US1014330A - Apparatus for heating compressed air. - Google Patents
Apparatus for heating compressed air. Download PDFInfo
- Publication number
- US1014330A US1014330A US27478005A US1905274780A US1014330A US 1014330 A US1014330 A US 1014330A US 27478005 A US27478005 A US 27478005A US 1905274780 A US1905274780 A US 1905274780A US 1014330 A US1014330 A US 1014330A
- Authority
- US
- United States
- Prior art keywords
- air
- conduit
- motor
- burner
- compressed 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
Links
- 238000010438 heat treatment Methods 0.000 title description 7
- 239000000446 fuel Substances 0.000 description 20
- 239000012530 fluid Substances 0.000 description 18
- 238000002485 combustion reaction Methods 0.000 description 9
- 238000003303 reheating Methods 0.000 description 9
- 230000001276 controlling effect Effects 0.000 description 6
- 238000005192 partition Methods 0.000 description 5
- 238000005086 pumping Methods 0.000 description 4
- 230000001105 regulatory effect Effects 0.000 description 4
- 230000005540 biological transmission Effects 0.000 description 2
- 238000001816 cooling Methods 0.000 description 2
- 239000007788 liquid Substances 0.000 description 2
- 208000027418 Wounds and injury Diseases 0.000 description 1
- 230000006835 compression Effects 0.000 description 1
- 238000007906 compression Methods 0.000 description 1
- 230000006378 damage Effects 0.000 description 1
- 208000014674 injury Diseases 0.000 description 1
- 238000009413 insulation Methods 0.000 description 1
- 238000000034 method Methods 0.000 description 1
- 230000004048 modification Effects 0.000 description 1
- 238000012986 modification Methods 0.000 description 1
- 230000008016 vaporization Effects 0.000 description 1
- XLYOFNOQVPJJNP-UHFFFAOYSA-N water Substances O XLYOFNOQVPJJNP-UHFFFAOYSA-N 0.000 description 1
Images
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
- F02C9/00—Controlling gas-turbine plants; Controlling fuel supply in air- breathing jet-propulsion plants
- F02C9/26—Control of fuel supply
- F02C9/32—Control of fuel supply characterised by throttling of fuel
Definitions
- This invention relates to the art of locally heating a pressure-fluid in a transmission line which conducts the fluid from the primary source of supply to a mechanically separate and more or less remote primary user.
- An example is the reheating of compressed air at a point adjacent to the compressed-air engine, tool or other user.
- the object is to provide a self-regulating internal-combustion reheat-er, which in a preferred form includes a suitable motor driven by the compressed air from the conduit whose contents are to be heated and operating a fuel pump which injects a supply of fuel into the air conduit.
- This fuel burns in the compressed air and heats the sameto such a temperature as will increase the economy without injury to the using or controlling apparatus.
- I may employ a suitable thermostatic regulator controlling the operation of the pump in such manner as to check the supply of fuel when the temperature has reached the desired maximum. Thereby the amount of fuel consumed is adjusted in proportion to the rate of flow or consumption of the compressed air.
- the automatic regulation may also be secured Without the thermostat as I shall hereinafter explain; This apparatus can be employed with some modification to heat or superheat other fluids, such as steam.
- Figure 1 represents an elevation of acompressed-air heating apparatus organized in accordance with my mvention, parts of the view being drawn to dilterent scales
- Fig. 2 represents a vertical section of the burner and thermostatic regulator
- Figs. 3 and 4 represent sections on the lines 3--3 and 4--4 of Fig. 2
- Fig. 7 represents an edge view of the motor-pump for injecting the fuel into the compressed-air conduit
- Figs. 8, 9 and 10 represent sections on' the lines 8 8 99 and 1010 of Fig. 7.
- 10 indicates a conduit supplied with compressed air" from [an aircompressor 11 and delivering to a suitable translating device'or devices 12 such as a compressed air tool or motor.
- The-conduit 10 is shown provided with an enlargement 13 having a partition 14 partially dividing its interior into two chambers 15 16 in series,
- the burner 17 constructed as a Bunsen burner, with a gas-nozzle 18 and a mixing-tube 19 into the lower part of which the air is drawn by the force of the gas jet in such proportion as to provide a flame within the chamber 15.
