GB1258762A - - Google Patents
Info
- Publication number
- GB1258762A GB1258762A GB1258762DA GB1258762A GB 1258762 A GB1258762 A GB 1258762A GB 1258762D A GB1258762D A GB 1258762DA GB 1258762 A GB1258762 A GB 1258762A
- Authority
- GB
- United Kingdom
- Prior art keywords
- forming
- passages
- jan
- recesses
- recess
- 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
- F23D—BURNERS
- F23D11/00—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space
- F23D11/36—Details, e.g. burner cooling means, noise reduction means
- F23D11/38—Nozzles; Cleaning devices therefor
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Nozzles (AREA)
Abstract
1,258,762. Making spray nozzles. JOSEPH LUCAS (INDUSTRIES) Ltd. 21 Jan., 1969 [4 Jan., 1968], No. 634/68. Heading B3A. [Also in Divisions B2 and F3-F4] A spray nozzle for producing a substantially flat fan-shaped spray pattern comprises a platelike member 17 having a recess 18, 19 on each face extending transversely of each other and forming a hole at their mid regions and a body 10, 11 in which the member is mounted, the body having two supply passages 16 communicating with opposite ends of one of the recesses. The nozzle is made by forming the plate-like member with the recesses and forming the body preferably from a flanged tube 10 in which is screwed an insert 11 which confines the plate-like member and a member 13 having two passages 16. The passages 16 are aligned with the ends of recess 18 on assembly.
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB63468 | 1968-01-04 |
Publications (1)
Publication Number | Publication Date |
---|---|
GB1258762A true GB1258762A (en) | 1971-12-30 |
Family
ID=9707793
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB1258762D Expired GB1258762A (en) | 1968-01-04 | 1968-01-04 |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB1258762A (en) |
Cited By (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0653591A1 (en) * | 1993-06-10 | 1995-05-17 | Nippon Sanso Corporation | Burner for liquid fuel |
EP2664848A4 (en) * | 2011-01-12 | 2018-03-21 | Mitsubishi Hitachi Power Systems, Ltd. | Spray nozzle, and combustion device having spray nozzle |
FR3068113A1 (en) * | 2017-06-27 | 2018-12-28 | Safran Helicopter Engines | FLAT JET FUEL INJECTOR FOR AN AIRCRAFT TURBOMACHINE |
US11230946B2 (en) | 2019-02-07 | 2022-01-25 | Raytheon Technologies Corporation | Non-uniform spray pattern oil delivery nozzle |
-
1968
- 1968-01-04 GB GB1258762D patent/GB1258762A/en not_active Expired
Cited By (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
EP0653591A1 (en) * | 1993-06-10 | 1995-05-17 | Nippon Sanso Corporation | Burner for liquid fuel |
EP0653591A4 (en) * | 1993-06-10 | 1997-06-04 | Nippon Oxygen Co Ltd | Burner for liquid fuel. |
EP2664848A4 (en) * | 2011-01-12 | 2018-03-21 | Mitsubishi Hitachi Power Systems, Ltd. | Spray nozzle, and combustion device having spray nozzle |
FR3068113A1 (en) * | 2017-06-27 | 2018-12-28 | Safran Helicopter Engines | FLAT JET FUEL INJECTOR FOR AN AIRCRAFT TURBOMACHINE |
WO2019001996A1 (en) | 2017-06-27 | 2019-01-03 | Safran Helicopter Engines | Flat-jet fuel injector for an aircraft turbine engine |
CN110832255A (en) * | 2017-06-27 | 2020-02-21 | 赛峰直升机发动机公司 | Flat jet fuel injector for aircraft turbine engine |
US11698188B2 (en) | 2017-06-27 | 2023-07-11 | Safran Helicopter Engines | Flat-jet fuel injector for an aircraft turbine engine |
US11230946B2 (en) | 2019-02-07 | 2022-01-25 | Raytheon Technologies Corporation | Non-uniform spray pattern oil delivery nozzle |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
PS | Patent sealed | ||
PCNP | Patent ceased through non-payment of renewal fee |