US2471476A - Process and apparatus for transmitting energy - Google Patents

Process and apparatus for transmitting energy Download PDF

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US2471476A
US2471476A US573765A US57376545A US2471476A US 2471476 A US2471476 A US 2471476A US 573765 A US573765 A US 573765A US 57376545 A US57376545 A US 57376545A US 2471476 A US2471476 A US 2471476A
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octafluorocyclobutane
temperatures
nickel
octafiuorocyclobutane
heat exchanger
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Anthony F Benning
Frederick B Downing
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KINETIC CHEMICALS Inc
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    • CCHEMISTRY; METALLURGY
    • C09DYES; PAINTS; POLISHES; NATURAL RESINS; ADHESIVES; COMPOSITIONS NOT OTHERWISE PROVIDED FOR; APPLICATIONS OF MATERIALS NOT OTHERWISE PROVIDED FOR
    • C09KMATERIALS FOR MISCELLANEOUS APPLICATIONS, NOT PROVIDED FOR ELSEWHERE
    • C09K5/00Heat-transfer, heat-exchange or heat-storage materials, e.g. refrigerants; Materials for the production of heat or cold by chemical reactions other than by combustion
    • C09K5/08Materials not undergoing a change of physical state when used
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01KSTEAM ENGINE PLANTS; STEAM ACCUMULATORS; ENGINE PLANTS NOT OTHERWISE PROVIDED FOR; ENGINES USING SPECIAL WORKING FLUIDS OR CYCLES
    • F01K25/00Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for
    • F01K25/08Plants or engines characterised by use of special working fluids, not otherwise provided for; Plants operating in closed cycles and not otherwise provided for using special vapours

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  • This invention relates to processes and apparatus for transmitting energy and particularly to such processes and apparatus employing octafluorocyclobutane as the energy transmitting medium.
  • Water particularly in the form of steam, has been most widely used as the medium for transmitting energy and especially for operating turblues and the like. which limit its use and the efiiciency of the apparatus in which it is used. Its boiling point is rather high for best results in many applications. It has a high critical pressure, over 3000pounds per square inch, which is impractical to attain commercially due to limitations in the strengths of materials and difficulties in design. Steam has a low density, which limits the power obtainable, and requires large and bulky apparatus. Steam is also deficient in entropy relationships along the saturation line, showing a decreasing entropy with increasing temperature. Consequently, steam turbines must be operated withinnarrow temperature limits fixed by the entropy at which the expansion is effected or the steam must be resuperheated between stages to prevent crossing the liquid line.
  • Mercury has also been proposed as a medium for transmitting energy. However, it is highly toxic and-high in cost which greatly limits its practical utilization. It has a high boiling point which limits its use in turbines and which makes the actual operating vapor density and pressure ever, such compoundsare quite unstable at desirable temperatures of operation of. the apparatus. Diphenyl and diphenyl ether have been proposed and appear to be quite stable at temperatures somewhat in excess of 300 G. However, due to their high boiling points of 255 C. to 270 C.,.their utility is quite limited.
  • a further object is to provide a process and apparatus whereby octafiuorocyclobutane can be successfully employed for transmitting energy at high temperatures.
  • a particular obi ect is to provide a process and apparatus for operating turbines and the likewith octafiuorocyclobutane as the power fluid.
  • Other objects are to advance the However, it has properties art. Still other objects will appear hereinafter.
  • octafluorocyclobutane Downing. Benning and McHarness disclose and claim octafluorocyclobutane as a new chemical compound and its preparation by pyrolysis of CHClFz. We have found that octafluorocyclobutane has many desirable properties which particularly adapt it for utilization as an energy transmitting medium. It is non-corrosive, nontoxic and non-inflammable. It has a boiling point of -4.7 C. and a freezing point or 40.7 C. It has critical constants which'are practically ideal for transmitting energy; These constants are:
  • the octafluorocyclobutane can be successfully employed for transmitting energy involving temperatures of from about 250 C. to about 400 C., if those parts of the apparatus in contact with the octafluorocyclobutane at such temperatures is made of a metal of the group of nickel and Inconel.