- the burner has also an outer or secondary mixing-tube 180 perforated and doublewa-lled to provide air-insulation for sepa-.
- 191 is an externally-heated reentrant hottube igniter for the burner and 192 is a glazed peep-tube for observing the condition of the flame and combustion-chamber walls.
- a thermostat shown as a Bourdon tube 20 par-.
- a vaporizing liquid such as water and hermetically sealed.
- This tube is fixed at one end 21 and its other end connects with a pivoted lever 23 carrying a valve 24 which controls the outlet from conduit 10 to a tap or branch conduit 25.
- the main resistance to the expansion of the Bourdon tube is furnished by a spring 26 having an adjustment .27 for regulating its a tension.
- the pipe 25 conducts a supplyof compressed air from the air conduit 10 to a combined motor and gas-compressor 28 composed of four motor cylinders 29 alternating with four gas-compressor cylinders 30.
- All of the pistons 31 32 are connected by pitmen 33 34 with a single crank 35 upon a crank-shaft 36.
- One of the pitmen 34 has an enlarged head, upon which the ends of the other pitmen are stepped 'and prevented from outward disconnection by bolts 37 and side-plates 370.
- the pistons are all. single acting.
- valve-rods 38 operated-from a single eccentric 39 located approximatel at an angle of 90 with the crank 35, t e valve structures being alongside 'of the compressor cylinders.
- Each valve structure .embodies a piston valve 40 controlling the admission of gas to one of the compressorcylinders 30, the discharge being controlled by an ordinary check-valve 41, and a second piston valve 42 controlling both. the admission and exhaust of compressed air to and from one of the motor cylinders 29 througha port or duct 43.
- the compressed air pipe- 25 has branches 44 leading to the several valve-chests and the compressed gas is led by branches 45 into a pipe 46 connecting with the burner 17. Admission of gas to the valve-chests is by way of pipes 47.
- Such adjustment determines the degree of coldnessof the motor exhaust and hence determines, first, the amount of cooling of the gas-compressor 1 cylinders by means of the jacketing'motorexhaust, and secondly the amount of cooling of the gas going to the gas-compressor cylpasses through a gas-refrigerator 244 cooled by the motor-exhaust.
- the maximum temperature attained is determined by the thermorangement of connections, in which the stat, whose temperature-controlled element is the Bourdontube 20.' When the critical temperature is reached, this tube, expanding,- tends to close the valve 24 against the tension of spring 26 and thus diminish the supply of compressed air to the motor-pump 28, whereupon the speed of the latter is checked and the supply'of fuel maintained at a point which will kee the temperature of the air constant.' This temperature is maintained irrespective of the quantity of air flowing in conduit 10, for obviously if the flow: is increased the temperature will tend to drop and the valve in 24 will open, sending more compressed air to the motor and affording an increased supply of fuel.
- the temperature imparted to the air should not be higher than is suited to the ordinary uncooled compressed-air tools and motors in common use.
- the motor ump 28 will operate with a wide range of speed and very little vibration. Owing to its absence of dead-centers its crank will creep around. at a very slow rate when required. It is to be noted, furthermore, that the application of maximum power is almost in a direct line.
- the compressor-cylinder requiring greatest application of power in the position of parts'there shown is the uppermost one in the figure,-while the motor cylinder best able to afford power, owing to the beginning of its stroke with compressed air at full pressure, is the cylinder 29 immediately to the left of the lowermostcompressor-cylinder 30, and the two pistons are almost in a straightsline with each other. I therefore prefer this kind of a compressorpump for using the air-power and deliver:
- My invention may be used for superheating steam or heating other fluids besides air, in which case the burner 17 would be supplied with both air and fuel from the motor pump 28 with suitable changes therei in which could be effected by a skilled mechanic.
- Fig. 1 also shows an alternate aroourse of the air is indicated by dotted arrows, whereby all of the compressed air used in the power-transmission line is passed through the motor-pump 28, being reduced in pressure only" slightly by performing 120 work "in the motor cylinders and passed on to do further work in the main translating devices.
