US820238A - Explosion-turbine. - Google Patents

Explosion-turbine. Download PDF

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US820238A
US820238A US25052305A US1905250523A US820238A US 820238 A US820238 A US 820238A US 25052305 A US25052305 A US 25052305A US 1905250523 A US1905250523 A US 1905250523A US 820238 A US820238 A US 820238A
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explosion
turbine
piston
cylinder
chamber
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Augustus L Moss
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    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02CGAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
    • F02C5/00Gas-turbine plants characterised by the working fluid being generated by intermittent combustion
    • F02C5/12Gas-turbine plants characterised by the working fluid being generated by intermittent combustion the combustion chambers having inlet or outlet valves, e.g. Holzwarth gas-turbine plants

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  • Figure 1 is a side elevation of the improvement.
  • Fig. 2 is a sectional side elevation of the mechanism for actuating the controllingvalves in the nozzles of the explosion-chambers.
  • Fig. 3 is a sectional side elevation of,
  • Fig.- 4 is a plan view of one of the explosion devices.
  • Fig. 5 is an enlarged cross-section of the improvement on the line 5 5 of Fig. 1.
  • Fig. 6 is a sectional side elevation of part of the improvement, showing one of the explosion devices in an exhausting position;
  • Fig, 7 is a cross-section of the improvement on the line 7 7 of Fig. 3, illustrating one of the exhausts; and
  • Fig. 8 is a diagrammatic view of the igniting devices.
  • a turbine-cylinder B On a suitablyconstructed frame A is mounted a turbine-cylinder B, in which is arranged to rotate a turbine-wheel C, having peripheral'buckets C and secured on a shaft D, jo urnaled in suitable bearings held on standards A, forming part of the main frame A.
  • a turbine-cylinder B Around the turbine-cylinder B are grouped a plurality of spaced explosioncylinders E, E, E and E 'for giving impact impulses in quick succession to the turbinewheel C at different dpoints of its periphery to insure a uniform an powerful running of the turbine.
  • Each of the explosion-cylinders E, E, E and E consists, essentially, of an explosionchamber F, secured to or forming part of the turbine-cylinder B and being preferably in the form of a cylinder, the axis of which is disposed radially to the axis of the turbine wheel O. From the inner end of the explosion-chambcr F extends a nozzle G for discharging the exploded charge against the buckets C of the turbine-wheel O to rotate the latter in the direction of the arroiv a, and in the nozzleGis arranged a valve H for opening and closing the nozzle G at the proper time and as hereinafter more fully described.
  • explosion-chamber F is mounted to reciprocate a piston 1, controlled from the turbine-wheel O and serving to draw in theexplosive charge and to compress the same previous to igniting the charge, as hereinafter more-fully explained.
  • Adjacent to the inner end of the explosion chamber F are arranged ages-chamber J and an air-chamber J, of which the chamber J is connected by a pipe J 2 with a suitable gassupply, while the other chamber J is provided with an airinlet pipe J
  • the chambers J and J are connected with the inner end of the explosion-chamber F by spring-pressed valves K and K, respectively, adapted to open inwardly on the piston 1 moving outwardly during the suction-stroke and during the time the pistonLis at the end of its inward strokeand after the explosion has taken place (see Fig. 6) to allow air and gas to rush into the inner end of the explosion-chamber to clean the latter of the products of combustion, sufficient suction being produced in the inner end of the cylinder by the action of the rotating turbine-wheel O.
  • an electric igniting device L for igniting the compressed charge at the proper time, and atthe same time the valve H moves suddenly into an open position.
  • a cross-head P On the outer end of the piston-rod I of the piston I is secured a cross-head P, from which extend rods 1 mounted to slide in suitable bearings and provided at their inner ends with friction-rollers I, engaging the eccentric camrooves of cams 1", secured to the main shaft D on opposite sides of the cylinder B, as plainly illustrated in Fig. 5.
  • the cams I rotate with the shaft D, and consequently impart a sliding motion to the rods 1 and to cause the cross-heads I and piston-rods I to impart.
  • valve H in the nozzle G of each explosion-cylinder E, E, E and E is preferably in the form of a cylindrical rocking valve, and in order to open and close the said valvein unison with the movement of the corresponding piston I the following device is provided: On the outer end of the stem H of the valve H is secured an arm H pulled on at one end by a spring H and pivotally connected at its other end by a link H with a rod H mounted to slide radially in suitable bearings and abutting with its inner end on the peripheral face of a cam H, secured on the main shaft D.
