US1008689A - Combustion-chamber. - Google Patents

Combustion-chamber. Download PDF

Info

Publication number
US1008689A
US1008689A US59414610A US1910594146A US1008689A US 1008689 A US1008689 A US 1008689A US 59414610 A US59414610 A US 59414610A US 1910594146 A US1910594146 A US 1910594146A US 1008689 A US1008689 A US 1008689A
Authority
US
United States
Prior art keywords
valve
chamber
valves
combustion chamber
air
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
Application number
US59414610A
Inventor
Benjamin H Blaisdell
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Priority to US59414610A priority Critical patent/US1008689A/en
Application granted granted Critical
Publication of US1008689A publication Critical patent/US1008689A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K7/00Plants 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
    • F02K7/02Plants 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

Definitions

  • This invention relates to combustion chambers for use in connection with gas engines of the turbine type; and it consists in the novel construction and combination of the parts hereinafter fully'described and claimed whereby the gas engine is supplied with pressure fluid todrive it.
  • Figurel isalongitudinal section through a combustion chamber constructed according to this invention.
  • Fig. 2 is a crosssection, taken on the line 00-0a in Fig. 1.
  • A is the explosion chamber in which a charge of air and hydrocarbon is ignited. This chamber is relatively very long in proportion to its diameter or width, and
  • one end of it is provided with a flange a or other approved means for connecting it to the turbine or other engine to be driven.
  • the igniter B is the igniter which is of any approved construction, such as an electric igniter. This igniter is arranged in the chamber A adjacent to its outlet end.
  • C is a water jacket encircling the combustion chamber and forming a boiler for generating steam. This jacket is provided with a steam dome 0, and a safety-valve c.
  • D is a cylinder or casing for the regulating valves arranged in the inlet end portion of the combustion chamber.
  • E is the air inlet passage at one side of the combustion chamber
  • F is the fuel inlet passage at its opposite side.
  • Any approved fuel can be used, such as a liquid hydrocarbon, combustible vapor or gas,'and the apparatus can be variously modified and changed to suit the particular kind of fuel used.
  • G is the air valve; and H is the gas valve.
  • These valves are semi-cylindrical in form, and they are slidable side by side in the cylinder D.
  • These valves and the cylinder are provided with any suitable ports 6 and f for the passage of air and gas respectively.
  • I is the valve spindle provided at one end with a T-shaped head 2' which engages with two recesses in the valves G and II respectively.
  • the valve spindle I projects through this cylinder D, and it is provided with a handle 71 on its projecting end for sliding it by hand when required.
  • the cushioning cylinder is provided with a cushioning piston j, and y" is a port of small area which permits air to pass from one side of the piston to the other, and which prevents the piston from moving too rapidly at the ends of its strokes.
  • K is a valve for admitting air to the ends of the cushioning cylinder; and 7c are adjustable plugs for regulating the outlet of air from the cylinder and adjusting the compression or cushioning.
  • These valves are semi-cylindrical in form and they are slidable in the valve cylinder D and on the valve spindle I.
  • the valves, or as many of them as necessary, are
  • suitable means such as grooves and keys for preventing them from revolving.
  • S is the water pipe which is connected to the water jacket and to a water port 8 in the combustion chamber and valve cylinder.
  • a valve 8' is provided for regulating the supply of water.
  • T is a steam pipe connected to the steam dome and to a steam port If in the combustion chamber and valve cylinder.
  • the valves N and P are provided with ports a and p which are placed in communication with the ports t and s respectively, and which communicate with a longitudinal passage 9 in the valve spindle leading through the air and gas valves into the combustion chamber.
  • the space a between the air valve and the steam valve is connected with the steam port by a passage o,'and the space '0 is constantly in communication with the space between the gas valve and the water valve.
  • W is an air inlet pipe connected at one end with the space in the valve cylinder between the cushioning cylinder J and the steam and water valves.
  • the other end of the pipe W is connected to the air inlet passage E, or to any other convenient source whence a supply of compressed air can be obtained.
  • the air and gas Valve are opened by hand, or by pressure from the pipe WV, and the steam and water valves are closed by the pressure of the air from the pipe W.
  • Air and gas are admitted under pressure to the combustion chamber through their respective passages E and F, their proportions being regulated by suitable valves, not shown.
  • the air and gas are compressed to any desirable extent by any approved devices, not shown, so that they may flow freely into the combustion chamber and become mixed therein.
  • the explosive mixture of air and gas passes longitudinally through the combustion chamber and is ignited when it reaches the igniter 13 near the outlet end of the chamber.
  • the pressure rises suddenly in the combustion chamber, and the gas and air valves are pro-- pelled rearwardly to close their respective ports, shock and undue impact being prevented by the cushioning piston.
  • the pressure thus obtained in the combustion chamber affords a means for driving a turbine gas engine or other similar motor.
  • WVhen the pressure in the combustion chamber falls below the pressure of the compressed air in the pipe I, the steam and water valves are moved forwardly to open the steam and water ports.
  • the steam and water valves slide upon the valve spindle I which remains stationary.
  • Steam and water from the water jacket are now injected through the combustion chamber into the motor and force the products of combustion out of the 'combustion chamber, and assist in driving the motor.
  • the valve 3 can be closed,if desired, and steam alone can be used as the scavenging fluid.
  • the air from the pipeW forces all the valves forward to their original positions, re-opening the air and gas valves G and H, and closing the steam and water valves.
  • the explosions in the combustion chamber take place intermittently'and at intervals regulated by the requirements of the motor.
  • the steam and water spray assist in propelling the motor and also prevent it and the valves from being overheated by the explosions.
  • the valves are automatic in their action being operated by the fluid pressure of the products of combustion and the compressed air and not by valve operating mechanism, but the form and arrangement of the valves may be changed and modified in many ways in carryingout this invention,
  • What I claim is: 1.
  • valve spindle connected to the said valves and provided with a passage which communicates constantly with the combustion chamber, a steam valve and a water valve arranged side by side and controlling the said passage and also slidable in the said cylinder, and means for admitting compressed air to the said cylinder to force all the said valves forwardly therein.

