GB706743A - Improvements relating to mechanism for controlling the speed of prime movers - Google Patents
Improvements relating to mechanism for controlling the speed of prime moversInfo
- Publication number
- GB706743A GB706743A GB4439/52A GB443952A GB706743A GB 706743 A GB706743 A GB 706743A GB 4439/52 A GB4439/52 A GB 4439/52A GB 443952 A GB443952 A GB 443952A GB 706743 A GB706743 A GB 706743A
- Authority
- GB
- United Kingdom
- Prior art keywords
- pendulum
- engine
- speed
- spring
- pressure difference
- 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
Links
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F01—MACHINES OR ENGINES IN GENERAL; ENGINE PLANTS IN GENERAL; STEAM ENGINES
- F01D—NON-POSITIVE DISPLACEMENT MACHINES OR ENGINES, e.g. STEAM TURBINES
- F01D21/00—Shutting-down of machines or engines, e.g. in emergency; Regulating, controlling, or safety means not otherwise provided for
- F01D21/02—Shutting-down responsive to overspeed
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
- Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
- Y02T50/00—Aeronautics or air transport
- Y02T50/60—Efficient propulsion technologies, e.g. for aircraft
Landscapes
- Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Supercharger (AREA)
Abstract
706,743. Speed governor; gas turbine plant. S. U. CARBURETTER CO., Ltd., and ROLLSROYCE, Ltd. Feb. 2, 1953 [Feb. 20, 1951], No. 4439/32. Classes 57 and 110 (3). [Also in Group XXIX] A speed-limiting governor contains an osci!- latable control device 2, Fig. 3, comprising an elastically-constrained pendulum with a liquidfilled bob divided into two chambers 5, 5A connected by means permitting transference of liquid to take place from one chamber to the other more readily in one direction than in the opposite direction to produce a pressure difference which is applied to a pressure-responsive system arranged to control the power regulator of a prime mover. Periodic impulsers, of frequency correlated with the instantaneous rotational speed of the prime mover, are applied to the pendulum which reacts to them at resonant response only when their frequency is close to, or at, the value which corresponds to the predetermined maximum speed of the prime mover which may be an internal-combustion engine, gas turbine, steam reciprocating engine or steam turbine. The impulse may be derived from a magnet 12 rotated by the engine and co-operating with a pole-piece 13. At resonant frequency the liquid, which may be mercury, surges through a venturi duct 6 or a non-return valve to produce the pressure difference which is communicated by ducts 9A either to bellows or capsules connected with opposite ends of a first-order lever linked to the engine regulator or to a spring-loaded diaphragm 86 in a servo mechanism. The diaphragm tilts a flexibly-mounted bar 90 to open a ball valve 94 which allows fuel to flow from a centrifugal pump 79 to a cylinder 98 provided with an outlet restrictor 101. A spring-loaded piston 99, displaced by the fuel, restricts the opening in a throttle 82 and hence reduces the speed of the engine. The chambers 5, 5A have distensible walls, and to prevent the possibility of the engine accelerating rapidly past the resonant frequency of the governor, a spring- loaded piston 14 may be provided so that when the pendulum is initially set into vibration the pressure difference acting through ports 16, 17 raises the piston against its spring and increases the resonant frequency. Alternatively, this result may be achieved by providing rigid cam surfaces to constrain the swing of the pendulum. The piston 14 may be controlled by a separate venturi duct. Figs. 8A and 9 show a torsional pendulum in which two chambers 46, 47 connected by venturi ducts 45 produce a pressure difference across a diaphragm 50 connected by a push rod 52 to the engine. Two spring-loaded piston 54, which are displaced inwardly by the pressure difference once the pendulum starts to vibrate, may be provided to increase the resonant frequency. Alternatively, the pendulum shaft may have splines to co-operate with cam surfaces. The pendulum may be excited by a rotating magnet 12 or by a pair of air-discharge pipes which are rotated through gearing from the engine and directed onto inclined vanes on the pendulum periphery.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4439/52A GB706743A (en) | 1952-02-20 | 1952-02-20 | Improvements relating to mechanism for controlling the speed of prime movers |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB4439/52A GB706743A (en) | 1952-02-20 | 1952-02-20 | Improvements relating to mechanism for controlling the speed of prime movers |
Publications (1)
Publication Number | Publication Date |
---|---|
GB706743A true GB706743A (en) | 1954-04-07 |
Family
ID=9777206
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB4439/52A Expired GB706743A (en) | 1952-02-20 | 1952-02-20 | Improvements relating to mechanism for controlling the speed of prime movers |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB706743A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
-
1952
- 1952-02-20 GB GB4439/52A patent/GB706743A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US8499874B2 (en) | 2009-05-12 | 2013-08-06 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8708083B2 (en) | 2009-05-12 | 2014-04-29 | Icr Turbine Engine Corporation | Gas turbine energy storage and conversion system |
US8866334B2 (en) | 2010-03-02 | 2014-10-21 | Icr Turbine Engine Corporation | Dispatchable power from a renewable energy facility |
US8984895B2 (en) | 2010-07-09 | 2015-03-24 | Icr Turbine Engine Corporation | Metallic ceramic spool for a gas turbine engine |
US8669670B2 (en) | 2010-09-03 | 2014-03-11 | Icr Turbine Engine Corporation | Gas turbine engine configurations |
US9051873B2 (en) | 2011-05-20 | 2015-06-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine shaft attachment |
US10094288B2 (en) | 2012-07-24 | 2018-10-09 | Icr Turbine Engine Corporation | Ceramic-to-metal turbine volute attachment for a gas turbine engine |
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