  • the cam H is provided with an abrupt portion H so that whenthe turbine isrunning and the shaft D and cam H turn in the direction of the arrow 0/ then the abrupt portion H comes successively opposite the inner ends of the rods H to allow the latter to slide suddenly inwardly, owing to the action of the springs H to turn the valve H from a nor- This action takes place at the time the piston I is in its locked position near the innermost end ofthe cylinder immediately before the explosion of the charge has taken lace in the explosion-chamber F.
  • the valve H is open and the exploded c arge passes through the nozzle G against the buckets O of the turbine-wheel C to rotate the latter in the direction of the arrow a.
  • the valve H remains 0 en after the explosion has taken place an during the time the piston I changes from near the end of its downstroke to the beginning of its upstroke, so that the buckets C, passing the terminal of the nozzle F, cause a suction in the inner end of the explosion-chamber F for the valves K and K to open.
  • the inrushing gas and air completely clears the inner end of the chamber F of the products of combustion, which rush through the open valve H and nozzle G into the turbine-cylinder B.
  • the valve H immediately closes and remains closed until the next explosion is to take place.
  • the products'of combustion which pass by Way of the nozzle G into the cylinder. B finally reach exhaust-chambers B, formed in the cylinder between adjacentexplosion devices, the beginning of a chamber B being a distance from the terminal of the preceding nozzle G, as will be readily understood by reference to Fi 3.
  • the products of combustion can pass from the chambers B to ports a in the hub of the turbine-wheel C and the shaft D into the hollow ortion D of the shaft, (see Fig. 5,) and this ollow portion is provided near its outer end with ports 6, opening into a chamber P, surroundin the shaft D, and having an exhaust-pipe I for carrying off the products of combustion to a suitable place.
  • the chambers B extend around the rim of the Wheel C to allow the gases to reach the ports a.
  • Each ignition device L is provided with spaced electrodes L and L connected by wires L and L with an induction-coil L connected with a suitable source of electrical energy 0, such as a battery, as indicated in Fig. 8.
  • the circuit-breaker Q for each induction-coil L consists of flexible contactplates Q and Q of which the contact-plate Q is connected by a wire Q with the induction-coil L and the other contact-plate is connected by a wire Q with an armature-lever for the induction-coil L Normally the contact-plates Q and Q are in an 0 en position, and one of the contact-p ates-as shown, the contact-plate Qis adapted to be engaged by an arm Q attached to one of the rods I preferably at the cam N so that when the piston I moves into an innermost osition the arm Q presses the contactlate a and moves the same in contact wit the other plate Q to close the circuit, thus causing the induction-coil L to send a current through the wires L and L
  • the explosion-chambers F of the several explosioncylinders E, E, E and E are preferably water-jacketed, as indicated in the drawings, and the cylinder B is likewise preferably water-jacketed to keep the turbine at the proper temp ature.
  • An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a disagainst the buckets in the direction of rotaplosion period.
  • An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a discharge-nozzle for discharging a motive agent against the buckets in the direction of rotation of the turbine-wheel, a piston in the explosion-chamber controlled from said turbinewheel for drawing in an explosive charge and for compressing the same previous to ignition, a valve in said nozzle for opening and closing the latter, and means operated by the piston-operating means for locking the piston during the explosion period.
  • An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a discharge-nozzle for discharging a motive agent against the buckets in the direction of rotation of the turbine-Wheel, a piston in the explosion chamber controlled from said turbine-wheel for drawing in an explosive charge and for compressing the same previous to ignition, means operated by the piston-operating means for locking the piston during the explosion period, and a valve operating in conjunction with said piston and opening qui kly at the end of the compression period of said piston.
  • An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a discharge-nozzle for discharging a motive agent against the buckets in the direction of rotation of the turbine-wheel, a piston in the explosion-chamber controlled from said turbine-wneel for drawing in an explosive charge and for compressing the same previous to ignition, means operated by the piston-operating means for locking the piston during the explosion period, and a valve operating in conjunction with the said piston and opening quickly at the end of the compression period of said piston and remaining open until after the beginning of the return stroke of the piston whereby the turbine-wheel may create a suction in the said working chamber to clear the same of the products of combustion.
