US2413751A - Expansion engine - Google Patents

Expansion engine Download PDF

Info

Publication number
US2413751A
US2413751A US539761A US53976144A US2413751A US 2413751 A US2413751 A US 2413751A US 539761 A US539761 A US 539761A US 53976144 A US53976144 A US 53976144A US 2413751 A US2413751 A US 2413751A
Authority
US
United States
Prior art keywords
cylinder
piston
engine
clearance
gas
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
US539761A
Inventor
Dennis Wolcott
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.)
Airco Inc
Original Assignee
Air Reduction Co Inc
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 Air Reduction Co Inc filed Critical Air Reduction Co Inc
Priority to US539761A priority Critical patent/US2413751A/en
Application granted granted Critical
Publication of US2413751A publication Critical patent/US2413751A/en
Anticipated expiration legal-status Critical
Expired - Lifetime legal-status Critical Current

Links

Images

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04248Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion
    • F25J3/04284Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams
    • F25J3/0429Generation of cold for compensating heat leaks or liquid production, e.g. by Joule-Thompson expansion using internal refrigeration by open-loop gas work expansion, e.g. of intermediate or oxygen enriched (waste-)streams of feed air, e.g. used as waste or product air or expanded into an auxiliary column
    • F25J3/04296Claude expansion, i.e. expanded into the main or high pressure column
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J3/00Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification
    • F25J3/02Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream
    • F25J3/04Processes or apparatus for separating the constituents of gaseous or liquefied gaseous mixtures involving the use of liquefaction or solidification by rectification, i.e. by continuous interchange of heat and material between a vapour stream and a liquid stream for air
    • F25J3/04763Start-up or control of the process; Details of the apparatus used
    • F25J3/04866Construction and layout of air fractionation equipments, e.g. valves, machines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F25REFRIGERATION OR COOLING; COMBINED HEATING AND REFRIGERATION SYSTEMS; HEAT PUMP SYSTEMS; MANUFACTURE OR STORAGE OF ICE; LIQUEFACTION SOLIDIFICATION OF GASES
    • F25JLIQUEFACTION, SOLIDIFICATION OR SEPARATION OF GASES OR GASEOUS OR LIQUEFIED GASEOUS MIXTURES BY PRESSURE AND COLD TREATMENT OR BY BRINGING THEM INTO THE SUPERCRITICAL STATE
    • F25J2240/00Processes or apparatus involving steps for expanding of process streams
    • F25J2240/02Expansion of a process fluid in a work-extracting turbine (i.e. isentropic expansion), e.g. of the feed stream
    • F25J2240/10Expansion of a process fluid in a work-extracting turbine (i.e. isentropic expansion), e.g. of the feed stream the fluid being air