  • "InconeP is an alloy whose typical composition is nickel 79.5%, chromium 13%, copper 0.2%, iron 6.5%, silicon 0.25%, manganese 0.25% and carbon 0.08%.
  • the steel employed in the above table was an S. A. E. 1340 steel whose composition is given in the 1944 S. A. E. handbook as follows: Carbon 0.380.43%; manganese 1.60-1.90%; phosphorus maximum 0.040%; sulfur maximum 0.040%; silicon 0.20-0.35% and balance iron.
  • the 18-8 stainless steel was an S. A. E. 30915) A. I. S. I. type 302) steel, the specifications for which are: Carbon 0.08-0.15%; manganese maximum 2.00%; silicon 0.75%; phosphorus maximum 0.03%; sulfur maximum 0.03%; chro mium HBO-20.00%; nickel 700-10.00% and the balance iron. It was found impossible to complete the tests because of the rapid decomposition of the octafluorocyclobutane which caused the safety discs in the bombs to blow in substantially less than 100 hours.
  • the apparatus embodying our invention may be any apparatus suited to transmitting energy and wherein a gaseous fluid at temperatures of from about 250 C. to about 400 C. is advantageously employed.
  • the apparatus may take the form of a heat exchanger wherein the octafluorocyclobutane is employed as a cooling medium or a heating medium at the indicated high temperatures.
  • Our invention is particularly adapted, however, to the operation of an engine involvin a prime mover of the character of a turbine.
  • a representative form of apparatus is indicated somewhat diagrammatically in Fig. 1 of the drawings accompanying this application.
  • the apparatus is shown as comprising a heater ID, a turbine l2, a heat exchanger H, a cooler l6 and a compressor ll, all connected by suitable conduits.
  • the octafluorocyclobutane may be heated in the heater I0 to about 600 F. and under a pressure of about 700 pounds per square inch.
  • the octafluorocyclobutane under such temperature and pressure may then be introduced into the turbine and expanded to drive the turbine, during which the temperature will be reduced to about 460 F. and the pressure will be reduced to about 50 pounds per square inch.
  • the exhaust from the turbine may then be passed through the heat exchanger l4 where it is brought into indirect heat exchange relationship with octafluorocyclobutane passing to the heater.
  • the exhaust gases may be cooled to a temperature of about 390 F. at a pressure of about 50 pounds per square inch.
  • the exhaust gases from the heat exchanger may then be passed to the cooler l6 wherein the temperature is further reduced to about 235 F.
  • the cooled fluid from the cooler will then be passed to the compressor i8 where it will be compressed to about 700 pounds per square inch and then returned to the heater through the heat exchanger.
  • the compressed octafluorocyclobutane will be heated to about 440 F.
  • the octafluorocyclobutane may be heated to about 750 F. at about 1000 pounds per square inch. It will then be conducted to the turbine and expanded to drive the turbine, whereby the temperature may be reduced to about 580 F. and the pressure may be reduced to about 75 pounds per square inch.
  • the exhaust gases from the turbine will then be passed through the heat exchanger in indirect heat relation to the octafluorocyclobutane passing to the heater. In the heat exchanger, the exhaust gases will be cooled to about 110 F. and converted to a mixture of liquid and vapor. when this mixture of liquid and vapor is passed to the condenser l6, it will be converted to a liquid at 1 about 100 F. and 75 pounds per square inch.
  • liquid from the condenser will then be passed to the pump wherein it will be subjected to a. pressure of about 1000 pounds per square inch and forced through the heat exchanger to the heater.
  • the octafluorocyclobutane While passing through the heat exchanger, the octafluorocyclobutane will be heated to about 540 F. and converted to a vapor which passes to the heater for further heating.