  • An explosion-turbine comprising a cylinder, a turbine wheel having peripheral buckets and arranged to turn in said cylinder, an explosion-chamber having a nozzle for discharging a motive agent against the buckcharge-nozzle for discharging amotive agent l ets of the turbine-wheel, a piston reciprocating in the said explosion-chamber and controlled from said il'LlIblllQJVllGQl, means for supplying said explosion-011amber with an explosive charge, an ignition device for ignitmg the said explosive charges, means operinder, a turbine-wheel having buckets and mounted to turn in said cylinder, an explos1on-chamber having a nozzle for discharging a motive agent against the buckets of the turi bine-whecl, a piston reciprocating in the said explosion-chamber and controlled irom the said turbine-wheel, means for supplying the said explosion-chamber with an explosive charge, a valve mthe said nozzle and operat ing in unison with
  • An explosion-turbine comprising a cylinder, a turbine wheel having peripheral buckets mounted to turn in the said cylinder, a plurality of explosion-cylinders spaced apart from each other and grouped around the said cylinder, each explosion-cylinder comprising aneXplosion-chamber having a nozzle for discharging an explosive charge against said buckets means for supplying an explosive charge to said explosion-chamber,
  • a reciprocating piston in the explosion-chamber for drawing in an explosive charge and for compressing the same immediately previous to the ignition of the charge by said igniting device, means connected with the turbine-wheel for operating the piston, and means operated by the piston-operating means for locking the piston during the explosion period.
  • An explosion-turbine comprising a cylinder, a turbine-wheel having peripheral buckets mounted to turn in the said cylinder a plurality of explosion cylinders spaced I i i E a l i l I l l l l I g i J 1' apart from each other and grouped around said cylinder, each explosion-cylinder comprising an explosion-chamber and having a nozzle for discharging an explosive charge against the said buckets, means for supplyingan explosive charge to said explosionchamber, an igniting device in the explosionchamber, a reciprocating piston in the said explosion-chamber for drawing in a charge and compressing the same immediately previous to the ignition of the charge by said igniting device, means connected with the turbine-whecl for operating the piston; means operated by the piston-operating means for locking the, piston during the explosion period, and an automatic valve in said discharge-nozzle.
  • An explosion-turbine comprising a cylinder, a turbine wheel having peripheral buckets and mounted to turn in the cylinder, a plurality of explosion cylinders spaced apart from each other and grouped around the cylinder, each explosion-cylinder comprising an explosion-chamber having a nozzle for discharging an explosive charge against said buckets, means for supplying the explosive charge to said explosion-chamber, an igniting device in the explosion-chamber, a reciprocating piston in the said explosionchamber for drawing in a charge and compressing the same immediately previous to the ignition of the charge by said igniting device, means for locking the piston against movement during the explosion period, an automatic valve in said discharge-nozzle, means for operating the said piston, and the said valve in unison from the turbine-wheel,

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  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Description

No. 820,238. PATENTED MAY 8, 1906 A. L. MOSS.
EXPLOSION TURBINE.
APPLICATION FILED MAlLlT. 1005.
4 $HBETS- SHEET 1 No. 820,238. PATENTED MAY 8, 1906.
A. L. MOSS.
EXPLOSION TURBINE.
APPLICATION FILED MAE.17. 1905.
4 SHEETS-SHEET 3.
WITNESSES. INVENTOR g y uszusllyfioss I ATTOFNEV I PATENTED MAY 8, 1906.
A. L. MOSS. EXPLOSION TURBINE. ATPLIOATION FILED MAR. 17. 1905.
4 SHEETSSHEET 4.
INVENTOR vfzyusZusL Mass wx 'A/ESSES UNITED sTAgEs "iPA r NT OFFIGE.
AUGUSTUS L. nose, or sANEtrsKY, oino.
EXPLOSlON-TURBiNE.
Specification of Letters Patent.
Application filed March 17,1905. Serial No. 250,523.
new and improved explosion-whine in which impact impulses are given in quick succession to the turbine-wheel at different points of its periphery to insure a uniform and powerful running of the turbine.
The invention consists of novel features and parts and combinations of the same, as will be more fully described hereinafter and then pointed out in the claims.
A'practical embodiment of the invention is represented in the accompanying drawings, forming a part of this specification, in which similar characters of reference indicate corresponding parts in all the views.