Definitions

  • This invention relates to expansion engines for liquefaction systems and particularly to improvements aflording high efllciency in the operation of expansion engines at low temperatures.
  • Another object of the invention is to minimize the losses due to the introduction of heat through friction between the moving parts.
  • Another object of the invention is to provide for the maintenance of a temperature differential between the cold portion of the cylinder and the lubricated portion, by the action of the air or gas used to drive the engine.
  • a further object of the invention is the provision of a structure in which parts subject to wear can be replaced readily and economically so that the enginecan be maintained at its original high efiiciency and at relatively low cost.
  • Fig. l is a vertical section illustrating one form of the invention.
  • Fig. 2 is a similar view illustrating a modification of the engine.
  • 5 indicates a suitable frame upon which a cylinder 6 is supported by bolts i.
  • the cylinder is in two sections, the upper section 8 being secured to the lower section 6 by bolts 9 extending through the'flanges It and H.
  • a rabbeted joint i2 is provided between the sections 6 and 8 of the cylinder to prevent escape of gas therethrough, and to insure accurate lineup of the two sections.
  • the construction of the cylinder in the form indicated permits the removal of the lower section 6 which is subjected to wear and the replacement thereof at intervals so that the engine can be maintained at its maximum eiliciency.
  • a head 13 is secured ,to the upper end of the valves in order that gas under pressure introduced through the inlet l8 may be expanded in the cylinder and discharged through the exhaust passage H.
  • the details of such mechanisms are well known in the art and require no further description.
  • piston 22 is supported and provided with piston rings 23 hearing against the internal surface of the cylinder 6 to prevent the escape or gas.
  • a piston rod 24 is connected in any suitable manner, for example threadedly, as indicated at 25, to a. block 28 secured at the end of the piston 22.
  • the piston rod 24 may be connected also to a conventional crosshead, crank,
  • crankshaft (not shown) adapted to translate movement of the piston.
  • the piston is filled with insulating material 21.
  • a casing 28 is disposed about the cylinder sections 6 and 8 and the head l3 and is filled with insulating material 29 to reduce flow of heat from the external atmosphere through the walls of the cylinder.
  • the lower end of the piston 22 has adiameter affording a relatively close fit with the cylinder 0.
  • the upper end of the piston has a reduced diameter aifording a substantial clearance between the piston and the upper section 8 of the cylinder.
  • the clearance space is preferably tapered and extends beyond the limit of the stroke of the piston indicated by the line :c.r.
  • the amount of radial clearance between the upper end of the piston and the section 8 of the cylinder may vary.
  • the radial clearance at the top of the piston is approximately .010 inch and at the bottom of the reduced portion the radial clearance is approximately .005 inch.
  • the radial clearance may vary from approximately .020 inch at the top of the piston to .002 inch at the bottom of the reduced section.
  • This heating effect has been repeatedlyobserved in the connecting piping between engine cylinders and indicator apparatus, and in engine parts having a single outlet connected to the cylinder and subject to fluctuating pressure. It is I here utilized for the purpose of establishing a large temperature gradient between the cold parts of the cylinder and the working parts which it is desirable to lubricate without difficulties due to freezing of oil or condensation of moisture. It is important of course that the cylinder section 8 be made of such material and of such thickness as to minimize heat conduction to the lower cylinder section-B in order to realize the most benefit from the heating effect. It is also desirableto extend the clearance space downward so that when the piston is in its upper position the space extends some distance below the lower limit of the piston travel. With this construction, the major portion of heat generated by compression of residual gas in the clearance space is transmitted to the cylinder 'wallsbelow the line .r-a:.
  • the use of a tapered piston permits the use of i a larger clearance space at the top. for a given clearance volume and reduces the possibility of contact between piston and cylinder at the top edge of the piston where contact is most apt to occur.
  • the frame supports the lower section 3
  • the upper section 33 of the cylinder is secured to the lower section 3! by bolts 34 extending through flanges 35 and 3B.
  • a rabbeted joint 31 is provided as in the previous embodiment of the invention.
  • a head 38 is secured by bolts 39 to a flange 40 at the upper end of the section 33 of the cylinder and provides inlet and exhaust passages 4
  • Valves 45 and 46 are actuated by mechanism. as in the preceding embodiment of the invention, to
  • a piston 41 is supported in the cylinder and provided with piston rings 48 to afford a gas-tight l fit.
  • the piston is connected in the manner previously described to a piston rod 49 which in turn is connected to a conventional crosshead. crank and crankshaft to translate movement of the piston.
  • the lower end of the piston has a substantiallytight lit in the section 3
  • the upper end of the piston consists of a block 50 of heat insulating material secured to the lower portion by a bolt 5
  • a liner 52 of heat insulating material is disposed within the upper section 33 of the cylinder.
  • the upper section of the piston is of reduced diameter, affording clearance preferably though not necessarily tapered, extending beyond the line .E-.l! representing the limit of travel of the piston.
  • the radial clearance between the piston and the cylinder wall should be within the limits hereinbefore specified.
  • An expansion engine for gases at relatively low temperatures comprising a cylinder, a cylinder head associated therewith including inlet and exhaust passages and valves controlling the delivery of gases to and from the cylinder and a piston movable in the cylinder and having a bearing surface closely fitting the internal surface of the cylinder at the end remote from the cylinder head, the other end of the piston having a reduced diameter affording a relatively narrow tapered radial clearance between the piston and cylinder walls, the maximum clearance being at the cylinder-head end of the piston, the length of that portion of the piston with reduced diameter being greater than the stroke of the piston.
  • An expansion engine for gases at relatively low temperatures comprising a cylinder, a cylinder head associated therewith including inlet and exhaust passages and valves controlling the delivery of gases to and from the cylinder, and a piston movable in the cylinder and having a bearing surface closely fitting the internal surface of the cylinder at the end remote from the cylinder head, the other end of the piston having a reduced diameter affording tapered radial clearance between the piston and cylinder walls, said clearance progressively decreasing from a maximum of .020 inch at the cylinder-head end of the piston to a minimum of .002 inch, the length of that portion of the piston with reduced diameter being greater than the stroke of the piston.
  • An expansion engine for gases at relatively low temperatures comprising a cylinder, a cylinder head associated therewith including inlet and exhaust passages and valves controlling the delivery of gases to and from the cylinder, and a piston movable in the cylinder and having a bearing surface closely fitting the internal surface of the cylinder at the and remote from the cylinder head, the other end of the piston having a reduced diameter affording tapered radial clearance between the piston and cylinder walls, said clearance progressively decreasing from a maximum of .010 inch at the cylinder-head end of the piston to a minimum of .005 inch, the length of that portion of the piston with reduced diameter being greater than the stroke of the piston.

