GB1497401A - Turbo-brakes - Google Patents
Turbo-brakesInfo
- Publication number
- GB1497401A GB1497401A GB3219474A GB3219474A GB1497401A GB 1497401 A GB1497401 A GB 1497401A GB 3219474 A GB3219474 A GB 3219474A GB 3219474 A GB3219474 A GB 3219474A GB 1497401 A GB1497401 A GB 1497401A
- Authority
- GB
- United Kingdom
- Prior art keywords
- compressor
- turbo
- brake
- july
- brakes
- 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
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16D—COUPLINGS FOR TRANSMITTING ROTATION; CLUTCHES; BRAKES
- F16D57/00—Liquid-resistance brakes; Brakes using the internal friction of fluids or fluid-like media, e.g. powders
- F16D57/02—Liquid-resistance brakes; Brakes using the internal friction of fluids or fluid-like media, e.g. powders with blades or like members braked by the fluid
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Compressors, Vaccum Pumps And Other Relevant Systems (AREA)
Abstract
1497401 Turbo-brakes DEFENCE SECRE- TARY OF STATE FOR 8 July 1975 [19 July 1974] 32194/74 Heading F2E A turbo-brake comprises a rotary gas compressor the discharge from which is directed so as to oppose rotation of a bladed or pocketed rotary brake connected to the compressor. As shown a single rotor 1 is formed with compressor blades 9 and pockets 13, air from the compressor passing to chamber 4 and thence via nozzles 7 tangentially against pockets 13. The brake may be applied to a turbine driven road vehicle, the rotor shaft 6 being connected to the output shaft of the power turbine via a hydraulic clutch and step-up gearing (Fig. 2, not shown), or to a turbine driven helicopter.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3219474A GB1497401A (en) | 1975-07-08 | 1975-07-08 | Turbo-brakes |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB3219474A GB1497401A (en) | 1975-07-08 | 1975-07-08 | Turbo-brakes |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1497401A true GB1497401A (en) | 1978-01-12 |
Family
ID=10334760
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB3219474A Expired GB1497401A (en) | 1975-07-08 | 1975-07-08 | Turbo-brakes |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1497401A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4373618A (en) * | 1979-08-21 | 1983-02-15 | Ford Motor Company | Reverse speed shift device for a motor vehicle change-speed gearbox |
-
1975
- 1975-07-08 GB GB3219474A patent/GB1497401A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4373618A (en) * | 1979-08-21 | 1983-02-15 | Ford Motor Company | Reverse speed shift device for a motor vehicle change-speed gearbox |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |