GB1382264A - Closed cycle vapour power generating system - Google Patents

Closed cycle vapour power generating system

Info

Publication number
GB1382264A
GB1382264A GB5581271A GB5581271A GB1382264A GB 1382264 A GB1382264 A GB 1382264A GB 5581271 A GB5581271 A GB 5581271A GB 5581271 A GB5581271 A GB 5581271A GB 1382264 A GB1382264 A GB 1382264A
Authority
GB
United Kingdom
Prior art keywords
condenser
tubes
vapour
shaft
annular
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
Application number
GB5581271A
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of GB1382264A publication Critical patent/GB1382264A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F28HEAT EXCHANGE IN GENERAL
    • F28BSTEAM OR VAPOUR CONDENSERS
    • F28B1/00Condensers in which the steam or vapour is separate from the cooling medium by walls, e.g. surface condenser
    • F28B1/06Condensers in which the steam or vapour is separate from the cooling medium by walls, e.g. surface condenser using air or other gas as the cooling medium
    • F28B1/08Condensers in which the steam or vapour is separate from the cooling medium by walls, e.g. surface condenser using air or other gas as the cooling medium employing moving walls
    • 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
    • F01K11/00Plants characterised by the engines being structurally combined with boilers or condensers
    • F01K11/04Plants characterised by the engines being structurally combined with boilers or condensers the boilers or condensers being rotated in use
    • 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
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F22STEAM GENERATION
    • F22BMETHODS OF STEAM GENERATION; STEAM BOILERS
    • F22B27/00Instantaneous or flash steam boilers
    • F22B27/12Instantaneous or flash steam boilers built-up from rotary heat-exchange elements, e.g. from tube assemblies

Landscapes

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

Abstract

1382264 Vapour power plant A MATVEY 1 Dec 1971 [1 Dec 1970] 55812/71 Heading F1Q [Also in Division F4] A closed cycle vapour power generation system is provided with a rotary condenser A including a tubular shaft 8 having an open end for receiving low pressure expanded vapour from an energy converter, an annular manifold 12 surrounding the opposite end portion of the tubular shaft and coaxial therewith, a multiplicity of spaced radially extending condenser tubes 9 arranged around the opposite end portion of the tubular shaft with their inner ends extending into open communication with the interior thereof and their outer ends extending into open communication with the interior 11 of the annular manifold 12 and means 19 to rotate the condenser. The condensate from the tubes 9 is thrown rapidly by centrifugal force into the annular space 11 from which it is directed into a multiplicity of radially extending pre-heater tubes 13, the outer ends of which are connected to an annular header tube 13a. The inner ends of superheater tubes 14 are connected to an annular collector tube 14a of the vapour generator B. The tubes are heated by hot gases from a burner (not shown) which is located in a combustion chamber E, shown in Fig. 3. This figure is a plan view of the condenser and vapour generator of Fig. 1. A vane type engine C is mounted to one side of the condenser-generator assembly and includes a vane cage or casing 63 having a cylindrical chamber 64 within which are fitted three concentric motor shafts 65, 66, 67. The shaft 65 carries at its left end radial vanes 68 mounted 120 degrees apart on a hub 69. The shaft 66 carries three radial vanes 70 mounted on the hub 71 and the shaft 67 carries three radial vanes 72. The application of the invention to an aircraft installation is described with reference to Fig. 16 (not shown). In this installation a turbine is employed and drives a propeller through reduction gearing. Working fluids that may be used include trichloroethylene carbon tetrachloride and various halogenated hydrocarbons. Reduction gears 20 (Fig. 1) may be used to drive auxiliary pumps as well as the condenser generator assembly. In a modification the combustion chamber E is replaced by a rotating combustion chamber which is supplied with fuel air mixture from a carburetter.
GB5581271A 1970-12-01 1971-12-01 Closed cycle vapour power generating system Expired GB1382264A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US9412270A 1970-12-01 1970-12-01

