GB529450A - Improvements in or relating to air-intake means for internal-combustion engines of aircraft - Google Patents
Improvements in or relating to air-intake means for internal-combustion engines of aircraftInfo
- Publication number
- GB529450A GB529450A GB1502339A GB1502339A GB529450A GB 529450 A GB529450 A GB 529450A GB 1502339 A GB1502339 A GB 1502339A GB 1502339 A GB1502339 A GB 1502339A GB 529450 A GB529450 A GB 529450A
- Authority
- GB
- United Kingdom
- Prior art keywords
- air
- tunnel
- intake
- aircraft
- stream
- 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
- 238000002485 combustion reaction Methods 0.000 title 1
- 230000015572 biosynthetic process Effects 0.000 abstract 1
- 239000000428 dust Substances 0.000 abstract 1
- 238000000926 separation method Methods 0.000 abstract 1
- 239000007921 spray Substances 0.000 abstract 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENT OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D33/00—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/02—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes
- B64D2033/0266—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants
- B64D2033/028—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of power plants for piston engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Separating Particles In Gases By Inertia (AREA)
Abstract
529,450. Spray carburetters. ELLIOTT, A. G. May 19, 1939, No. 15023. [Class 7 (iii)] In order to avoid the formation of ice or snow in the air intakes, particularly of aircraft engines, and to assist in the separation of dust &c. from the air supplied to the engines, a tunnel 12, open at both ends, is arranged so as to pass through it an air-stream in excess of that required by the engine, the air-inlet pipe 15 having its intake opening 16 situated within the tunnel so that air from the airstream has to undergo a change in its direction of motion in order to enter the intake opening. The tunnel preferably diverges at its inlet end 13 and converges at its outlet end 14, the air intake 16 being placed at the point of maximum air pressure. The end of the intake 16 may lie across the tunnel, facing the outlet 14 ; or it may be oblique, but still directed rearwardly ; or it may be parallel to the air-stream, with a projecting lip at its front end. The air-inlet pipe 15 is preferably combined with an aircleaner, connected to the carburetter by a self-detachable connection as described in Specification 502,496, [Group XXVIII].
Priority Applications (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1502339A GB529450A (en) | 1939-05-19 | 1939-05-19 | Improvements in or relating to air-intake means for internal-combustion engines of aircraft |
Applications Claiming Priority (1)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB1502339A GB529450A (en) | 1939-05-19 | 1939-05-19 | Improvements in or relating to air-intake means for internal-combustion engines of aircraft |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| GB529450A true GB529450A (en) | 1940-11-21 |
Family
ID=10051693
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| GB1502339A Expired GB529450A (en) | 1939-05-19 | 1939-05-19 | Improvements in or relating to air-intake means for internal-combustion engines of aircraft |
Country Status (1)
| Country | Link |
|---|---|
| GB (1) | GB529450A (en) |
Cited By (1)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114813156A (en) * | 2022-06-27 | 2022-07-29 | 中国航发四川燃气涡轮研究院 | High-altitude test bed cold-hot immersion test device and method for turboshaft engine |
-
1939
- 1939-05-19 GB GB1502339A patent/GB529450A/en not_active Expired
Cited By (2)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| CN114813156A (en) * | 2022-06-27 | 2022-07-29 | 中国航发四川燃气涡轮研究院 | High-altitude test bed cold-hot immersion test device and method for turboshaft engine |
| CN114813156B (en) * | 2022-06-27 | 2022-10-25 | 中国航发四川燃气涡轮研究院 | High-altitude test bed cold-hot immersion test device and method for turboshaft engine |
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