Landscapes

  • Engineering & Computer Science (AREA)
  • Physics & Mathematics (AREA)
  • Mechanical Engineering (AREA)
  • Thermal Sciences (AREA)
  • General Engineering & Computer Science (AREA)
  • Pistons, Piston Rings, And Cylinders (AREA)

Description

Jan. 7, 1947. r w. DENNIS EXPANS ION ENGINE Filed June 10, 1944 2 Sheets-Sheet l ATTQRNEYS Jan.,7, 1947. 'w. DENNIS EXPANSION ENGINE Filed June 10, 1944 2 Sheets-Sheet 2 m. M T a V o Na w J .A Wm
Patented Jan. 7, 19 47 EXPANSION GINE Wolcott Dennis, Darien, Conn., assignor to Air Incorporated, New York,
Reduction Company,
a corporation of New York Application June 10, 1944, Serial Nor 539,761 I (Cl- 121-1) 3 Claims. 1
This invention relates to expansion engines for liquefaction systems and particularly to improvements aflording high efllciency in the operation of expansion engines at low temperatures.
In the liquefaction of gases by compression and subsequent expansion as for example in the well known Claude system, a part of the compressed and cooled gas is expanded in an engine with external work. Although engines'have been employed in such systems for many years, little improvement has been effected with respect to the efliciency of operation. It has been assumed that certain undesirable losses in the operation of the engine were unavoidable.
It is the oblect of the present invention to pro vide an engine adapted to afford a higher heat drop-efllciency than has been possible in engines heretofore available for expansion of gases at low temperatures.
Another object of the invention is to minimize the losses due to the introduction of heat through friction between the moving parts.
Another object of the invention is to provide for the maintenance of a temperature differential between the cold portion of the cylinder and the lubricated portion, by the action of the air or gas used to drive the engine.
A further object of the invention is the provision of a structure in which parts subject to wear can be replaced readily and economically so that the enginecan be maintained at its original high efiiciency and at relatively low cost.
Other objects and advantages of the invention will be apparent as it is better understood by reference to the following specification and the accompanying drawings, in which Fig. l is a vertical section illustrating one form of the invention; and
Fig. 2 is a similar view illustrating a modification of the engine.
Referring to the drawings, 5 indicates a suitable frame upon which a cylinder 6 is supported by bolts i. The cylinder is in two sections, the upper section 8 being secured to the lower section 6 by bolts 9 extending through the'flanges It and H. A rabbeted joint i2 is provided between the sections 6 and 8 of the cylinder to prevent escape of gas therethrough, and to insure accurate lineup of the two sections. The construction of the cylinder in the form indicated permits the removal of the lower section 6 which is subjected to wear and the replacement thereof at intervals so that the engine can be maintained at its maximum eiliciency.
A head 13 is secured ,to the upper end of the valves in order that gas under pressure introduced through the inlet l8 may be expanded in the cylinder and discharged through the exhaust passage H. The details ofsuch mechanisms are well known in the art and require no further description.
Within the cylinder-6 a piston 22 is supported and provided with piston rings 23 hearing against the internal surface of the cylinder 6 to prevent the escape or gas. A piston rod 24 is connected in any suitable manner, for example threadedly, as indicated at 25, to a. block 28 secured at the end of the piston 22. The piston rod 24 may be connected also to a conventional crosshead, crank,
and crankshaft (not shown) adapted to translate movement of the piston. Preferably the piston is filled with insulating material 21. A casing 28 is disposed about the cylinder sections 6 and 8 and the head l3 and is filled with insulating material 29 to reduce flow of heat from the external atmosphere through the walls of the cylinder.
As indicated in the drawing, the lower end of the piston 22 has adiameter affording a relatively close fit with the cylinder 0. 'The upper end of the piston has a reduced diameter aifording a substantial clearance between the piston and the upper section 8 of the cylinder. The clearance space is preferably tapered and extends beyond the limit of the stroke of the piston indicated by the line :c.r. The amount of radial clearance between the upper end of the piston and the section 8 of the cylinder may vary. Preferably the radial clearance at the top of the piston is approximately .010 inch and at the bottom of the reduced portion the radial clearance is approximately .005 inch. However, the radial clearance may vary from approximately .020 inch at the top of the piston to .002 inch at the bottom of the reduced section. v
The provision of an unusually large clearance space between the upper portion of the piston and the cylinder walls which are normally in contact with the cold expanded gases, serves two i useful purposes. First, all possibility of physical contact and the generation of heat by friction in this portion of the cylinder is eliminated and second, a heating effect is obtained in the lower part of this space by the action of the gas being used to operate the engine without in any way interfering with the attainment of high eiiiciency. This heating effect results when gas is admitted to the cylinder at the beginning of the working stroke with a resulting compression of the residual gas in the clearance space into the lower end of this space. In being compressed this gas becomes heated and transfers part of its heat of compression to the cylinder and piston walls near the bottom end of the clearance space. On expansion the gas in the clearance space cools but the cooling effect on the walls at the bottom of the space is much less than the previously noted heating effect because the mass of gas in contact with the previously heated walls is greatly reduced by the expansion process.
