GB467504A - Improvements in and relating to fluid-pressure power installations - Google Patents

Improvements in and relating to fluid-pressure power installations

Info

Publication number
GB467504A
GB467504A GB3468035A GB3468035A GB467504A GB 467504 A GB467504 A GB 467504A GB 3468035 A GB3468035 A GB 3468035A GB 3468035 A GB3468035 A GB 3468035A GB 467504 A GB467504 A GB 467504A
Authority
GB
United Kingdom
Prior art keywords
engine
cylinder
exhaust
turbine
low
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
GB3468035A
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.)
WHITE S MARINE ENGINEERING COM
Original Assignee
WHITE S MARINE ENGINEERING COM
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 WHITE S MARINE ENGINEERING COM filed Critical WHITE S MARINE ENGINEERING COM
Priority to GB3468035A priority Critical patent/GB467504A/en
Publication of GB467504A publication Critical patent/GB467504A/en
Expired legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B17/00Reciprocating-piston machines or engines characterised by use of uniflow principle
    • F01B17/02Engines
    • F01B17/04Steam engines
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F01MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
    • F01BMACHINES OR ENGINES, IN GENERAL OR OF POSITIVE-DISPLACEMENT TYPE, e.g. STEAM ENGINES
    • F01B2170/00Steam engines, e.g. for locomotives or ships
    • F01B2170/04To-be-deleted with administrative transfer to parent group
    • F01B2170/0405To-be-deleted with administrative transfer to parent group
    • F01B2170/0435Compound machines with double or plural expansion; Auxiliaries driven by main engine

Landscapes

  • Engineering & Computer Science (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Engine Equipment That Uses Special Cycles (AREA)

Abstract

467,504. Reciprocating engines; marine power plant. WHITE, W. A., and WHITE'S MARINE ENGINEERING CO., Ltd. Dec. 13, 1935, No. 34680. [Classes 110 (iii) and 122 (iii)] Comprises a condensable, fluidpressure reciprocator with two or more stages, in which the crankangles are chosen to give a good mechanical balance, and superheating is effected between the stages so that the low-pressure cylinder does more work than a higher-pressure cylinder in the ratio of from 1À3 to 1 to 1À1 to 1. In a specific construction, the H.P. cranks are at 55‹ and the L.P. cranks at 108‹ apart. In the double-compound engine shown, which may be used in the power-plant described in Specification 362,255, high and low-pressure cylinders A<1>, A<2>, B<1>, B<2> are arranged as shown. The low-pressure cylinders are adapted to do more work than the high-pressure cylinders in the ratio of 1À3 to 1. The H.P. exhaust is superheated by superheated steam before entry into the L.P. cylinder. The reheater comprises heat-transferring units C<1>, C<2> with internal tubes c secured to the backs of the engine and fed with superheated steam through a fitting D, the steam passing through a pipe e to the H.P. valve chests. The H.P. cylinders exhaust, through pipes f, f and the heaters C<1>, C<2> to the L.P. chests b<1>, b<2> respectively. The L.P. cylinder's exhaust from pipes i, i<1> passes through a pipe k to the turbine, or by a change-over-valve to the condenser. The reheater tubes may be bent to conform to the plan of the engine. Instead of a three power-shaft arrangement as described in the above Specification, the crankshaft may drive directly the propeller shaft, and the turbine geared to it. Alternatively, the turbine may drive the auxiliaries. The reciprocating-engine may be used alone.
GB3468035A 1935-12-13 1935-12-13 Improvements in and relating to fluid-pressure power installations Expired GB467504A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3468035A GB467504A (en) 1935-12-13 1935-12-13 Improvements in and relating to fluid-pressure power installations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3468035A GB467504A (en) 1935-12-13 1935-12-13 Improvements in and relating to fluid-pressure power installations

Publications (1)

Publication Number Publication Date
GB467504A true GB467504A (en) 1937-06-14

Family

ID=10368633

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3468035A Expired GB467504A (en) 1935-12-13 1935-12-13 Improvements in and relating to fluid-pressure power installations

Country Status (1)

Country Link
GB (1) GB467504A (en)

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