Figure 1 is a side elevation of the improvement. Fig. 2 is a sectional side elevation of the mechanism for actuating the controllingvalves in the nozzles of the explosion-chambers. Fig. 3 is a sectional side elevation of,
the improvement. Fig.- 4 is a plan view of one of the explosion devices. Fig. 5 is an enlarged cross-section of the improvement on the line 5 5 of Fig. 1. Fig. 6 is a sectional side elevation of part of the improvement, showing one of the explosion devices in an exhausting position; Fig, 7 is a cross-section of the improvement on the line 7 7 of Fig. 3, illustrating one of the exhausts; and Fig. 8 is a diagrammatic view of the igniting devices.
On a suitablyconstructed frame A is mounted a turbine-cylinder B, in which is arranged to rotate a turbine-wheel C, having peripheral'buckets C and secured on a shaft D, jo urnaled in suitable bearings held on standards A, forming part of the main frame A. Around the turbine-cylinder B are grouped a plurality of spaced explosioncylinders E, E, E and E 'for giving impact impulses in quick succession to the turbinewheel C at different dpoints of its periphery to insure a uniform an powerful running of the turbine.
Each of the explosion-cylinders E, E, E and E consists, essentially, of an explosionchamber F, secured to or forming part of the turbine-cylinder B and being preferably in the form of a cylinder, the axis of which is disposed radially to the axis of the turbine wheel O. From the inner end of the explosion-chambcr F extends a nozzle G for discharging the exploded charge against the buckets C of the turbine-wheel O to rotate the latter in the direction of the arroiv a, and in the nozzleGis arranged a valve H for opening and closing the nozzle G at the proper time and as hereinafter more fully described.
In the explosion-chamber F is mounted to reciprocate a piston 1, controlled from the turbine-wheel O and serving to draw in theexplosive charge and to compress the same previous to igniting the charge, as hereinafter more-fully explained.
Adjacent to the inner end of the explosion chamber F are arranged ages-chamber J and an air-chamber J, of which the chamber J is connected by a pipe J 2 with a suitable gassupply, while the other chamber J is provided with an airinlet pipe J The chambers J and J are connected with the inner end of the explosion-chamber F by spring-pressed valves K and K, respectively, adapted to open inwardly on the piston 1 moving outwardly during the suction-stroke and during the time the pistonLis at the end of its inward strokeand after the explosion has taken place (see Fig. 6) to allow air and gas to rush into the inner end of the explosion-chamber to clean the latter of the products of combustion, sufficient suction being produced in the inner end of the cylinder by the action of the rotating turbine-wheel O.
In the inner end of the explosion-chamber F is arranged an electric igniting device L for igniting the compressed charge at the proper time, and atthe same time the valve H moves suddenly into an open position.
In order to reciprocate the piston I in the cylinder F, the following device is provided: On the outer end of the piston-rod I of the piston I is secured a cross-head P, from which extend rods 1 mounted to slide in suitable bearings and provided at their inner ends with friction-rollers I, engaging the eccentric camrooves of cams 1", secured to the main shaft D on opposite sides of the cylinder B, as plainly illustrated in Fig. 5. When the turbine-wheel O is rotating, then the cams I rotate with the shaft D, and consequently impart a sliding motion to the rods 1 and to cause the cross-heads I and piston-rods I to impart. a reciprocating motion to the pistons I in the explosion-chambers F of the several cylinders E, E, E and E As the pistons I Patented May 8, 1906.
' mally closed into an open position.
