GB527612A - A combined gas injection valve and ignition apparatus for internal combustion engines - Google Patents
A combined gas injection valve and ignition apparatus for internal combustion enginesInfo
- Publication number
- GB527612A GB527612A GB1187139A GB1187139A GB527612A GB 527612 A GB527612 A GB 527612A GB 1187139 A GB1187139 A GB 1187139A GB 1187139 A GB1187139 A GB 1187139A GB 527612 A GB527612 A GB 527612A
- Authority
- GB
- United Kingdom
- Prior art keywords
- stem
- valve
- gas
- supplied
- baffle
- 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
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
Abstract
527,612. Gaseous-fuel injectors. TOWNSHEND, E. F. R. April 20, 1939, No. 11871. [Class 7 (iii)] In a compressed-gas fuel injector for internal-combustion engines, means are provided at the injection orifice for establishing a hot zone of sufficiently high temperature to initiate ignition. Gas supplied under pressure through passages 28, 26, 24, 25, 23 is injected through an orifice 4 when a valve 2 is lifted by pressure supplied at 14 from a fuel pump to a piston 8 on the valve stem 1. The gas pressure raises a serrated baffle 46 from a conical seating on a flame plate 45, which is formed with passages 47 through which air is drawn from the compressed charge in the cylinder, to mix with ' the gas passing through the venturishaped passage in the plate 45. The valve 2 is closed by a spring 17, and the baffle 46 is closed by springs 39, 40 on its stem 41. For providing the hot igniting-zone, a terminal 35 is connected in series with an inductive resistance, dynamo &c. and carries a disc 34 bearing on the flange 38 of a cup 37 on which rest the springs 39, 40 on the stem 41, so that when the baffle 46 is moved downwards away from the flame plate 45, an electric arc is formed between them. High-tension ignition may be used with sparking-points adjacent the injection nozzle ; or an incandescent electric igniter may be employed. Lubricating-oil may be supplied to an annular recess 20 around the valve stem 1, and another annular recess 19 above this is connected to atmosphere in order to prevent gas leaking along the stem from reaching the hydraulic chamber 13 around the piston 8. Excess fuel supplied by the'pump to this chamber passes back to the tank through a relief valve.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1187139A GB527612A (en) | 1939-04-20 | 1939-04-20 | A combined gas injection valve and ignition apparatus for internal combustion engines |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB1187139A GB527612A (en) | 1939-04-20 | 1939-04-20 | A combined gas injection valve and ignition apparatus for internal combustion engines |
Publications (1)
Publication Number | Publication Date |
---|---|
GB527612A true GB527612A (en) | 1940-10-11 |
Family
ID=9994188
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1187139A Expired GB527612A (en) | 1939-04-20 | 1939-04-20 | A combined gas injection valve and ignition apparatus for internal combustion engines |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB527612A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112610359A (en) * | 2020-12-28 | 2021-04-06 | 中国航天空气动力技术研究院 | Solid rocket engine fixing device of embedded installation |
CN113910949A (en) * | 2021-10-25 | 2022-01-11 | 俞朝水 | Buried charging pile for biogas power generation |
-
1939
- 1939-04-20 GB GB1187139A patent/GB527612A/en not_active Expired
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
CN112610359A (en) * | 2020-12-28 | 2021-04-06 | 中国航天空气动力技术研究院 | Solid rocket engine fixing device of embedded installation |
CN112610359B (en) * | 2020-12-28 | 2022-02-22 | 中国航天空气动力技术研究院 | Solid rocket engine fixing device of embedded installation |
CN113910949A (en) * | 2021-10-25 | 2022-01-11 | 俞朝水 | Buried charging pile for biogas power generation |
CN113910949B (en) * | 2021-10-25 | 2023-09-01 | 深圳市鸿嘉利新能源有限公司 | Bury formula marsh gas electricity generation with filling electric pile |
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