  • the surfaces of the heater, turbineand conduits connecting the same which surfaces are in contact with the octafluorocyclobutane, will be made of a metal of the group of nickel and Inconel in order to avoid objectionable decomposition of the octafluorocyclobutane.
  • the surfaces of the heat exchanger, in contact with the octafluorocyclobutane are preferably made of nickel or Inconel,
  • the cooler or condenser, the compressor or pump and the conduits connecting them. with each other and with the heat exchanger may be made of ordinary or stainless steel without inducing objectionable decomposition of the octafiuorocyclobutane.
  • the process of protectively conducting octafluorocyclobutane attemperatures of from about 250 C. to about 400 C. which comprises enclosing the octafiuorocyclobutane in a conductor in which at least the surfaces in contact with the octafluorocyclobutane are made of a metal of the group consisting of nickel and an alloy whose composition is. essentially nickel 79.5%, chromium 13%, copper 0.2%, iron 6.5%, silicon 0.25%, manganese 0.25% and carbon 0.08%.
  • the process of protectively conducting 'octafiuorocyclobutane at temperatures of from about 250 C. to about 400 C. which comprises enclosing the octafluorocyclobutane in a conductor in which at least the surfaces in contact with the octafiuorocyclobutane are' made of an alloy whose composition is essentially nickel 79.5%, chromium 13%, copper 0.2%, iron 63%, silicon 0.25%, manganese 0.25% and carbon 0. 8%.
  • the process of transferring heat which comprises heating octafluorocyclobutane to temperatures of from about 250 C. to about400 C. andthen passing it in indirect heat transfer relation with a body of material to be heated, and maintaining the octafiuorocyclobutane, while at temperatures between about 250 C. and about 400 C., in direct contact with only an alloy whose compositioni's essentially nickel 79.5%, chromium 13%, copper 0.2% iron 6.5%, silicon 0.25%, manganese 0.25% and carbon 0.08%.-

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Description

May 31, 1949. A. F. BENNING ETI'AL 2,471,476
PROCESS AND APPARATUS FOR TRANSMITTING ENERGY Filed Jan. 20, um
14 [HEAT exaumazfl I 1N VEN TOR! fi wi k Bulb I BY Z k ?atented May 31, 1949 FFIC PROCESS APPARAEUS FQR TRANSMITTING ENERGY corporation ot Delaware Application January 20, 1965, Serial No. 578365 4 Claims. a
This invention relates to processes and apparatus for transmitting energy and particularly to such processes and apparatus employing octafluorocyclobutane as the energy transmitting medium.
Water, particularly in the form of steam, has been most widely used as the medium for transmitting energy and especially for operating turblues and the like. which limit its use and the efiiciency of the apparatus in which it is used. Its boiling point is rather high for best results in many applications. It has a high critical pressure, over 3000pounds per square inch, which is impractical to attain commercially due to limitations in the strengths of materials and difficulties in design. Steam has a low density, which limits the power obtainable, and requires large and bulky apparatus. Steam is also deficient in entropy relationships along the saturation line, showing a decreasing entropy with increasing temperature. Consequently, steam turbines must be operated withinnarrow temperature limits fixed by the entropy at which the expansion is effected or the steam must be resuperheated between stages to prevent crossing the liquid line.
Mercury has also been proposed as a medium for transmitting energy. However, it is highly toxic and-high in cost which greatly limits its practical utilization. It has a high boiling point which limits its use in turbines and which makes the actual operating vapor density and pressure ever, such compoundsare quite unstable at desirable temperatures of operation of. the apparatus. Diphenyl and diphenyl ether have been proposed and appear to be quite stable at temperatures somewhat in excess of 300 G. However, due to their high boiling points of 255 C. to 270 C.,.their utility is quite limited.
It is an object of our invention to provide a process and apparatus for transmittingenergy employing a novel energy transmitting medium. A further object is to provide a process and apparatus whereby octafiuorocyclobutane can be successfully employed for transmitting energy at high temperatures. A particular obi ect is to provide a process and apparatus for operating turbines and the likewith octafiuorocyclobutane as the power fluid. Other objects are to advance the However, it has properties art. Still other objects will appear hereinafter.