- the air goes to the compressor-cylinders of motor-pump v28 through a valved pipe 100, and after ex- .hausting' from said cylinders, it enters the burner casing 13 through pipe 102 instead of passing out into the atmosphere by branch 101.
- a stop-valve 103 is provided in the air conduit 10 to prevent 130 duit connecting the two,
- the motor cylinders act as meters of the quantity of air to the translating devices and they automatically provide the necessary quantity of gas required to furnish the desired moderate temperature, the capacities of the gascom pressor cylinders being so established as to be in the necessary proportion to the aircompressor cylinders.
- the thermostat may then be-omitted or disconnected.
- I have shown the same motor-pump adapted for both the described methods of regulating the amount of fuel, although in practice it mightbe preferable'to have this device differently proportioned in the two cases.
- a fluid conduit supplied from a remote point, of a local heater for said conduit comprising an internal-combustion burner in the conduit adapted-t0 moderately heat the fluid, and a pumping and regulating device supplied with motive fluid fromthe conduit and adapted to inject the fuel for said burner, said device bein sensitive to the quantity of fluid flowing 1n the conduit, so as to injflect fuel in proportion to said. quantity of 2.
- a compressed air system comprising mechanically-separate primary air compressing and using devices connected by a transmlssion conduit, an internal-combustion burner in said conduit adjacent to the air-using device, and local pumping means supplied with motive fluid from the conduit for injecting the burner fuel.
- Fluid reheating means comprising a pressure conduit adapted to be interposed between a source of pressure-fluid supply and a remote using device, an internalcombustion reheating burner in said conduit, an indep1 ndently-running motor-pump supplied wit motive fluid from said conduit for injecting the burner .fuel, and a thermostat subject to the reheating temperashown, to direct theair in ture and controlling the motive-fluid supply to said motor-pump.
- a ressure fluid conduit an internal-combustion heater therein, a local motor-pump supplied with fluid by a branch from said conduit and adapted to inject the burner fuel, a throttle-valve in said branch, and a thermostat subject to the burner temperature and controlling said throttle-valve.
- a reheating apparatus comprising a compressed-air conduit, an internal-combustion burner therein, a gas-compressor to supply said burner, a motor using the conduit-air, and means for refrigerating with the motor exhaust the gas supplied to said compressor.
- a reheating apparatus comprising a compressed air conduit, an internal-combustion burner therein, a gas-compressor to supply said burner, a motor using the conduit air, and means gas-compressor with the motor-exhaust.
- a compressed-air reheater comprising a compressed-air conduit, an internal-combustion burner therein, a motor-pump driven by the conduit-air for supplying fuel to said burner, means for coolingthe fuel-'supply with the motor exhaust, and means for varying the temperature of the conduit-air supplied to said motor-pump.
- a compressedair reheater comprising acompressed-air conduit, an internal-combustion burner therein, a local" motor supplied with conduit-air from points anterior and posterior to said burner, distributing valve-mechanism in the motor-supply line for adjusting the proportions of heated and unheated air oing to the motor, and a thermostat sub ect to the temperature of the said valve-mechheated air and controllin anism for causing the atter to. variably throttle the air supplied to the motor.
- Reheating apparatus comprising a fluid conduit havin an enlarged section provided with a eflecting partition, a burner in the conduit on one side of said partition, a branch outlet and outlet-valve on the remote side of said partition, a motor-pump supplied with heated air from said outlet and adapted to supply fuel under pressure to the burner, and a thermostat on. the remote side of the partition controllin said valve.
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Feeding And Controlling Fuel (AREA)
Description
S. A. REEVE. APPARATUS FOR HEATING COMPRESSED AIR.
APPLICATION FILED AUG. 18, 1905.
Patented Jan. 9, 1912.
4 SHEBTS-SHEET 1.
s. A. BEEVE. APPARATUS FOR HEATING OOMPRESSED AIR- APPLIOATION FILED AUG. 18, 1905.
Patented Jan. 9, 1912.
1 SHEETSSHEET 2.
S. A. REEVE.
APPARATUS FOR HEATING COMPRESSED AIR.
