GB696131A - Improvements in liquid fuel supply systems for gas turbine engines - Google Patents
Improvements in liquid fuel supply systems for gas turbine enginesInfo
- Publication number
- GB696131A GB696131A GB1620750A GB1620750A GB696131A GB 696131 A GB696131 A GB 696131A GB 1620750 A GB1620750 A GB 1620750A GB 1620750 A GB1620750 A GB 1620750A GB 696131 A GB696131 A GB 696131A
- Authority
- GB
- United Kingdom
- Prior art keywords
- gas turbine
- pressure difference
- fuel supply
- liquid fuel
- restriction
- 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
- F02C7/22—Fuel supply systems
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Physical Or Chemical Processes And Apparatus (AREA)
Abstract
696,131. Gas turbine plant. DOWTY EQUIPMENT, Ltd. June 25, 1951 [June 28, 1950], No. 16207/50. Class 110(iii) [Also in Groups XI and XXIX] In a gas turbine.liquid fuel supply system in which the rate of fuel flow to the burners is controlled by means responsive to the pressure difference across a restriction in the burner delivery line, the restriction comprises a plurality of small area passages arranged in parallel such that the flow rate is substantially directly proportional to the pressure difference. The restriction may be fabricated from corrugated strip material, from a plurality of rods or wires clamped together or by porous metal or other porous material. The pores of the metal or other material should be as large as possible provided.that the Reynolds number is such that it gives a substantially linear relationship between the flow and pressure difference.
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1620750A GB696131A (en) | 1950-06-28 | 1950-06-28 | Improvements in liquid fuel supply systems for gas turbine engines |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1620750A GB696131A (en) | 1950-06-28 | 1950-06-28 | Improvements in liquid fuel supply systems for gas turbine engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB696131A true GB696131A (en) | 1953-08-26 |
Family
ID=10073093
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1620750A Expired GB696131A (en) | 1950-06-28 | 1950-06-28 | Improvements in liquid fuel supply systems for gas turbine engines |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB696131A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2152238A (en) * | 1983-12-12 | 1985-07-31 | Gen Electric | Apparatus and method for degrading antimistic fuel |
-
1950
- 1950-06-28 GB GB1620750A patent/GB696131A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB2152238A (en) * | 1983-12-12 | 1985-07-31 | Gen Electric | Apparatus and method for degrading antimistic fuel |
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