The above and other objects may be accomplished in accordance with our invention which comprises apparatus and the process of operating the same for transmitting energy wherein octafiuorocyclobutane is employed at temperatures above 200 C. and not substantially in excess of 400 0., in which the parts or the apparatus in contact with the octafluorocyclobutane at the temperatures aforesaid are made of a metal of the group of nickel and Inconel. We have found that octafluorocyclobutane can be successfully employed under such circumstances with many advantages.
In copending application Serial No. 535,208.
filed May 11, 1944, now Patent No. 2,384,821,
Downing. Benning and McHarness disclose and claim octafluorocyclobutane as a new chemical compound and its preparation by pyrolysis of CHClFz. We have found that octafluorocyclobutane has many desirable properties which particularly adapt it for utilization as an energy transmitting medium. It is non-corrosive, nontoxic and non-inflammable. It has a boiling point of -4.7 C. and a freezing point or 40.7 C. It has critical constants which'are practically ideal for transmitting energy; These constants are:
tc=115.3 C. pc=393 pounds per square inch absolute dc=0.612 g./cc.
It is readily ieasible to heat this fluid above the critical pressure, eliminating ebullition complete- 1y with a resulting smooth temperature gradient ed adiabatic expansion under almost any condition within the superheat range without danger of crossing the saturation line.
We have found, however, that, when octafiuorocyclobutane is heated at temperatures substantially above 200 C. and particularly at temperatures of about 250 C. and higher in the presence of ordinary steel, stainless steel and bronze, it decomposes to a very material extent with the deposition of gums, carbon and other decomposition products on the surfaces in contact therewith. On the other hand, we have found that, if the octafluorocyclobutane is maintained in contact with only a metal of the group of nickel and Inconel while at temperatures substantially above 200 C. and not substantially in excess of 400 C., the octafluorocyclobutane will not decompose to a material extent, but will be extremely stable. Therefore, the octafluorocyclobutane can be successfully employed for transmitting energy involving temperatures of from about 250 C. to about 400 C., if those parts of the apparatus in contact with the octafluorocyclobutane at such temperatures is made of a metal of the group of nickel and Inconel. "InconeP is an alloy whose typical composition is nickel 79.5%, chromium 13%, copper 0.2%, iron 6.5%, silicon 0.25%, manganese 0.25% and carbon 0.08%.
The effect of metals, on the decomposition of octafluorocyclobutane at high temperatures, are shown by a series of tests, wherein a bomb, constructed of the metal to be tested, was charged with a known weight of the octafluorocyclobutane. The ratio of metal surface toweight of octafluorocyclobutane was substantially as follows:
Volume/surface of bomb=0.31 cc./sq. cm. Surface/weight of charge=10 sq. om./g. Density of gas in charged bomb=0.32 g./cc.
Table Temperature, C 250 300 350 I 400 600-530 Steel- 7 23 40 Nickel 2, 400 Iuoonel 5 2, 400
The steel employed in the above table was an S. A. E. 1340 steel whose composition is given in the 1944 S. A. E. handbook as follows: Carbon 0.380.43%; manganese 1.60-1.90%; phosphorus maximum 0.040%; sulfur maximum 0.040%; silicon 0.20-0.35% and balance iron.
Attempts were made to carry out the same tests in bombs made of 18-8 stainless and in bronze. The 18-8 stainless steel was an S. A. E. 30915) A. I. S. I. type 302) steel, the specifications for which are: Carbon 0.08-0.15%; manganese maximum 2.00%; silicon 0.75%; phosphorus maximum 0.03%; sulfur maximum 0.03%; chro mium HBO-20.00%; nickel 700-10.00% and the balance iron. It was found impossible to complete the tests because of the rapid decomposition of the octafluorocyclobutane which caused the safety discs in the bombs to blow in substantially less than 100 hours. For example, in the 18-8 stainless steel bomb at 350 (1., the discs blew during the first 29 hours and an analysis of the residue left in the bomb indicated a decomposition of at least 3 times that in an ordinary steel bomb after 100 hours. The results in the bronze bomb were similar.
