GB719585A - An improved atomising injector for liquids - Google Patents
An improved atomising injector for liquidsInfo
- Publication number
- GB719585A GB719585A GB18419/52A GB1841952A GB719585A GB 719585 A GB719585 A GB 719585A GB 18419/52 A GB18419/52 A GB 18419/52A GB 1841952 A GB1841952 A GB 1841952A GB 719585 A GB719585 A GB 719585A
- Authority
- GB
- United Kingdom
- Prior art keywords
- axis
- fuel
- chambers
- injector
- july
- 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
- F23D11/24—Burners using a direct spraying action of liquid droplets or vaporised liquid into the combustion space by pressurisation of the fuel before a nozzle through which it is sprayed by a substantial pressure reduction into a space
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Fuel-Injection Apparatus (AREA)
Abstract
719,585. Spray-producers. SOC. NATIONALE D'ETUDE ET DE CONSTRUCTION DE MOTEURS D'AVIATION. July 21, 1952 [July 26, 1951], No. 18419/52. Class 69 (3). [Also in Groups XI and XXVII] An atomizing injector for liquid, e.g. liquid fuel, for use in a duct through which air is circulated, comprises a generally cylindrical body 1 adapted to be mounted with its axis generally parallel to that of the air duct, and containing an axial fuel intake cavity 3 from which the fuel passes through passages 7 to cylindrical chambers 6 annularly disposed around the cavity 3 with their axes generally perpendicular to the axis of the body 1, each passage 7 being inclined to the axis of and eccentric relatively to a chamber 6, and the fuel is discharged through atomizing holes 9 as conical sprays directed radially 'with respect to the axis of the body 1. The holes 9 are formed in a sleeve 8 closing the outer ends of the chambers 6 and fitted over a reduced portion of the body 1, being locked against a shoulder 10 on the latter by a cap nut 11 screwed onto an extension 1b of the body. In a modified construction the chambers 6 and orifices 9 are arranged in two rings axially spaced along the injector body 1.
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| FR719585X | 1951-07-26 |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB719585A true GB719585A (en) | 1954-12-01 |
Family
ID=9091156
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB18419/52A Expired GB719585A (en) | 1951-07-26 | 1952-07-21 | An improved atomising injector for liquids |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB719585A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3991940A (en) * | 1975-04-14 | 1976-11-16 | Aga Aktiebolag | Oxygen-fuel gas burner nozzle |
-
1952
- 1952-07-21 GB GB18419/52A patent/GB719585A/en not_active Expired
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| US3991940A (en) * | 1975-04-14 | 1976-11-16 | Aga Aktiebolag | Oxygen-fuel gas burner nozzle |
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