SE8305863L - ROBOT - Google Patents
ROBOTInfo
- Publication number
- SE8305863L SE8305863L SE8305863A SE8305863A SE8305863L SE 8305863 L SE8305863 L SE 8305863L SE 8305863 A SE8305863 A SE 8305863A SE 8305863 A SE8305863 A SE 8305863A SE 8305863 L SE8305863 L SE 8305863L
- Authority
- SE
- Sweden
- Prior art keywords
- missile
- intakes
- edges
- vortices
- ingestion
- Prior art date
Links
- 238000004873 anchoring Methods 0.000 abstract 1
- 230000037406 food intake Effects 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
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02C—GAS-TURBINE PLANTS; AIR INTAKES FOR JET-PROPULSION PLANTS; CONTROLLING FUEL SUPPLY IN AIR-BREATHING JET-PROPULSION PLANTS
- F02C7/00—Features, components parts, details or accessories, not provided for in, or of interest apart form groups F02C1/00 - F02C6/00; Air intakes for jet-propulsion plants
- F02C7/04—Air intakes for gas-turbine plants or jet-propulsion plants
-
- 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
- B64D2033/0253—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft
- B64D2033/026—Arrangements in aircraft of power plant parts or auxiliaries not otherwise provided for of combustion air intakes specially adapted for particular type of aircraft for supersonic or hypersonic aircraft
-
- 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
- B64D2033/0273—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 jet engines
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Radar Systems Or Details Thereof (AREA)
- Aiming, Guidance, Guns With A Light Source, Armor, Camouflage, And Targets (AREA)
- Lining And Supports For Tunnels (AREA)
Abstract
The ingestion of vortices into engine intakes 13, Fig 1, at the rear of a guided missile 10 is prevented by having intakes whose breadth increases with radial distance from the surface of the missile and by providing, forwards of each of the intakes, longitudinally extending vortex anchoring edges 12. The edges are constituted by strakes extending along a cylindrical missile body or, where the missile body is of triangular or square cross-section (Figs 5 & 6 not shown) by the corner edges of the body. <IMAGE>
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB8230413 | 1982-10-28 |
Publications (2)
Publication Number | Publication Date |
---|---|
SE8305863D0 SE8305863D0 (en) | 1983-10-25 |
SE8305863L true SE8305863L (en) | 1990-09-14 |
Family
ID=10533823
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
SE8305863A SE8305863L (en) | 1982-10-28 | 1983-10-25 | ROBOT |
Country Status (4)
Country | Link |
---|---|
DE (1) | DE3338697A1 (en) |
GB (1) | GB2230844B (en) |
IT (1) | IT8349204A0 (en) |
SE (1) | SE8305863L (en) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
RU2446994C2 (en) * | 2009-04-21 | 2012-04-10 | Открытое акционерное общество "Корпорация "Тактическое ракетное вооружение" | Aircraft engine air intake |
CN112985192A (en) * | 2021-04-01 | 2021-06-18 | 南昌航空大学 | Pneumatic layout of double-oblique-swept-wing air-surface cruise missile |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4381017A (en) * | 1980-04-05 | 1983-04-26 | Messerschmitt-Boelkow-Blohm Gesellschaft Mit Beschraenkter Haftung | Air inlet, especially a two-dimensional air inlet set at an angle on one side for gas turbine jet propulsion plants for driving airplanes |
JPS595777B2 (en) * | 1980-11-15 | 1984-02-07 | 富士重工業株式会社 | Air suction device for aircraft-mounted gas turbine engine |
-
1983
- 1983-10-20 GB GB8328105A patent/GB2230844B/en not_active Expired - Lifetime
- 1983-10-21 IT IT8349204A patent/IT8349204A0/en unknown
- 1983-10-25 SE SE8305863A patent/SE8305863L/en not_active Application Discontinuation
- 1983-10-25 DE DE19833338697 patent/DE3338697A1/en not_active Withdrawn
Also Published As
Publication number | Publication date |
---|---|
GB2230844B (en) | 1991-03-20 |
GB2230844A (en) | 1990-10-31 |
DE3338697A1 (en) | 1991-01-03 |
IT8349204A0 (en) | 1983-10-21 |
SE8305863D0 (en) | 1983-10-25 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
NAV | Patent application has lapsed |
Ref document number: 8305863-6 Effective date: 19910501 |