GB859805A - Improvements relating to gas turbine engine combustion systems - Google Patents
Improvements relating to gas turbine engine combustion systemsInfo
- Publication number
- GB859805A GB859805A GB24270/59A GB2427059A GB859805A GB 859805 A GB859805 A GB 859805A GB 24270/59 A GB24270/59 A GB 24270/59A GB 2427059 A GB2427059 A GB 2427059A GB 859805 A GB859805 A GB 859805A
- Authority
- GB
- United Kingdom
- Prior art keywords
- plug
- boss
- flame tube
- flange
- secured
- 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
- F23—COMBUSTION APPARATUS; COMBUSTION PROCESSES
- F23R—GENERATING COMBUSTION PRODUCTS OF HIGH PRESSURE OR HIGH VELOCITY, e.g. GAS-TURBINE COMBUSTION CHAMBERS
- F23R3/00—Continuous combustion chambers using liquid or gaseous fuel
- F23R3/42—Continuous combustion chambers using liquid or gaseous fuel characterised by the arrangement or form of the flame tubes or combustion chambers
- F23R3/60—Support structures; Attaching or mounting means
-
- 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
- F02C7/26—Starting; Ignition
- F02C7/264—Ignition
- F02C7/266—Electric
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Pressure-Spray And Ultrasonic-Wave- Spray Burners (AREA)
Abstract
859,805. Generating combustion products under pressure. GENERAL MOTORS CORPORATION. July 15, 1959 [July 21, 1958], No. 24270/59. Class 51 (1). In gas turbine engine combustion equipment of the kind comprising a series of flame tubes disposed within an annular casing, each flame tube has at its upstream end a boss having an aperture to receive an actual or a dummy igniter plug, the plug and the boss having inter-engageable parts so arranged that the plug can be inserted through the aperture and may then be rotated to a position in which the parts can engage so that the flame tube can then be supported on the plug and the plug cannot be withdrawn. The object of the invention is to support the flame tubes temporarily pending the insertion of the fuel injector nozzles. The flame tube 22 is disposed within an annular casing, the outer wall of which is shown at 12, being normally supported at its upstream end by means of the fuel injector nozzle 42 engaging a central opening 38 in the flame tube end wall 28, and at its downstream end by means of the transition section 29 which engages within an annular sleeve 27 secured to the flame tube, the transition section being secured at its upstream end to the outer casing 20 by means of supports 31. A hollow boss member 50 is secured at the upstream end of the flame tube by means of a sheet metal plate 48, the radially inner end of the boss being formed with a transverse slot 54 which provides two ledge portions 55. The igniter plug 56 is provided with a flange 64 on its stem portion 62, the flange being of circular form with two side pieces cut away to provide a pair of parallel straight edges 66, the flange being so dimensioned that it may pass through the boss 50 when the edges 66 are disposed parallel to the sides of the slot 54. To support the flame tube therefore before the fuel injector nozzle 42 is fitted, the igniter plug 56 is entered through the opening 58 in the outer casing 12, through the aperture in the boss 50 and then through the opening 60 in the flame tube end wall 28, the plug being disposed so that the flats 66 on the flange 64 are parallel to the sides of the slot 54 in the boss 50 to permit this. The igniter plug is then turned through 90 degrees so that openings in the plug mounting plate 70 align with openings in the plate 76 fixed to the outer casing 12, the plug being secured in position by means of bolts 78. In this position the ledges 55 of the boss 50 rest on the curved end portions 68 of the flange 64 whereby the flame tube is temporarily supported on the igniter plug. Upon insertion of the injector nozzle 42, the flame tube will be displaced slightly so that the boss 50 is lifted off the flange 64, as shown in Fig. 1.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
US859805XA | 1958-07-21 | 1958-07-21 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB859805A true GB859805A (en) | 1961-01-25 |
Family
ID=22195196
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB24270/59A Expired GB859805A (en) | 1958-07-21 | 1959-07-15 | Improvements relating to gas turbine engine combustion systems |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB859805A (en) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2900976A1 (en) * | 2006-05-11 | 2007-11-16 | Snecma Sa | Spark plug mounting method for gas turbine engine, involves correcting alignment difference on adapter so that after mounting clearance is more than preset minimal value, mounting sparkplug on adapter, and fixing adapter on case |
FR2951505A1 (en) * | 2009-10-20 | 2011-04-22 | Snecma | Spark plug arrangement for combustion chamber of gas turbine engine, has complementary anti-rotation units cooperating with anti-rotation units of sliding cross member, and annular projection part arranged inside sliding cross member |
FR2957975A1 (en) * | 2010-03-24 | 2011-09-30 | Snecma | Spark plug positioning device for combustion chamber of engine in airplane, has vent including support plane for receiving contact ring, where support plane is defined by flange whose portion is in straight or concave shape |
CN105423344A (en) * | 2016-01-12 | 2016-03-23 | 西北工业大学 | Flame tube structure of combustion chamber of ground gas turbine |
WO2020128292A1 (en) * | 2018-12-21 | 2020-06-25 | Turbotech | Turbomachine combustion chamber |
-
1959
- 1959-07-15 GB GB24270/59A patent/GB859805A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2900976A1 (en) * | 2006-05-11 | 2007-11-16 | Snecma Sa | Spark plug mounting method for gas turbine engine, involves correcting alignment difference on adapter so that after mounting clearance is more than preset minimal value, mounting sparkplug on adapter, and fixing adapter on case |
FR2951505A1 (en) * | 2009-10-20 | 2011-04-22 | Snecma | Spark plug arrangement for combustion chamber of gas turbine engine, has complementary anti-rotation units cooperating with anti-rotation units of sliding cross member, and annular projection part arranged inside sliding cross member |
FR2957975A1 (en) * | 2010-03-24 | 2011-09-30 | Snecma | Spark plug positioning device for combustion chamber of engine in airplane, has vent including support plane for receiving contact ring, where support plane is defined by flange whose portion is in straight or concave shape |
CN105423344A (en) * | 2016-01-12 | 2016-03-23 | 西北工业大学 | Flame tube structure of combustion chamber of ground gas turbine |
CN105423344B (en) * | 2016-01-12 | 2017-12-29 | 西北工业大学 | A kind of flame tube structure of ground combustion machine combustion chamber |
WO2020128292A1 (en) * | 2018-12-21 | 2020-06-25 | Turbotech | Turbomachine combustion chamber |
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