APPLIOATION FILED AUG. 18, 1905.
1,014,330, Patented Jan. 9, 1912.
wine/55643 j. f/JM' s. A. REEVE.
APPARATUS FOR HEATING COMPRESSED AIR.
APPLICATION FILED AUG. 18, 1905.
* Patented J an. 9, 1912.
4 SHEETSSHEET 4.
UNITED STATES PATENT OFFICE.
' SIDNEY A. new, or woncns'mn, uassacnusm'rs, assxeuon, .BY unsure ass'xeug MENTS, '10 O. P. POWERLCOMPANY, OF NEW JERSEY.
OI NEWARK, NEW JERSEY, A CORPORATION APPARATUS FOR HEATING COMPRESSED AIR.
Specification of letters latent.
Patented Jan. 9.191 2.
- Application filed August 18, 1905. Serial'NoL 274,780.
To-all whom it may concern:
Be it lmownthat I, SIDNEY A. REEVE, a citizen of the United States, residing at Worcester, in the county of Worcester and State of Massachusetts, have invented certain new and useful Improvements in Apparatus for Heating Compressed Air, of which the following specification and accompanying drawings illustrate. the invention in a form which I now regard as the best out of the various forms in which it may be embodied.
This invention relates to the art of locally heating a pressure-fluid in a transmission line which conducts the fluid from the primary source of supply to a mechanically separate and more or less remote primary user. An example is the reheating of compressed air at a point adjacent to the compressed-air engine, tool or other user.
The object is to provide a self-regulating internal-combustion reheat-er, which in a preferred form includes a suitable motor driven by the compressed air from the conduit whose contents are to be heated and operating a fuel pump which injects a supply of fuel into the air conduit. This fuel burns in the compressed air and heats the sameto such a temperature as will increase the economy without injury to the using or controlling apparatus. In conjunction with the foregoing I may employ a suitable thermostatic regulator controlling the operation of the pump in such manner as to check the supply of fuel when the temperature has reached the desired maximum. Thereby the amount of fuel consumed is adjusted in proportion to the rate of flow or consumption of the compressed air. The automatic regulation may also be secured Without the thermostat as I shall hereinafter explain; This apparatus can be employed with some modification to heat or superheat other fluids, such as steam.
Of the accompanying drawings, Figure 1 represents an elevation of acompressed-air heating apparatus organized in accordance with my mvention, parts of the view being drawn to dilterent scales, Fig. 2 represents a vertical section of the burner and thermostatic regulator, Figs. 3 and 4 represent sections on the lines 3--3 and 4--4 of Fig. 2, Figs. 5 and 6-represent sections on the lines 5-5 and.66 of Fig. 3, Fig. 7 represents an edge view of the motor-pump for injecting the fuel into the compressed-air conduit,
Figs. 8, 9 and 10 represent sections on' the lines 8 8 99 and 1010 of Fig. 7.
The same reference characters indicate the same parts in all the figures.
In the drawings, 10 indicates a conduit supplied with compressed air" from [an aircompressor 11 and delivering to a suitable translating device'or devices 12 such as a compressed air tool or motor. The-conduit 10 is shown provided with an enlargement 13 having a partition 14 partially dividing its interior into two chambers 15 16 in series,
in the former of which is located the burner 17, constructed as a Bunsen burner, with a gas-nozzle 18 and a mixing-tube 19 into the lower part of which the air is drawn by the force of the gas jet in such proportion as to provide a flame within the chamber 15. The burner has also an outer or secondary mixing-tube 180 perforated and doublewa-lled to provide air-insulation for sepa-.
rating the interior upward hot flow from the outer downward flow of cold air going tothe burner through the annular passage 190.
191 is an externally-heated reentrant hottube igniter for the burner and 192 is a glazed peep-tube for observing the condition of the flame and combustion-chamber walls.