Landscapes

  • 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

B. H. BLAISDELL.
COMBUSTION CHAMBER.
APPLICATION FILED NOV. 25, 1910.
Patented Nov. 14, 1911.
I 31mm Wihawoeo COLUMBIA PLAMJGIIAPH C4?" WASHINGTON, D4 C.
BENJAMIN I-I. BLAISDELL, 0F MANILA, PHILIPPINE ISLANDS.
COMBUSTION-CHAMBER.
Specification of Letters Patent.
Patented Nov. 14, 1911.
Application filed November 25, 1910. Serial No. 594,146.
To all whom it may concern:
Be it known that I, BENJAMIN H. BLAIS- DELL, a citizen of the United States, residing at Manila, in the Philippine Islands, have invented certain new and useful Improvements in Combustion-Chambers; and I do hereby declare the following to be a full, clear, and exact description of the inven tion, such as will enable others skilled in the art to which it appertains to make and use the same.
This invention relates to combustion chambers for use in connection with gas engines of the turbine type; and it consists in the novel construction and combination of the parts hereinafter fully'described and claimed whereby the gas engine is supplied with pressure fluid todrive it.
In the drawings, Figurel isalongitudinal section through a combustion chamber constructed according to this invention. Fig. 2 is a crosssection, taken on the line 00-0a in Fig. 1.
A is the explosion chamber in which a charge of air and hydrocarbon is ignited. This chamber is relatively very long in proportion to its diameter or width, and
one end of it is provided with a flange a or other approved means for connecting it to the turbine or other engine to be driven.
B is the igniter which is of any approved construction, such as an electric igniter. This igniter is arranged in the chamber A adjacent to its outlet end.
C is a water jacket encircling the combustion chamber and forming a boiler for generating steam. This jacket is provided with a steam dome 0, and a safety-valve c.
D is a cylinder or casing for the regulating valves arranged in the inlet end portion of the combustion chamber. i
E is the air inlet passage at one side of the combustion chamber, and F is the fuel inlet passage at its opposite side. Any approved fuel can be used, such as a liquid hydrocarbon, combustible vapor or gas,'and the apparatus can be variously modified and changed to suit the particular kind of fuel used.
G is the air valve; and H is the gas valve. These valves are semi-cylindrical in form, and they are slidable side by side in the cylinder D. These valves and the cylinder are provided with any suitable ports 6 and f for the passage of air and gas respectively.
I is the valve spindle provided at one end with a T-shaped head 2' which engages with two recesses in the valves G and II respectively.
J is acushioning cylinder which forms a cover for closing the outer end of the valve cylinder D. The valve spindle I projects through this cylinder D, and it is provided with a handle 71 on its projecting end for sliding it by hand when required. The cushioning cylinder is provided with a cushioning piston j, and y" is a port of small area which permits air to pass from one side of the piston to the other, and which prevents the piston from moving too rapidly at the ends of its strokes.
K is a valve for admitting air to the ends of the cushioning cylinder; and 7c are adjustable plugs for regulating the outlet of air from the cylinder and adjusting the compression or cushioning.
N is the steam valve; and P is the water valve. These valves are semi-cylindrical in form and they are slidable in the valve cylinder D and on the valve spindle I. The valves, or as many of them as necessary, are
provided with suitable means, such as grooves and keys for preventing them from revolving.
S is the water pipe which is connected to the water jacket and to a water port 8 in the combustion chamber and valve cylinder. A valve 8' is provided for regulating the supply of water.
T is a steam pipe connected to the steam dome and to a steam port If in the combustion chamber and valve cylinder.
The valves N and P are provided with ports a and p which are placed in communication with the ports t and s respectively, and which communicate with a longitudinal passage 9 in the valve spindle leading through the air and gas valves into the combustion chamber.
The space a between the air valve and the steam valve is connected with the steam port by a passage o,'and the space '0 is constantly in communication with the space between the gas valve and the water valve.
W is an air inlet pipe connected at one end with the space in the valve cylinder between the cushioning cylinder J and the steam and water valves. The other end of the pipe W is connected to the air inlet passage E, or to any other convenient source whence a supply of compressed air can be obtained.
In starting the apparatus the air and gas Valve are opened by hand, or by pressure from the pipe WV, and the steam and water valves are closed by the pressure of the air from the pipe W. Air and gas are admitted under pressure to the combustion chamber through their respective passages E and F, their proportions being regulated by suitable valves, not shown. The air and gas are compressed to any desirable extent by any approved devices, not shown, so that they may flow freely into the combustion chamber and become mixed therein. The explosive mixture of air and gas passes longitudinally through the combustion chamber and is ignited when it reaches the igniter 13 near the outlet end of the chamber. The pressure rises suddenly in the combustion chamber, and the gas and air valves are pro-- pelled rearwardly to close their respective ports, shock and undue impact being prevented by the cushioning piston. The pressure thus obtained in the combustion chamber affords a means for driving a turbine gas engine or other similar motor. WVhen the pressure in the combustion chamber falls below the pressure of the compressed air in the pipe I, the steam and water valves are moved forwardly to open the steam and water ports. The steam and water valves slide upon the valve spindle I which remains stationary. Steam and water from the water jacket are now injected through the combustion chamber into the motor and force the products of combustion out of the 'combustion chamber, and assist in driving the motor. The valve 3 can be closed,if desired, and steam alone can be used as the scavenging fluid. When the steam pressure falls in the combustion chamber below the pressure of the air. in the air pipe W, the air from the pipeWforces all the valves forward to their original positions, re-opening the air and gas valves G and H, and closing the steam and water valves.