of the several cylinders E, E, E and E are actuated from the same cams, it is evident that the pistons I are actuated in the proper succession to cause successive compression of the charges in the several explosion-chambers previous to their ignition. During the time the ignition takes place in cylinders E, E, E or E the corresponding piston I is automatically locked against movement, and for this purpose the following arrangement is made: The cross-head I for each piston I is adapted to be engaged by a locking-catch N, secured on a shaft N, journaled in suitable bearings on the outer end of the explosion-chamber F, and the said catch N is normally held out of the path of the cross-head I by a spring N On the'shaft N is secured a crank-arm N adapted to be engaged by a cam N fixed on one of the rods 1 so that'when the piston I moves inward and about reaches the end of its inward stroke then the cam N acts on the crank-arm N to impart a swinging motion to the shaft N and to the catch N to engage the latter with a cross-head I to hold the latter, andconsequently the piston I, against return movement. When the piston I is on the return or o utward stroke, the cam N moves out of engagement with the crank-arm N thus releasing the shaft N and the catch N, which latter is immediately pulled back into an inactive position by its spring N The latch N holds the piston I temporarily against outward movement, so that the force of the explosion is taken up by the latch and not by the cam I and shaft D. The valve H in the nozzle G of each explosion-cylinder E, E, E and E is preferably in the form of a cylindrical rocking valve, and in order to open and close the said valvein unison with the movement of the corresponding piston I the following device is provided: On the outer end of the stem H of the valve H is secured an arm H pulled on at one end by a spring H and pivotally connected at its other end by a link H with a rod H mounted to slide radially in suitable bearings and abutting with its inner end on the peripheral face of a cam H, secured on the main shaft D. The cam H is provided with an abrupt portion H so that whenthe turbine isrunning and the shaft D and cam H turn in the direction of the arrow 0/ then the abrupt portion H comes successively opposite the inner ends of the rods H to allow the latter to slide suddenly inwardly, owing to the action of the springs H to turn the valve H from a nor- This action takes place at the time the piston I is in its locked position near the innermost end ofthe cylinder immediately before the explosion of the charge has taken lace in the explosion-chamber F. Thus w en the explosion takes place the valve H is open and the exploded c arge passes through the nozzle G against the buckets O of the turbine-wheel C to rotate the latter in the direction of the arrow a. The valve H remains 0 en after the explosion has taken place an during the time the piston I changes from near the end of its downstroke to the beginning of its upstroke, so that the buckets C, passing the terminal of the nozzle F, cause a suction in the inner end of the explosion-chamber F for the valves K and K to open. When this takes place, the inrushing gas and air completely clears the inner end of the chamber F of the products of combustion, which rush through the open valve H and nozzle G into the turbine-cylinder B. As soon as the inner end of the ex losion-chamber is cleared of the products 0 combustion the valve H immediately closes and remains closed until the next explosion is to take place. The products'of combustion which pass by Way of the nozzle G into the cylinder. B finally reach exhaust-chambers B, formed in the cylinder between adjacentexplosion devices, the beginning of a chamber B being a distance from the terminal of the preceding nozzle G, as will be readily understood by reference to Fi 3.
The products of combustion can pass from the chambers B to ports a in the hub of the turbine-wheel C and the shaft D into the hollow ortion D of the shaft, (see Fig. 5,) and this ollow portion is provided near its outer end with ports 6, opening into a chamber P, surroundin the shaft D, and having an exhaust-pipe I for carrying off the products of combustion to a suitable place. The chambers B extend around the rim of the Wheel C to allow the gases to reach the ports a.
Each ignition device L is provided with spaced electrodes L and L connected by wires L and L with an induction-coil L connected with a suitable source of electrical energy 0, such as a battery, as indicated in Fig. 8. The circuit-breaker Q for each induction-coil L consists of flexible contactplates Q and Q of which the contact-plate Q is connected by a wire Q with the induction-coil L and the other contact-plate is connected by a wire Q with an armature-lever for the induction-coil L Normally the contact-plates Q and Q are in an 0 en position, and one of the contact-p ates-as shown, the contact-plate Qis adapted to be engaged by an arm Q attached to one of the rods I preferably at the cam N so that when the piston I moves into an innermost osition the arm Q presses the contactlate a and moves the same in contact wit the other plate Q to close the circuit, thus causing the induction-coil L to send a current through the wires L and L and the electrodes L and L ,With a spark passing from one electrode L to the other electrode L Thus it will be seen that when the piston I is moved into an innermost position and compresses the previously drawn-in charge the IIC saaass explosive charge is ignited by the spark referred to, and the force of the explosive charge is exerted against the buckets C, as previously ex lained, to rotate the turbine-wheel C in the irection of the arrow a I do not limit myself to the particular arrangement of. igniting devices above described, as the same may be varied without deviating from the spirit of my invention.