In the opposite chamber 16 is located a thermostat shown as a Bourdon tube 20 par-.
tially filled with a vaporizing liquid such as water and hermetically sealed. This tube is fixed at one end 21 and its other end connects with a pivoted lever 23 carrying a valve 24 which controls the outlet from conduit 10 to a tap or branch conduit 25. The main resistance to the expansion of the Bourdon tube is furnished by a spring 26 having an adjustment .27 for regulating its a tension. The pipe 25 conducts a supplyof compressed air from the air conduit 10 to a combined motor and gas-compressor 28 composed of four motor cylinders 29 alternating with four gas-compressor cylinders 30. All of the pistons 31 32 are connected by pitmen 33 34 with a single crank 35 upon a crank-shaft 36. One of the pitmen 34 has an enlarged head, upon which the ends of the other pitmen are stepped 'and prevented from outward disconnection by bolts 37 and side-plates 370. The pistons are all. single acting.
The air and gas distribution is controlled by four valve-rods 38 operated-from a single eccentric 39 located approximatel at an angle of 90 with the crank 35, t e valve structures being alongside 'of the compressor cylinders. Each valve structure .embodies a piston valve 40 controlling the admission of gas to one of the compressorcylinders 30, the discharge being controlled by an ordinary check-valve 41, and a second piston valve 42 controlling both. the admission and exhaust of compressed air to and from one of the motor cylinders 29 througha port or duct 43. The compressed air pipe- 25 has branches 44 leading to the several valve-chests and the compressed gas is led by branches 45 into a pipe 46 connecting with the burner 17. Admission of gas to the valve-chests is by way of pipes 47. Exhaust air discharges into the central portion ofthe air-tight casing 48, of the motor-pump, e gas-compressor cylinders by table by means of a handle 243. They open inders, which before reaching said cylinders and close their respective ports proportionately by longitudinal motlon and inversely by rotatory motion, so that-by turning the handle, the proportions of heated and nonheated air goingto drive the motor pump,
may be regulated; Such adjustment determines the degree of coldnessof the motor exhaust and hence determines, first, the amount of cooling of the gas-compressor 1 cylinders by means of the jacketing'motorexhaust, and secondly the amount of cooling of the gas going to the gas-compressor cylpasses through a gas-refrigerator 244 cooled by the motor-exhaust.
In the' o eration of this apparatus a small portion 0 heated compressed air from the conduit 10 is tapped ofl throu h pipe 25 to the motor-pump28, mixed if esired with a proportion of non-heated air from branch 242, and there aflr'ords power for the compression of gas (or it may be the pumping of liquid fuel) to a pressure hi her than that of the air conduit 10. This el burns in the compressed air in chamber 15 and serves to impart thereto any desired moderate temperature, say 600 F. There is of course a very large excess of air'in the conduit over what will satisfy the amount of fuel, introduced. -The maximum temperature attained is determined by the thermorangement of connections, in which the stat, whose temperature-controlled element is the Bourdontube 20.' When the critical temperature is reached, this tube, expanding,- tends to close the valve 24 against the tension of spring 26 and thus diminish the supply of compressed air to the motor-pump 28, whereupon the speed of the latter is checked and the supply'of fuel maintained at a point which will kee the temperature of the air constant.' This temperature is maintained irrespective of the quantity of air flowing in conduit 10, for obviously if the flow: is increased the temperature will tend to drop and the valve in 24 will open, sending more compressed air to the motor and affording an increased supply of fuel. The temperature imparted to the air should not be higher than is suited to the ordinary uncooled compressed-air tools and motors in common use.
The motor ump 28 will operate with a wide range of speed and very little vibration. Owing to its absence of dead-centers its crank will creep around. at a very slow rate when required. It is to be noted, furthermore, that the application of maximum power is almost in a direct line. For example, in Fig. 8 the compressor-cylinder requiring greatest application of power in the position of parts'there shown is the uppermost one in the figure,-while the motor cylinder best able to afford power, owing to the beginning of its stroke with compressed air at full pressure, is the cylinder 29 immediately to the left of the lowermostcompressor-cylinder 30, and the two pistons are almost in a straightsline with each other. I therefore prefer this kind of a compressorpump for using the air-power and deliver:
ing the fuel, although it is obvious that other 105 forms of apparatus might be used for a like purpose.