' The explosions in the combustion chamber take place intermittently'and at intervals regulated by the requirements of the motor. The steam and water spray assist in propelling the motor and also prevent it and the valves from being overheated by the explosions. The valves are automatic in their action being operated by the fluid pressure of the products of combustion and the compressed air and not by valve operating mechanism, but the form and arrangement of the valves may be changed and modified in many ways in carryingout this invention,
What I claim is: 1. The combination, with a tubular combustion chamber of great length in proportion to its width, said chamber'having an inlet at one end and an outlet at its other end, and the said outlet and the passage through the chamber being constantly open and unobstructed; of an igniter arranged at the outlet end of the chamber, and automatic valve mechanism controlling the admission of combustible fluid through the said inlet, said valve mechanism being operated intermittently by direct exposure to the varying pressure of the fluid contents of the chamber.
2. The combination, with a tubular combustion chamber of great length in proportion to its width, said chamber having an inlet at one end and an outlet at its other end, and the said outlet and the passage through the chamber being constantly open and unobstructed; of an igniter arranged at the outlet end of the chamber, automatic valve mechanism controlling the admission of combustible fluid through the said inlet, said valve mechanism being operated intermittently by direct exposure to the varying pressure of the fluid contents of the chamber, and means for admitting scavenging fluid to the said chamber to scavenge its contents in the interval between the combustion of one charge and the admission of another charge.
3. The combination, with a combustion chamber having an inlet for the combustible charge at one end and an outlet for the high pressure gases at the other end, of an igniter arranged in the said chamber adjacent to its out-let, valve mechanism controlling the supmitting steam and water'to the combustion chamber, and a cylinder for compressed air which opens the steam and water valves when the pressure in the combustion chamber falls after ignition.
5. The combination, with a combustion chamber, and a boiler heated by said chamber, of automatic valves for air and fuel which close when the contents of the chamber are ignited, a valve for admitting scavenging fluid from the said boiler to the combustion chamber, and a cylinder for compressed air which opens the said valve when the pressure in the combustion chamber falls after ignition.
6. The combination, with a combustion chamber, of a valve cylinder secured in one end portion of the combustion chamber, automatic valves for air and fuel which slide in the said cylinder and close when the contents of the chamber are ignited, and
means for admitting compressed air to the said cylinder behind the said valves to open them when the pressure falls in the combustion chamber.
7. The combination, with a combustion chamber, of a valve cylinder secured in one end portion of the combination chamber, automatic valves for air and fuel which slide in the said cylinder and close when the contents of the chamber are ignited, a valve spindle connected to the said valves-and projecting from the valve cylinder, and a cushioning device connected to the said spindle and preventing the valves from moving too suddenly.
8. The combination, with a combustion chamber, of a valve cylinder secured in one end portion of the chamber, automatic valves for air and fuel which slide in the said cylinder and close when the contents of the chamber are ignited, a valve spindle connected to the said valves and provided with a passage which communicates constantly with the combustion chamber, and a valve for scavenging fluid slidable in the said cylinder and controlling the said passage through the valve spindle.
9. The combination, with a combustion chamber, of a valve cylinder secured in one end portion of the chamber, automatic valves for air and fuel which slide in the said cylinder and close when the contents of the chamber are ignited, a valve spindle connected to the said valves and provided with a passage which communicates constantly with the combustion chamber, a steam valve and a water valve arranged side by side and controlling the said passage and also slidable in the said cylinder, and means for admitting compressed air to the said cylinder to force all the said valves forwardly therein.
10. The combination, with a combustion chamber for a gas turbine having an igniter at its outlet end, and having also automatic valves for air, fuel and scavenging fluid at its opposite end, said valves being operated by the varying pressure of the fluid contents of the said chamber; of means for generating steam from the surplus heat of combustion, said automatic valves being arranged to admit the steam to the combustion chamber in the interval between the combustion of one charge and. the admission of another charge, to scavenge its contents and to assist in driving the turbine; and means for mix 1 ing cooling fluid with the said steam to prevent the turbine from being overheated.
In testimony whereof I have affixed my signature in the presence of two witnesses.
BENJAMIN H. BLAISDELL.
l/Vitnesses:
MICH. W. JENKINS, FRANS L. CRnIsosToMo.
Copies of this patent may be obtained for five cents each, by addressing the Commissioner of Patents. Washington, D. G.
US59414610A 1910-11-25 1910-11-25 Combustion-chamber. Expired - Lifetime US1008689A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US59414610A US1008689A (en) 1910-11-25 1910-11-25 Combustion-chamber.