The operation is as follows: When the machine is running and the several parts are in the position illustrated in Fig. 5:, then an explosion has taken place in the explosion-cylinder E to turn the turbine-wheel C in the direction of the arrow a, while in the explosion-cylinder E the piston I is moving inward to compress the previously drawn-in charge while in the explosion-cylinder E the piston I is at the end of its suctionstrokethat is, has drawn into the explosion-chamber F the desired mixture of gas and air. In the explosion-cylinder E the piston I is at the beginning of the suction-stroke, and in all three cylinders E, E and E the valve H is in a closed position. As the turbine-wheel C rotates the valve H in the explosion-cylinder I gradually gradually closes, and about the time this takes place an explosion takes place in the explosion-cylinder E, so as to give another impulse to the turbine-wheel C, it being understood that when this explosion takes place in the explosion-cylinder E its valve H opens suddenly to direct the charge against the buckets C, as above explained. During the final compression of the charge and the ignition and explosion of the charge in the explosion-cylinder E compression takes place in the cylinder E and at the end of the compression period the mixture is ignited in the cylinder E so that another impulse is given to the turbine-wheel C. In a like manner a final impulse is given to the wheel C shortly after by the exploded charge in the explosion-cylinder E and then the next impulse is given to the wheel by the explosion from the explosion-cylinder E to complete the cycle. Thus it will be seen that during each revolution of the turbine-wheel C four successive impulses are given to the buckets C in quick succession to insure a uniform and powerful running of the turbine.
The explosion-chambers F of the several explosioncylinders E, E, E and E are preferably water-jacketed, as indicated in the drawings, and the cylinder B is likewise preferably water-jacketed to keep the turbine at the proper temp ature.
Having thus. escribed my invention, I claim as new and desire to secure by Letters Patent 1. An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a disagainst the buckets in the direction of rotaplosion period.
2. An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a discharge-nozzle for discharging a motive agent against the buckets in the direction of rotation of the turbine-wheel, a piston in the explosion-chamber controlled from said turbinewheel for drawing in an explosive charge and for compressing the same previous to ignition, a valve in said nozzle for opening and closing the latter, and means operated by the piston-operating means for locking the piston during the explosion period.
3. An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a discharge-nozzle for discharging a motive agent against the buckets in the direction of rotation of the turbine-Wheel, a piston in the explosion chamber controlled from said turbine-wheel for drawing in an explosive charge and for compressing the same previous to ignition, means operated by the piston-operating means for locking the piston during the explosion period, and a valve operating in conjunction with said piston and opening qui kly at the end of the compression period of said piston.
4. An explosion-turbine comprising a cylinder, a turbine-wheel mounted to turn in said cylinder and provided with peripheral buckets, an explosion-chamber having a discharge-nozzle for discharging a motive agent against the buckets in the direction of rotation of the turbine-wheel, a piston in the explosion-chamber controlled from said turbine-wneel for drawing in an explosive charge and for compressing the same previous to ignition, means operated by the piston-operating means for locking the piston during the explosion period, and a valve operating in conjunction with the said piston and opening quickly at the end of the compression period of said piston and remaining open until after the beginning of the return stroke of the piston whereby the turbine-wheel may create a suction in the said working chamber to clear the same of the products of combustion.
5. An explosion-turbine comprising a cylinder, a turbine wheel having peripheral buckets and arranged to turn in said cylinder, an explosion-chamber having a nozzle for discharging a motive agent against the buckcharge-nozzle for discharging amotive agent l ets of the turbine-wheel, a piston reciprocating in the said explosion-chamber and controlled from said il'LlIblllQJVllGQl, means for supplying said explosion-011amber with an explosive charge, an ignition device for ignitmg the said explosive charges, means operinder, a turbine-wheel having buckets and mounted to turn in said cylinder, an explos1on-chamber having a nozzle for discharging a motive agent against the buckets of the turi bine-whecl, a piston reciprocating in the said explosion-chamber and controlled irom the said turbine-wheel, means for supplying the said explosion-chamber with an explosive charge, a valve mthe said nozzle and operat ing in unison with said piston, an automatic i locking device for said piston, and means whereby the piston-operating means may control the operation of said locking device. 7. An explosion-turbine, comprising a cylinder, a turbine wheel having peripheral buckets mounted to turn in the said cylinder, a plurality of explosion-cylinders spaced apart from each other and grouped around the said cylinder, each explosion-cylinder comprising aneXplosion-chamber having a nozzle for discharging an explosive charge against said buckets means for supplying an explosive charge to said explosion-chamber,
an igniting device in the explosion-chamber,
a reciprocating piston in the explosion-chamber for drawing in an explosive charge and for compressing the same immediately previous to the ignition of the charge by said igniting device, means connected with the turbine-wheel for operating the piston, and means operated by the piston-operating means for locking the piston during the explosion period.
