GB723368A - Vehicle gas turbines - Google Patents
Vehicle gas turbinesInfo
- Publication number
- GB723368A GB723368A GB1572452A GB1572452A GB723368A GB 723368 A GB723368 A GB 723368A GB 1572452 A GB1572452 A GB 1572452A GB 1572452 A GB1572452 A GB 1572452A GB 723368 A GB723368 A GB 723368A
- Authority
- GB
- United Kingdom
- Prior art keywords
- coupling
- shaft
- compressor
- gearing
- turbine
- 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
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/36—Power transmission arrangements between the different shafts of the gas turbine plant, or between the gas-turbine plant and the power user
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
723,368. Gas-turbine plant. ROVER CO., Ltd. June 12, 1953 [June 23, 1952], No. 15724/52. Class 110 (3). [Also in Group XXXI] In a vehicle gas-turbine plant having a power turbine and a compressor turbine, the compressor has combined with it mechanism whereby the compressor may be driven by motion of the vehicle, the mechanism including a unidirectional clutch and a slipable friction coupling. Gases from the combustion chamber pass first to the compressor turbine g and then to the power turbine f, the latter driving the road wheels through the shaft and gearing k, m. A shaft q carrying a pinion r is driven from the gearing k and drives a shaft t through gearing u, s. The shaft t carries a disc v forming part of the slipable coupling, the other part of the coupling comprising an axially-slidable disc w which is loaded by a spring x. The two discs are contained in a hollow rotary member y secured to a sleeve 2. The sleeve is connected to a co-axial sleeve 4 by means of a unidirectional clutch 5, the sleeve 4 being connected to the compressor rotor o through gearing 6, 7. The discs v and w of the coupling are provided with rings 3 of friction material and the pressure of the spring x is adjustable so that the coupling can slip when a predetermined torque is exceeded. Alternatively, or in addition, the coupling may be adapted to slip when a predetermined speed of the shaft is reached, for example, by means of a centrifugal device 8, 9. Specification 617,856 is referred to.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1572452A GB723368A (en) | 1952-06-23 | 1952-06-23 | Vehicle gas turbines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1572452A GB723368A (en) | 1952-06-23 | 1952-06-23 | Vehicle gas turbines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB723368A true GB723368A (en) | 1955-02-09 |
Family
ID=10064357
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1572452A Expired GB723368A (en) | 1952-06-23 | 1952-06-23 | Vehicle gas turbines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB723368A (en) |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3045428A (en) * | 1960-07-06 | 1962-07-24 | Walter G Finch | Vortex gas turbine |
US3188807A (en) * | 1962-10-05 | 1965-06-15 | Bendix Corp | Variable torque transmitting mechanism for a re-expansion gas turbine |
US3237404A (en) * | 1965-05-03 | 1966-03-01 | Gen Motors Corp | Re-expansion gas turbine engine with power transfer between turbines |
US3266248A (en) * | 1964-03-06 | 1966-08-16 | Gen Motors Corp | Gas turbine engine fuel and power regulating system |
US4598542A (en) * | 1984-01-07 | 1986-07-08 | Rolls-Royce Limited | Gas turbine power plant |
GB2233394A (en) * | 1989-04-17 | 1991-01-09 | Gen Electric | A gas turbine engine rotor assembly |
-
1952
- 1952-06-23 GB GB1572452A patent/GB723368A/en not_active Expired
Cited By (7)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3045428A (en) * | 1960-07-06 | 1962-07-24 | Walter G Finch | Vortex gas turbine |
US3188807A (en) * | 1962-10-05 | 1965-06-15 | Bendix Corp | Variable torque transmitting mechanism for a re-expansion gas turbine |
US3266248A (en) * | 1964-03-06 | 1966-08-16 | Gen Motors Corp | Gas turbine engine fuel and power regulating system |
US3237404A (en) * | 1965-05-03 | 1966-03-01 | Gen Motors Corp | Re-expansion gas turbine engine with power transfer between turbines |
US4598542A (en) * | 1984-01-07 | 1986-07-08 | Rolls-Royce Limited | Gas turbine power plant |
GB2233394A (en) * | 1989-04-17 | 1991-01-09 | Gen Electric | A gas turbine engine rotor assembly |
GB2233394B (en) * | 1989-04-17 | 1994-02-09 | Gen Electric | A gas turbine engine rotor assembly |
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