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US59414610A US1008689A (en) 1910-11-25 1910-11-25 Combustion-chamber.

Publications (1)

Publication Number Publication Date
US1008689A true US1008689A (en) 1911-11-14

Family

ID=3077000

Family Applications (1)

Application Number Title Priority Date Filing Date
US59414610A Expired - Lifetime US1008689A (en) 1910-11-25 1910-11-25 Combustion-chamber.

Country Status (1)

Country Link
US (1) US1008689A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2523012A (en) * 1947-11-01 1950-09-19 Daniel And Florence Guggenheim Intermittent feed mechanism for combustion chambers
US2563022A (en) * 1944-02-12 1951-08-07 Daniel And Florence Guggenheim Fuel feeding mechanism for detonating combustion apparatus
US2630674A (en) * 1947-02-01 1953-03-10 Daniel And Florence Guggenheim Device for feeding liquid combustion agents to a combustion chamber used in propulsion apparatus

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2563022A (en) * 1944-02-12 1951-08-07 Daniel And Florence Guggenheim Fuel feeding mechanism for detonating combustion apparatus
US2630674A (en) * 1947-02-01 1953-03-10 Daniel And Florence Guggenheim Device for feeding liquid combustion agents to a combustion chamber used in propulsion apparatus
US2523012A (en) * 1947-11-01 1950-09-19 Daniel And Florence Guggenheim Intermittent feed mechanism for combustion chambers

Similar Documents

Publication Publication Date Title
US980801A (en) Internal-combustion engine.
US1510688A (en) Power plant
US1008689A (en) Combustion-chamber.
US985793A (en) Internal-combustion motor.
US870720A (en) Internal-combustion engine.
US1008583A (en) Combustion-chamber.
US865725A (en) Generation of vapor.
US1156534A (en) Heat-engine.
US278255A (en) G-as engine
US1132381A (en) Pressure-generator.
US260513A (en) Gas-motor engine
US459404A (en) lanchester
US939229A (en) Internal-combustion gas-turbine.
US1152003A (en) Gas-producer for explosive-engines.
US1305581A (en) And one-fourth to everett e
US178121A (en) Improvement in gas-engines
US870308A (en) Engine.
US587375A (en) siddle
US594372A (en) Igniter for explosive-engines
US337226A (en) anthony
US971760A (en) Engine.
US1054728A (en) Power device.
US610034A (en) Gas-engine
US688245A (en) Explosive-engine.
US673008A (en) Furnace.