GB805543A - Improvements in heating apparatus operated by means of a pulsatory combustion chamber - Google Patents
Improvements in heating apparatus operated by means of a pulsatory combustion chamberInfo
- Publication number
- GB805543A GB805543A GB31354/55A GB3135455A GB805543A GB 805543 A GB805543 A GB 805543A GB 31354/55 A GB31354/55 A GB 31354/55A GB 3135455 A GB3135455 A GB 3135455A GB 805543 A GB805543 A GB 805543A
- Authority
- GB
- United Kingdom
- Prior art keywords
- chamber
- injectors
- combustion
- fuel
- modification
- 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
- F23C—METHODS OR APPARATUS FOR COMBUSTION USING FLUID FUEL OR SOLID FUEL SUSPENDED IN A CARRIER GAS OR AIR
- F23C15/00—Apparatus in which combustion takes place in pulses influenced by acoustic resonance in a gas mass
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Air Supply (AREA)
Abstract
805,543. Combustion apparatus. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. Nov. 2, 1955 [Nov. 10, 1954,] No. 31354/55. Class 51 (1). [Also in Group XIII] Air required for the combustion of liquid fuel in a member 6, Fig. 1, and a chamber 8 of the apparatus shown is introduced from the atmosphere by intermittent gas puffs issuing from a nozzle 3 forming part of a combustion device comprising a chamber 1 in which fuel fed through an injector 4 is burnt in pulses, the necessary air entering through a duct 2. The liquid fuel is gravity fed through injectors 9, 10, 11, from a tank 13 and the gas issuing from the nozzle 3 comprises combustion products plus fuel from the injector 9. The injectors may be pump-fed and flame holders-such as 14, Fig. 2-may be placed downstream of them. In a modification, chamber 1, Fig. 2, has a 180 degree bend 15 such that any blow back through the duct 2 may be utilized to deliver air to the chamber 8. Additional injectors 10<SP>1</SP>, 11<SP>1</SP> are provided together with an additional member 6a and flame holders 14. In another modification, the member 6, Fig. 3, which receives the exhaust gas puffs is followed by successive members 6<SP>1</SP>, 6<SP>2</SP>. Injectors 9, 10, 10<SP>1</SP>, 10<SP>2</SP>, 11 are provided. A further embodiment having injectors 9, 9<SP>1</SP>, 10, 10<SP>1</SP>, 11, 11<SP>1</SP>, Fig. 4, has two combustion devices each discharging through a member 6, 6<SP>1</SP> into a chamber 8. In a modification of this construction, the devices discharge into a common member 6. In another modification, a steam generator has fuel injectors 9, 10, Fig. 6, and the chamber 8 accommodates water tubes 16 whilst passing through the member 6 are superheater tubes 16d. Feed water enters at 16b. In an application of the combustion apparatus to a boiler the water is heated in a tubular coil lining the wall of the member 6 and the chamber 8. The hot gases from the combustion apparatus may be used for space or fluid heating, combustion air heating or, in a boiler, for pre-heating feed water.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR805543X | 1954-11-10 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB805543A true GB805543A (en) | 1958-12-10 |
Family
ID=9251360
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31354/55A Expired GB805543A (en) | 1954-11-10 | 1955-11-02 | Improvements in heating apparatus operated by means of a pulsatory combustion chamber |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB805543A (en) |
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4033120A (en) * | 1975-08-21 | 1977-07-05 | Canadian Patents And Development Limited | Thrust augmenting fluid rectifier for a pulsed combustor |
FR2513357A1 (en) * | 1981-08-01 | 1983-03-25 | British Petroleum Co | IGNITION DEVICE, ESPECIALLY FOR A PULSATION BURNER |
CN1088452C (en) * | 1999-10-19 | 2002-07-31 | 成都开飞高能化学工业有限公司 | Process for preparing glycol antimony as polyester catalyst |
-
1955
- 1955-11-02 GB GB31354/55A patent/GB805543A/en not_active Expired
Cited By (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4033120A (en) * | 1975-08-21 | 1977-07-05 | Canadian Patents And Development Limited | Thrust augmenting fluid rectifier for a pulsed combustor |
FR2513357A1 (en) * | 1981-08-01 | 1983-03-25 | British Petroleum Co | IGNITION DEVICE, ESPECIALLY FOR A PULSATION BURNER |
CN1088452C (en) * | 1999-10-19 | 2002-07-31 | 成都开飞高能化学工业有限公司 | Process for preparing glycol antimony as polyester catalyst |
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