8. An explosion-turbine, comprising a cylinder, a turbine-wheel having peripheral buckets mounted to turn in the said cylinder a plurality of explosion cylinders spaced I i i E a l i l I l l l l I g i J 1' apart from each other and grouped around said cylinder, each explosion-cylinder comprising an explosion-chamber and having a nozzle for discharging an explosive charge against the said buckets, means for supplyingan explosive charge to said explosionchamber, an igniting device in the explosionchamber, a reciprocating piston in the said explosion-chamber for drawing in a charge and compressing the same immediately previous to the ignition of the charge by said igniting device, means connected with the turbine-whecl for operating the piston; means operated by the piston-operating means for locking the, piston during the explosion period, and an automatic valve in said discharge-nozzle.
9. An explosion-turbine comprising a cylinder, a turbine wheel having peripheral buckets and mounted to turn in the cylinder, a plurality of explosion cylinders spaced apart from each other and grouped around the cylinder, each explosion-cylinder comprising an explosion-chamber having a nozzle for discharging an explosive charge against said buckets, means for supplying the explosive charge to said explosion-chamber, an igniting device in the explosion-chamber, a reciprocating piston in the said explosionchamber for drawing in a charge and compressing the same immediately previous to the ignition of the charge by said igniting device, means for locking the piston against movement during the explosion period, an automatic valve in said discharge-nozzle, means for operating the said piston, and the said valve in unison from the turbine-wheel,
and means whereby the piston-operating means may operate the locking device.
In testimony whereof I have signed my name to this specification in the presence of two subscribing Witnesses.
AUGUSTUS L. MOSS.
Witnesses:
H. L. PEEKE, J OHN, H. IMMEL.
US25052305A 1905-03-17 1905-03-17 Explosion-turbine. Expired - Lifetime US820238A (en)

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Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461195A (en) * 1945-01-30 1949-02-08 United Aircraft Corp Generator mounting
US2728537A (en) * 1953-01-06 1955-12-27 Arthur B Elkins Aircraft with shrouded propelling and lifting rotors
US2829493A (en) * 1953-09-24 1958-04-08 Hobson Walter Control apparatus for a gas turbine with a plurality of intermittent type combustion chambers
US2945348A (en) * 1958-11-26 1960-07-19 Tychota Kazimierz Combustion apparatus for a gas turbine of the reaction type
US4807440A (en) * 1987-02-24 1989-02-28 Ahmed Salem Internal combustion engine
US20090199812A1 (en) * 2003-03-21 2009-08-13 Jung Kuang Chou Structure of the rotary engine
ES2411829R1 (en) * 2011-03-01 2013-09-13 Bergado Sergio Soto AXIAL INJECTION MOTOR
US20140007837A1 (en) * 2012-07-09 2014-01-09 Isaac Erik Anderson Shockwave Rotor Detonation (Omni-Engine, Ubiquitous X engine) Multipurpose Engine

Cited By (9)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2461195A (en) * 1945-01-30 1949-02-08 United Aircraft Corp Generator mounting
US2728537A (en) * 1953-01-06 1955-12-27 Arthur B Elkins Aircraft with shrouded propelling and lifting rotors
US2829493A (en) * 1953-09-24 1958-04-08 Hobson Walter Control apparatus for a gas turbine with a plurality of intermittent type combustion chambers
US2945348A (en) * 1958-11-26 1960-07-19 Tychota Kazimierz Combustion apparatus for a gas turbine of the reaction type
US4807440A (en) * 1987-02-24 1989-02-28 Ahmed Salem Internal combustion engine
US20090199812A1 (en) * 2003-03-21 2009-08-13 Jung Kuang Chou Structure of the rotary engine
ES2411829R1 (en) * 2011-03-01 2013-09-13 Bergado Sergio Soto AXIAL INJECTION MOTOR
US20140007837A1 (en) * 2012-07-09 2014-01-09 Isaac Erik Anderson Shockwave Rotor Detonation (Omni-Engine, Ubiquitous X engine) Multipurpose Engine
US9970294B2 (en) * 2012-07-09 2018-05-15 Isaac Erik Anderson Shockwave rotor detonation (omni-engine, ubiquitous X engine) multipurpose engine

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