My invention may be used for superheating steam or heating other fluids besides air, in which case the burner 17 would be supplied with both air and fuel from the motor pump 28 with suitable changes therei in which could be effected by a skilled mechanic. Fig. 1 also shows an alternate aroourse of the air is indicated by dotted arrows, whereby all of the compressed air used in the power-transmission line is passed through the motor-pump 28, being reduced in pressure only" slightly by performing 120 work "in the motor cylinders and passed on to do further work in the main translating devices. In this case the air goes to the compressor-cylinders of motor-pump v28 through a valved pipe 100, and after ex- .hausting' from said cylinders, it enters the burner casing 13 through pipe 102 instead of passing out into the atmosphere by branch 101.- For this arrangement a stop-valve 103 is provided in the air conduit 10 to prevent 130 duit connecting the two,
direct passage of the air into casing 13, and other stop-valves 104 105 106 107 in the various pipes as either of the two alternate paths described. When all of the air passes through the motor-pump, the motor cylinders act as meters of the quantity of air to the translating devices and they automatically provide the necessary quantity of gas required to furnish the desired moderate temperature, the capacities of the gascom pressor cylinders being so established as to be in the necessary proportion to the aircompressor cylinders. The thermostat may then be-omitted or disconnected. For convenience of illustration I have shown the same motor-pump adapted for both the described methods of regulating the amount of fuel, although in practice it mightbe preferable'to have this device differently proportioned in the two cases.
What I claim as new and desire to secure by Letters Patent is:
1. In the art of reheating elastic pressure fluids, the combination with a fluid conduit supplied from a remote point, of a local heater for said conduit comprising an internal-combustion burner in the conduit adapted-t0 moderately heat the fluid, and a pumping and regulating device supplied with motive fluid fromthe conduit and adapted to inject the fuel for said burner, said device bein sensitive to the quantity of fluid flowing 1n the conduit, so as to injflect fuel in proportion to said. quantity of 2. A compressed air system comprising mechanically-separate primary air compressing and using devices connected by a transmlssion conduit, an internal-combustion burner in said conduit adjacent to the air-using device, and local pumping means supplied with motive fluid from the conduit for injecting the burner fuel.
3. The combination of an air-compressor, a separate air-engine, a transmission conand a local selfregulating internal-combustion burner and fuel-pumping mechanism for reheating the air adjacent to the point of use, said mechanism being supplied with motive fluid from the condult and sensitive to the quantity of air-flow in the conduit.
4. Fluid reheating means comprising a pressure conduit adapted to be interposed between a source of pressure-fluid supply and a remote using device, an internalcombustion reheating burner in said conduit, an indep1 ndently-running motor-pump supplied wit motive fluid from said conduit for injecting the burner .fuel, and a thermostat subject to the reheating temperashown, to direct theair in ture and controlling the motive-fluid supply to said motor-pump.
5. In combination, a ressure fluid conduit, an internal-combustion heater therein, a local motor-pump supplied with fluid by a branch from said conduit and adapted to inject the burner fuel, a throttle-valve in said branch, and a thermostat subject to the burner temperature and controlling said throttle-valve.
6. A reheating apparatus comprising a compressed-air conduit, an internal-combustion burner therein, a gas-compressor to supply said burner, a motor using the conduit-air, and means for refrigerating with the motor exhaust the gas supplied to said compressor.
7. A reheating apparatus comprising a compressed air conduit, an internal-combustion burner therein, a gas-compressor to supply said burner, a motor using the conduit air, and means gas-compressor with the motor-exhaust.
8. A compressed-air reheater comprising a compressed-air conduit, an internal-combustion burner therein, a motor-pump driven by the conduit-air for supplying fuel to said burner, means for coolingthe fuel-'supply with the motor exhaust, and means for varying the temperature of the conduit-air supplied to said motor-pump.
9. A compressedair reheater comprising acompressed-air conduit, an internal-combustion burner therein, a local" motor supplied with conduit-air from points anterior and posterior to said burner, distributing valve-mechanism in the motor-supply line for adjusting the proportions of heated and unheated air oing to the motor, and a thermostat sub ect to the temperature of the said valve-mechheated air and controllin anism for causing the atter to. variably throttle the air supplied to the motor.