Publications (1)

Publication Number Publication Date
GB1382264A true GB1382264A (en) 1975-01-29

Family

ID=22243194

Family Applications (1)

Application Number Title Priority Date Filing Date
GB5581271A Expired GB1382264A (en) 1970-12-01 1971-12-01 Closed cycle vapour power generating system

Country Status (7)

Country Link
US (1) US3744938A (en)
CA (1) CA948861A (en)
DE (1) DE2159548A1 (en)
FR (1) FR2117243A5 (en)
GB (1) GB1382264A (en)
IT (1) IT945232B (en)
SE (1) SE387702B (en)

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2141179A (en) * 1983-05-07 1984-12-12 Roger Stuart Brierley Vapour turbine power plant
US6611068B2 (en) * 1998-05-19 2003-08-26 Sure Power Corporation Power system

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2607581B1 (en) * 1986-12-02 1989-01-13 Ancet Victor AMBIENT HEAT CONVERTER
US6257196B1 (en) * 1999-09-07 2001-07-10 Alfredo Alvarado Rotary disc engine
US20050217636A1 (en) * 2004-04-06 2005-10-06 Turner Mars S Toric pulsating continuous combustion rotary engine compressor or pump
US8308423B2 (en) * 2006-10-12 2012-11-13 United Technologies Corporation Variable area fan nozzle for accommodating a foreign object strike event
US7461626B2 (en) * 2006-12-21 2008-12-09 Ford Global Technologies, Llc Powertrain including a rotary IC engine and a continuously variable planetary gear unit
US7730869B2 (en) * 2007-04-13 2010-06-08 Yan Li Housing wheel engine
US9157323B2 (en) * 2009-12-07 2015-10-13 Mars Sterling Turner Oscillatory rotary engine
US11428156B2 (en) 2020-06-06 2022-08-30 Anatoli Stanetsky Rotary vane internal combustion engine

Family Cites Families (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1095034A (en) * 1912-10-29 1914-04-28 Antonio Sanchez Rotary internal-combustion engine.
DE533780C (en) * 1926-04-16 1931-09-18 Hans Simmon Tube heat exchanger
US2211292A (en) * 1938-11-07 1940-08-13 Gerald E Ryerson Split cycle internal combustion engine
FR873495A (en) * 1940-06-22 1942-07-09 Rotary Pallet Machine
US2349848A (en) * 1942-12-08 1944-05-30 Davids Robert Brewster Relative motion rotative mechanism
GB653935A (en) * 1947-11-06 1951-05-30 Motala Verkstad Ab Improvements in and relating to recuperative heat exchangers
US2576284A (en) * 1948-02-19 1951-11-27 Crocchi Piero Vapor electricity generator set
GB746350A (en) * 1954-07-16 1956-03-14 William Charles Berrisford Improvements relating to rotary engines
US3203405A (en) * 1961-02-03 1965-08-31 Sabet Huschang Rotary engine
SE206743C1 (en) * 1962-03-23 1966-08-09
US3396632A (en) * 1966-04-19 1968-08-13 Leblanc Michel Volumetric maching suitable for operation as pump, engine, or motor pump
US3476056A (en) * 1968-04-01 1969-11-04 Gen Motors Corp Pump with oscillating vanes

Cited By (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB2141179A (en) * 1983-05-07 1984-12-12 Roger Stuart Brierley Vapour turbine power plant
US6611068B2 (en) * 1998-05-19 2003-08-26 Sure Power Corporation Power system

Also Published As

Publication number Publication date
IT945232B (en) 1973-05-10
FR2117243A5 (en) 1972-07-21
SE387702B (en) 1976-09-13
DE2159548A1 (en) 1972-06-29
US3744938A (en) 1973-07-10
CA948861A (en) 1974-06-11

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Legal Events

Date Code Title Description
PS Patent sealed [section 19, patents act 1949]
PLNP Patent lapsed through nonpayment of renewal fees