US2609168A (en) | Jet airfoil brake | |
GB1201526A (en) | Gas turbine power units | |
GB710412A (en) | Means for controlling the speed of ram jet-propelled air craft, missiles or other aerial bodies | |
GB670933A (en) | Improvements in or relating to devices for increasing the maximum speed of vehicles or craft driven by internal combustion engines | |
GB698588A (en) | Improvements in or relating to the impulse driving of water vehicles | |
GB946739A (en) | Jet propulsion engine for water craft | |
GB2147052A (en) | Additional propellant for rocket | |
GB844528A (en) | Improvements in or relating to ignition devices for propulsion engines of the continuous internal combustion type | |
GB706924A (en) | Improvements in or relating to aircraft | |
Lent | Spear Shaped Weather Rocket: Annular Nozzle Feature of Design | |
US1627154A (en) | Automobile torpedo |