10. Reheating apparatus comprising a fluid conduit havin an enlarged section provided with a eflecting partition, a burner in the conduit on one side of said partition, a branch outlet and outlet-valve on the remote side of said partition, a motor-pump supplied with heated air from said outlet and adapted to supply fuel under pressure to the burner, and a thermostat on. the remote side of the partition controllin said valve.
testimony whereof I have hereunto set my hand in the presence of two subscribing witnesses, the 6th day of May 1905.
I'IENRY P. -MURRAY, Ror W. BURGESS.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US27478005A US1014330A (en) | 1905-08-18 | 1905-08-18 | Apparatus for heating compressed air. |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| US27478005A US1014330A (en) | 1905-08-18 | 1905-08-18 | Apparatus for heating compressed air. |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| US1014330A true US1014330A (en) | 1912-01-09 |
Family
ID=3082636
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| US27478005A Expired - Lifetime US1014330A (en) | 1905-08-18 | 1905-08-18 | Apparatus for heating compressed air. |
Country Status (1)
| Country | Link |
|---|---|
| US (1) | US1014330A (en) |
Cited By (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2736167A (en) * | 1956-02-28 | teague | ||
| US2742755A (en) * | 1949-11-14 | 1956-04-24 | Rolls Royce | Fuel system for pilot burners of gasturbine engines reheat equipment |
| US2750892A (en) * | 1952-11-13 | 1956-06-19 | Bendix Aviat Corp | Turbine driven pump means |
| US3275222A (en) * | 1965-01-11 | 1966-09-27 | Andre J Meyer | Rotary liquid piston machines |
| US20070110590A1 (en) * | 2003-11-18 | 2007-05-17 | Carsten Pabst | Multipiston pump |
-
1905
- 1905-08-18 US US27478005A patent/US1014330A/en not_active Expired - Lifetime
Cited By (6)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US2736167A (en) * | 1956-02-28 | teague | ||
| US2742755A (en) * | 1949-11-14 | 1956-04-24 | Rolls Royce | Fuel system for pilot burners of gasturbine engines reheat equipment |
| US2750892A (en) * | 1952-11-13 | 1956-06-19 | Bendix Aviat Corp | Turbine driven pump means |
| US3275222A (en) * | 1965-01-11 | 1966-09-27 | Andre J Meyer | Rotary liquid piston machines |
| US20070110590A1 (en) * | 2003-11-18 | 2007-05-17 | Carsten Pabst | Multipiston pump |
| US7766626B2 (en) * | 2003-11-18 | 2010-08-03 | Robert Bosch Gmbh | Multipiston pump |
Similar Documents
| Publication | Publication Date | Title |
|---|---|---|
| US2777301A (en) | All-purpose power and air conditioning system | |
| US972504A (en) | Continuous-combustion heat-engine. | |
| US2238905A (en) | Gas turbine plant | |
| US2298625A (en) | Elastic fluid power plant | |
| US2418911A (en) | Gas turbine cycle | |
| US3839858A (en) | Reciprocating machine | |
| US1014330A (en) | Apparatus for heating compressed air. | |
| US2618431A (en) | Control system for gas turbine air compressor plants | |
| US1306865A (en) | Prime moveb | |
| US3550371A (en) | Hot gas engine with speed control | |
| US841791A (en) | Accumulator for flash-boilers. | |
| US1038805A (en) | Hot-air engine. | |
| USRE22201E (en) | Gas turbine plant | |
| US2418477A (en) | Steam power plant | |
| US982871A (en) | Generating apparatus. | |
| US603425A (en) | Governor for air-compressors | |
| US1608445A (en) | Power plant | |
| US268210A (en) | Alfred d | |
| US623137A (en) | creuzbaur | |
| US861393A (en) | Regulating apparatus for heat-engines. | |
| US720778A (en) | Utilization of liquefied air in the production of mechanical energy. | |
| US726442A (en) | Flash-boiler system. | |
| US985563A (en) | Automatic regulation of the evaporating pressure in refrigerating systems. | |
| US975651A (en) | Thermodynamic motor. | |
| US331359A (en) | Air-engine |