The apparatus embodying our invention may be any apparatus suited to transmitting energy and wherein a gaseous fluid at temperatures of from about 250 C. to about 400 C. is advantageously employed. The apparatus may take the form of a heat exchanger wherein the octafluorocyclobutane is employed as a cooling medium or a heating medium at the indicated high temperatures. Our invention is particularly adapted, however, to the operation of an engine involvin a prime mover of the character of a turbine. A representative form of apparatus is indicated somewhat diagrammatically in Fig. 1 of the drawings accompanying this application.
In the drawings, the apparatus is shown as comprising a heater ID, a turbine l2, a heat exchanger H, a cooler l6 and a compressor ll, all connected by suitable conduits. As illustrative of a possible operation of such apparatus, in accordance with our invention, the octafluorocyclobutane may be heated in the heater I0 to about 600 F. and under a pressure of about 700 pounds per square inch. The octafluorocyclobutane under such temperature and pressure may then be introduced into the turbine and expanded to drive the turbine, during which the temperature will be reduced to about 460 F. and the pressure will be reduced to about 50 pounds per square inch. The exhaust from the turbine may then be passed through the heat exchanger l4 where it is brought into indirect heat exchange relationship with octafluorocyclobutane passing to the heater. In this heat exchanger, the exhaust gasesmay be cooled to a temperature of about 390 F. at a pressure of about 50 pounds per square inch. The exhaust gases from the heat exchanger may then be passed to the cooler l6 wherein the temperature is further reduced to about 235 F. The cooled fluid from the cooler will then be passed to the compressor i8 where it will be compressed to about 700 pounds per square inch and then returned to the heater through the heat exchanger. In the heat exchanger, the compressed octafluorocyclobutane will be heated to about 440 F. For successful operation without material decomposition of the octafluorocyclobutane, it will be essential that the surfaces of the heater, the turbine and the conduits connecting them be made of nickel or Inconel. This is illustrative of an operation employing a non-condensing cycle.
If it is desired to operate with a condensing cycle, this may be done by substituting a condenser for the cooler IS. The octafluorocyclobutane may be heated to about 750 F. at about 1000 pounds per square inch. It will then be conducted to the turbine and expanded to drive the turbine, whereby the temperature may be reduced to about 580 F. and the pressure may be reduced to about 75 pounds per square inch. The exhaust gases from the turbine will then be passed through the heat exchanger in indirect heat relation to the octafluorocyclobutane passing to the heater. In the heat exchanger, the exhaust gases will be cooled to about 110 F. and converted to a mixture of liquid and vapor. when this mixture of liquid and vapor is passed to the condenser l6, it will be converted to a liquid at 1 about 100 F. and 75 pounds per square inch. The
liquid from the condenser will then be passed to the pump wherein it will be subjected to a. pressure of about 1000 pounds per square inch and forced through the heat exchanger to the heater. While passing through the heat exchanger, the octafluorocyclobutane will be heated to about 540 F. and converted to a vapor which passes to the heater for further heating. Under these conditions, also, the surfaces of the heater, turbineand conduits connecting the same, which surfaces are in contact with the octafluorocyclobutane, will be made of a metal of the group of nickel and Inconel in order to avoid objectionable decomposition of the octafluorocyclobutane. Also, under these conditions, the surfaces of the heat exchanger, in contact with the octafluorocyclobutane, are preferably made of nickel or Inconel,
although this is not absolutely necessary since the rate of decomposition in steel is not particularly high at the maximum temperature (238 C.) attained therein. In both cycles, the cooler or condenser, the compressor or pump and the conduits connecting them. with each other and with the heat exchanger may be made of ordinary or stainless steel without inducing objectionable decomposition of the octafiuorocyclobutane.