This heating effect has been repeatedlyobserved in the connecting piping between engine cylinders and indicator apparatus, and in engine parts having a single outlet connected to the cylinder and subject to fluctuating pressure. It is I here utilized for the purpose of establishing a large temperature gradient between the cold parts of the cylinder and the working parts which it is desirable to lubricate without difficulties due to freezing of oil or condensation of moisture. It is important of course that the cylinder section 8 be made of such material and of such thickness as to minimize heat conduction to the lower cylinder section-B in order to realize the most benefit from the heating effect. It is also desirableto extend the clearance space downward so that when the piston is in its upper position the space extends some distance below the lower limit of the piston travel. With this construction, the major portion of heat generated by compression of residual gas in the clearance space is transmitted to the cylinder 'wallsbelow the line .r-a:.
The use of a tapered piston permits the use of i a larger clearance space at the top. for a given clearance volume and reduces the possibility of contact between piston and cylinder at the top edge of the piston where contact is most apt to occur.
Referring to Fig. 2, the frame supports the lower section 3| of the cylinder through bolts 32.
The upper section 33 of the cylinder is secured to the lower section 3! by bolts 34 extending through flanges 35 and 3B. A rabbeted joint 31 is provided as in the previous embodiment of the invention. A head 38 is secured by bolts 39 to a flange 40 at the upper end of the section 33 of the cylinder and provides inlet and exhaust passages 4| and 42 terminating in valve seats 43 and 44. Valves 45 and 46 are actuated by mechanism. as in the preceding embodiment of the invention, to
control the flow of gas under pressure from the inlet passage 4| and withdrawal of the expanded gas through the exhaust passage 42.
A piston 41 is supported in the cylinder and provided with piston rings 48 to afford a gas-tight l fit. The piston is connected in the manner previously described to a piston rod 49 which in turn is connected to a conventional crosshead. crank and crankshaft to translate movement of the piston. The lower end of the piston has a substantiallytight lit in the section 3| of the cylinder. The upper end of the piston consists of a block 50 of heat insulating material secured to the lower portion by a bolt 5|. A liner 52 of heat insulating material is disposed within the upper section 33 of the cylinder.
As in the preceding embodiment of the invention, the upper section of the piston is of reduced diameter, affording clearance preferably though not necessarily tapered, extending beyond the line .E-.l! representing the limit of travel of the piston. The radial clearance between the piston and the cylinder wall should be within the limits hereinbefore specified. The same advantages are attained in this modification, and further advantages resulting from the elimination of heat flow from the warm end of the cylinder to the cold end as the result-of use of the insulating material at the upper end of the piston and in the wall of the upper section 33 of the cylinder.
It has been demonstrated that an engine constructed in accordance with the principles set forth has a heat drop efficiency of 88% under operating conditions such as exist in its application to a Claude cycle.
Various changes may be made in the construction and arrangement-of the apparatus within the scope of the appended claims, without departing from the invention or sacrificing the advantages thereof.
I claim:
1. An expansion engine for gases at relatively low temperatures comprising a cylinder, a cylinder head associated therewith including inlet and exhaust passages and valves controlling the delivery of gases to and from the cylinder and a piston movable in the cylinder and having a bearing surface closely fitting the internal surface of the cylinder at the end remote from the cylinder head, the other end of the piston having a reduced diameter affording a relatively narrow tapered radial clearance between the piston and cylinder walls, the maximum clearance being at the cylinder-head end of the piston, the length of that portion of the piston with reduced diameter being greater than the stroke of the piston.
2. An expansion engine for gases at relatively low temperatures comprising a cylinder, a cylinder head associated therewith including inlet and exhaust passages and valves controlling the delivery of gases to and from the cylinder, and a piston movable in the cylinder and having a bearing surface closely fitting the internal surface of the cylinder at the end remote from the cylinder head, the other end of the piston having a reduced diameter affording tapered radial clearance between the piston and cylinder walls, said clearance progressively decreasing from a maximum of .020 inch at the cylinder-head end of the piston to a minimum of .002 inch, the length of that portion of the piston with reduced diameter being greater than the stroke of the piston.
3. An expansion engine for gases at relatively low temperatures comprising a cylinder, a cylinder head associated therewith including inlet and exhaust passages and valves controlling the delivery of gases to and from the cylinder, and a piston movable in the cylinder and having a bearing surface closely fitting the internal surface of the cylinder at the and remote from the cylinder head, the other end of the piston having a reduced diameter affording tapered radial clearance between the piston and cylinder walls, said clearance progressively decreasing from a maximum of .010 inch at the cylinder-head end of the piston to a minimum of .005 inch, the length of that portion of the piston with reduced diameter being greater than the stroke of the piston.
v WOLCOT'I DENNIS.
US539761A 1944-06-10 1944-06-10 Expansion engine Expired - Lifetime US2413751A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
US539761A US2413751A (en) 1944-06-10 1944-06-10 Expansion engine

