GB849131A - Improvements in or relating to fuel systems for propeller-driving gas turbine engines - Google Patents
Improvements in or relating to fuel systems for propeller-driving gas turbine enginesInfo
- Publication number
- GB849131A GB849131A GB2272758A GB2272758A GB849131A GB 849131 A GB849131 A GB 849131A GB 2272758 A GB2272758 A GB 2272758A GB 2272758 A GB2272758 A GB 2272758A GB 849131 A GB849131 A GB 849131A
- Authority
- GB
- United Kingdom
- Prior art keywords
- throttle
- propeller
- gas turbine
- relating
- turbine engines
- 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
- 239000000446 fuel Substances 0.000 title abstract 5
- 230000002441 reversible effect Effects 0.000 abstract 3
- 238000002485 combustion reaction Methods 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D47/00—Equipment not otherwise provided for
Landscapes
- Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Output Control And Ontrol Of Special Type Engine (AREA)
Abstract
849,131. Driving variable pitch propellers. ROLLS-ROYCE Ltd., and LUCAS (INDUSTRIES) Ltd., J. June 18, 1959 [July 15, 1958], No. 22727/58. Class 114. [Also in Groups XXVI and XXIX] A fuel system for a gas turbine engine 15 driving a reversible pitch propeller 18 comprises two throttle valves 54, 67 arranged in parallel passages in a pressure fuel line 26, 29 leading to combustion equipment 13 of the engine, which throttles are connected via pinions 57, 70 to a pilot's control 73 so that one throttle (the forward throttle 54) is operative to vary the fuel supply during normal forward thrust operation and the other throttle (the reverse throttle 67) is operative to vary the fuel supply during operation with the propeller in reverse pitch.
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2272758A GB849131A (en) | 1958-07-15 | 1958-07-15 | Improvements in or relating to fuel systems for propeller-driving gas turbine engines |
BE588614A BE588614A (en) | 1958-07-15 | 1960-03-14 | Improvements to the fuel systems of gas turbine engines operating a propeller. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB2272758A GB849131A (en) | 1958-07-15 | 1958-07-15 | Improvements in or relating to fuel systems for propeller-driving gas turbine engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB849131A true GB849131A (en) | 1960-09-21 |
Family
ID=10184141
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB2272758A Expired GB849131A (en) | 1958-07-15 | 1958-07-15 | Improvements in or relating to fuel systems for propeller-driving gas turbine engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB849131A (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10316689B2 (en) | 2016-08-22 | 2019-06-11 | Rolls-Royce Corporation | Gas turbine engine health monitoring system with shaft-twist sensors |
-
1958
- 1958-07-15 GB GB2272758A patent/GB849131A/en not_active Expired
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US10316689B2 (en) | 2016-08-22 | 2019-06-11 | Rolls-Royce Corporation | Gas turbine engine health monitoring system with shaft-twist sensors |
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