From all of the above, it will be apparent that, by our invention, we have provided a process and apparatus which makes it possible to employ octafluorocyclobutane as an energy transmitting medium and obtain the advantages of the desirable properties of the octafluorocyclobutane and without obtaining objectionable decomposition of the octafiuorocyclobutane. It will be readily apparent to those skilled in the art that many variations may be made in the construction and type of the apparatus and its mode of operation without departing from the spirit or scope of our invention. Accordingly, our invention is not to be limited to the specific embodiments disclosed, but we intend to cover our invention broadly as in the appended claims.
We claim:
1. The process of protectively conducting octafluorocyclobutane attemperatures of from about 250 C. to about 400 C. which comprises enclosing the octafiuorocyclobutane in a conductor in which at least the surfaces in contact with the octafluorocyclobutane are made of a metal of the group consisting of nickel and an alloy whose composition is. essentially nickel 79.5%, chromium 13%, copper 0.2%, iron 6.5%, silicon 0.25%, manganese 0.25% and carbon 0.08%.
2. The process of protectively conducting 'octafiuorocyclobutane at temperatures of from about 250 C. to about 400 C. which comprises enclosing the octafluorocyclobutane in a conductor in which at least the surfaces in contact with the octafiuorocyclobutane are' made of an alloy whose composition is essentially nickel 79.5%, chromium 13%, copper 0.2%, iron 63%, silicon 0.25%, manganese 0.25% and carbon 0. 8%.
3. The process of transferring heat which comprises heating octafluorocyclobutane to temperatures of from about 250 C. to about400 C. andthen passing it in indirect heat transfer relation with a body of material to be heated, and maintaining the octafiuorocyclobutane, while at temperatures between about 250 C. and about 400 C., in direct contact with only an alloy whose compositioni's essentially nickel 79.5%, chromium 13%, copper 0.2% iron 6.5%, silicon 0.25%, manganese 0.25% and carbon 0.08%.-
4. The method of operating an engine which comprises heating octafluorocyclobutane under superatmospheric pressures to a temperature between about 250 C. and about 400 C., expanding the heated octafiuorocyclobutane through a turbine, cooling the octafiuorocyclobutane exhausted from the turbine and then condensing the cooled octafluorocyclobutane, maintaining the octafiuorocyclobutane while at temperatures between about 250 C. and about 40 C. in direct contact with only an alloy whose composition is essentially nickel 79.5%, chromium 13%, copper 0.2%, iron 6.5%, silicon 0.25%, manganese 0.25%
and carbon 0.08%
ANTHONY F. BENNING. FREDERICK B. DOWNING.
REFERENCES CITED The following references are of record in the OTHER REFERENCES Directory of Materials, 11th edition, supplement to Machine Design for October 1943, page 169.
Nickel and'its Alloys, circular of the Bureau of Standards No. 100.
International Nickel Company Bulletin No.T-7, January 1939. Pages 5, 6, 12-14.
Chemical and Metallurgical Engineering," McGraw-Hill Publ. 00., N. Y., Sept. 1944. Page 105.