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US539761A US2413751A (en) 1944-06-10 1944-06-10 Expansion engine

Publications (1)

Publication Number Publication Date
US2413751A true US2413751A (en) 1947-01-07

Family

ID=24152528

Family Applications (1)

Application Number Title Priority Date Filing Date
US539761A Expired - Lifetime US2413751A (en) 1944-06-10 1944-06-10 Expansion engine

Country Status (1)

Country Link
US (1) US2413751A (en)

Cited By (18)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2591933A (en) * 1948-10-04 1952-04-08 Yuba Mfg Company Steam engine having a unitary valve actuator
US3150647A (en) * 1963-11-04 1964-09-29 Schreiber Gus Internal combustion engines
US3314337A (en) * 1964-01-31 1967-04-18 Dresser Ind Piston for an expansion engine
US3496720A (en) * 1967-02-25 1970-02-24 Philips Corp Hot-gas engine with solid cap on expansion piston
US3675738A (en) * 1970-03-02 1972-07-11 Vannevar Bush Engine sealing
US4024704A (en) * 1970-09-23 1977-05-24 Hudson Perry D Combustion products pressure generator continuous burner type and engines
US4543978A (en) * 1983-07-25 1985-10-01 Chicago Bridge & Iron Company Single tank for dual thermal energy storage with internal movable partition
US5284084A (en) * 1991-01-17 1994-02-08 Utex Industries, Inc. Light weight piston
US6457947B1 (en) * 1997-08-29 2002-10-01 Luk Fahrzeug-Hydraulik Gmbh & Co. Kg Piston compressor for refrigerant, with thermal insulation
US8656895B2 (en) * 2011-12-29 2014-02-25 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US8720317B2 (en) 2011-12-29 2014-05-13 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US8899192B2 (en) 2011-12-29 2014-12-02 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US9097203B2 (en) 2011-12-29 2015-08-04 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US9169797B2 (en) 2011-12-29 2015-10-27 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US9951714B2 (en) 2014-04-30 2018-04-24 Federal-Mogul Llc Steel piston with filled gallery
US10215229B2 (en) 2013-03-14 2019-02-26 Etagen, Inc. Mechanism for maintaining a clearance gap
US10985641B2 (en) 2018-07-24 2021-04-20 Mainspring Energy, Inc. Linear electromagnetic machine system with bearing housings having pressurized gas
US12255514B2 (en) 2021-07-30 2025-03-18 Mainspring Energy, Inc. Systems and methods for flexure-based bearing mounting

Non-Patent Citations (1)

* Cited by examiner, † Cited by third party
Title
None *

Cited By (23)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2591933A (en) * 1948-10-04 1952-04-08 Yuba Mfg Company Steam engine having a unitary valve actuator
US3150647A (en) * 1963-11-04 1964-09-29 Schreiber Gus Internal combustion engines
US3314337A (en) * 1964-01-31 1967-04-18 Dresser Ind Piston for an expansion engine
US3496720A (en) * 1967-02-25 1970-02-24 Philips Corp Hot-gas engine with solid cap on expansion piston
US3675738A (en) * 1970-03-02 1972-07-11 Vannevar Bush Engine sealing
US4024704A (en) * 1970-09-23 1977-05-24 Hudson Perry D Combustion products pressure generator continuous burner type and engines
US4543978A (en) * 1983-07-25 1985-10-01 Chicago Bridge & Iron Company Single tank for dual thermal energy storage with internal movable partition
US5284084A (en) * 1991-01-17 1994-02-08 Utex Industries, Inc. Light weight piston
US6457947B1 (en) * 1997-08-29 2002-10-01 Luk Fahrzeug-Hydraulik Gmbh & Co. Kg Piston compressor for refrigerant, with thermal insulation
US8720317B2 (en) 2011-12-29 2014-05-13 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
USRE49259E1 (en) 2011-12-29 2022-10-25 Mainspring Energy, Inc. Methods and systems for managing a clearance gap in a piston engine
US8770090B2 (en) 2011-12-29 2014-07-08 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US8899192B2 (en) 2011-12-29 2014-12-02 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US9004038B2 (en) 2011-12-29 2015-04-14 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US9097203B2 (en) 2011-12-29 2015-08-04 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US9169797B2 (en) 2011-12-29 2015-10-27 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US8656895B2 (en) * 2011-12-29 2014-02-25 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US10006401B2 (en) 2011-12-29 2018-06-26 Etagen, Inc. Methods and systems for managing a clearance gap in a piston engine
US10215229B2 (en) 2013-03-14 2019-02-26 Etagen, Inc. Mechanism for maintaining a clearance gap
US9951714B2 (en) 2014-04-30 2018-04-24 Federal-Mogul Llc Steel piston with filled gallery
US10985641B2 (en) 2018-07-24 2021-04-20 Mainspring Energy, Inc. Linear electromagnetic machine system with bearing housings having pressurized gas
US11616428B2 (en) 2018-07-24 2023-03-28 Mainspring Energy, Inc. Linear electromagnetic machine system
US12255514B2 (en) 2021-07-30 2025-03-18 Mainspring Energy, Inc. Systems and methods for flexure-based bearing mounting

Similar Documents

Publication Publication Date Title
US2413751A (en) Expansion engine
US3465651A (en) Composite pistons
US2410405A (en) Piston
US3074243A (en) Vortex water cooler
US2575394A (en) Reciprocating piston and cylinder mechanism
US3640082A (en) Cryogenic refrigerator cycle
US3128605A (en) Closed cycle cryogenic system
GB1456420A (en) Method of refrigeration which combines two thermodynamic cycles and a cryogenic machine for carrying out said method
US2239922A (en) Internal combustion engine
US1306865A (en) Prime moveb
KR20210063407A (en) Labyrinth Piston Compressor
US2239883A (en) Expansion engine
US2500085A (en) Engine
US2243541A (en) Compound compressor
US2439957A (en) Pump for liquefied gases
US2030509A (en) Process and apparatus for cooling gaseous mixtures
US3675738A (en) Engine sealing
US3274781A (en) Cryogenic expansion engine
US4226169A (en) Adjustable expandable cryogenic piston and ring
Collins Helium liquefier
GB1160607A (en) Expansion Engine for Cryogenic Refrigerators & Liquefiers & Apparatus Embodying the same
US1724553A (en) Fluid compressor
US940474A (en) Combustion-engine.
US2465633A (en) Gas seal for reciprocating rods
US1467503A (en) Cooling mechanism for compressors