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Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2591874A (en) * 1950-04-06 1952-04-08 Clayton F Ritchie Bubble-forming writing instrument
US2655788A (en) * 1946-10-07 1953-10-20 Rateau Soc Turbine gas engine adapted to operate with or without atmospheric air chiefly for the propulsion of warships
US2852564A (en) * 1955-01-21 1958-09-16 Reichhold Chemicals Inc Process for controlling reaction temperature in vapor phase oxidation of alcohols to aldehydes
US3040528A (en) * 1959-03-22 1962-06-26 Tabor Harry Zvi Vapor turbines
US3154928A (en) * 1962-04-24 1964-11-03 Conch Int Methane Ltd Gasification of a liquid gas with simultaneous production of mechanical energy
US3224199A (en) * 1964-10-19 1965-12-21 Hawker Siddeley Canada Ltd Closed cycle gas turbine
US3225538A (en) * 1960-03-25 1965-12-28 Catacycle Company Inc Conversion of heats of chemical reactions to sensible energy
US3234738A (en) * 1962-10-11 1966-02-15 Wilfred L Cook Low temperature power cycle
US3237403A (en) * 1963-03-19 1966-03-01 Douglas Aircraft Co Inc Supercritical cycle heat engine
US3339663A (en) * 1964-06-09 1967-09-05 James H Anderson Vehicular power plant
US3376706A (en) * 1965-06-28 1968-04-09 Angelino Gianfranco Method for obtaining mechanical energy from a thermal gas cycle with liquid phase compression
US3495402A (en) * 1968-01-18 1970-02-17 John W Yates Power system
US3670500A (en) * 1970-06-22 1972-06-20 Arthur H Schultz Thermodynamic power system and methods
US3708979A (en) * 1971-04-12 1973-01-09 Massachusetts Inst Technology Circuital flow hot gas engines
US3867816A (en) * 1970-11-04 1975-02-25 George M Barrett Low pollution reciprocating heat engine
US3872673A (en) * 1972-02-10 1975-03-25 Atomenergi Ab Accumulation power station
US3998059A (en) * 1973-07-12 1976-12-21 National Research Development Corporation Power systems
US4085590A (en) * 1976-01-05 1978-04-25 The United States Of America As Represented By The United States Department Of Energy Hydride compressor
US11028735B2 (en) 2010-08-26 2021-06-08 Michael Joseph Timlin, III Thermal power cycle

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US1154880A (en) * 1912-03-18 1915-09-28 John Patten Power-generating system.
US1483298A (en) * 1918-12-09 1924-02-12 Commentry Fourchambault & Deca Alloy comprising iron, nickel, chromium, molybdenum
GB294243A (en) * 1927-07-22 1929-06-06 Siemens Ag Improvements in and relating to vapour engines for aircraft
US1837439A (en) * 1928-04-23 1931-12-22 Holzwarth Hans Turbine blade for gas and steam turbines
US2220934A (en) * 1934-01-20 1940-11-12 Rustless Iron & Steel Corp Alloy steel articles
US2301404A (en) * 1939-03-20 1942-11-10 Bradford B Holmes Method of translating heat energy into motive power

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US1154880A (en) * 1912-03-18 1915-09-28 John Patten Power-generating system.
US1483298A (en) * 1918-12-09 1924-02-12 Commentry Fourchambault & Deca Alloy comprising iron, nickel, chromium, molybdenum
GB294243A (en) * 1927-07-22 1929-06-06 Siemens Ag Improvements in and relating to vapour engines for aircraft
US1837439A (en) * 1928-04-23 1931-12-22 Holzwarth Hans Turbine blade for gas and steam turbines
US2220934A (en) * 1934-01-20 1940-11-12 Rustless Iron & Steel Corp Alloy steel articles
US2301404A (en) * 1939-03-20 1942-11-10 Bradford B Holmes Method of translating heat energy into motive power

Cited By (19)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2655788A (en) * 1946-10-07 1953-10-20 Rateau Soc Turbine gas engine adapted to operate with or without atmospheric air chiefly for the propulsion of warships
US2591874A (en) * 1950-04-06 1952-04-08 Clayton F Ritchie Bubble-forming writing instrument
US2852564A (en) * 1955-01-21 1958-09-16 Reichhold Chemicals Inc Process for controlling reaction temperature in vapor phase oxidation of alcohols to aldehydes
US3040528A (en) * 1959-03-22 1962-06-26 Tabor Harry Zvi Vapor turbines
US3225538A (en) * 1960-03-25 1965-12-28 Catacycle Company Inc Conversion of heats of chemical reactions to sensible energy
US3154928A (en) * 1962-04-24 1964-11-03 Conch Int Methane Ltd Gasification of a liquid gas with simultaneous production of mechanical energy
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