DE2157960A1 - Lärmdämpfer für Flugzeug-Strahltriebwerke - Google Patents
Lärmdämpfer für Flugzeug-StrahltriebwerkeInfo
- Publication number
- DE2157960A1 DE2157960A1 DE19712157960 DE2157960A DE2157960A1 DE 2157960 A1 DE2157960 A1 DE 2157960A1 DE 19712157960 DE19712157960 DE 19712157960 DE 2157960 A DE2157960 A DE 2157960A DE 2157960 A1 DE2157960 A1 DE 2157960A1
- Authority
- DE
- Germany
- Prior art keywords
- nozzle
- parts
- thrust
- jet
- downstream
- 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.)
- Pending
Links
- 238000011144 upstream manufacturing Methods 0.000 claims description 5
- 238000002485 combustion reaction Methods 0.000 claims description 2
- 239000006096 absorbing agent Substances 0.000 claims 1
- 230000001629 suppression Effects 0.000 description 3
- 239000007789 gas Substances 0.000 description 2
- 230000004308 accommodation Effects 0.000 description 1
- 238000010276 construction Methods 0.000 description 1
- 238000005192 partition Methods 0.000 description 1
- 230000000007 visual effect Effects 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/44—Nozzles having means, e.g. a shield, reducing sound radiation in a specified direction
-
- 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—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for
- B64D33/04—Arrangement in aircraft of power plant parts or auxiliaries not otherwise provided for of exhaust outlets or jet pipes
- B64D33/06—Silencing exhaust or propulsion jets
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
- F02K1/40—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet
- F02K1/42—Nozzles having means for dividing the jet into a plurality of partial jets or having an elongated cross-section outlet the means being movable into an inoperative position
Landscapes
- Engineering & Computer Science (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Mechanical Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Aviation & Aerospace Engineering (AREA)
- Testing Of Engines (AREA)
Applications Claiming Priority (2)
| Application Number | Priority Date | Filing Date | Title |
|---|---|---|---|
| GB5688770 | 1970-11-30 | ||
| GB6040470A GB1371785A (en) | 1970-11-30 | 1970-12-19 | Noise suppressor for jet engines |
Publications (1)
| Publication Number | Publication Date |
|---|---|
| DE2157960A1 true DE2157960A1 (de) | 1972-08-24 |
Family
ID=26267654
Family Applications (1)
| Application Number | Title | Priority Date | Filing Date |
|---|---|---|---|
| DE19712157960 Pending DE2157960A1 (de) | 1970-11-30 | 1971-11-23 | Lärmdämpfer für Flugzeug-Strahltriebwerke |
Country Status (3)
| Country | Link |
|---|---|
| US (1) | US3706353A (enExample) |
| DE (1) | DE2157960A1 (enExample) |
| FR (1) | FR2115475B1 (enExample) |
Families Citing this family (5)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| FR2242568B2 (enExample) * | 1973-08-31 | 1976-10-01 | Snecma | |
| FR2242570B1 (enExample) * | 1973-08-31 | 1976-06-18 | Snecma | |
| US5422443A (en) * | 1991-10-18 | 1995-06-06 | Hughes Missile Systems Company | Rocket exhaust disrupter shapes |
| US5717172A (en) * | 1996-10-18 | 1998-02-10 | Northrop Grumman Corporation | Sound suppressor exhaust structure |
| RU2171900C2 (ru) * | 1996-10-18 | 2001-08-10 | Нортроп-Грамман Корпорейшн | Выхлопная система с устройством для подавления звука |
Family Cites Families (4)
| Publication number | Priority date | Publication date | Assignee | Title |
|---|---|---|---|---|
| GB580995A (en) * | 1944-01-21 | 1946-09-26 | British Thomson Houston Co Ltd | Improvements in and relating to aircraft employing jet propulsion |
| US2486967A (en) * | 1945-07-25 | 1949-11-01 | United Aircraft Corp | Airplane wing with jet propulsion apparatus |
| US2928238A (en) * | 1953-06-08 | 1960-03-15 | Lockheed Aircraft Corp | Jet deflector and orifice control |
| GB874427A (en) * | 1958-06-03 | 1961-08-10 | Alec Tucker | New or improved speed and direction control means for water craft |
-
1971
- 1971-11-23 US US201511A patent/US3706353A/en not_active Expired - Lifetime
- 1971-11-23 DE DE19712157960 patent/DE2157960A1/de active Pending
- 1971-11-29 FR FR7142697A patent/FR2115475B1/fr not_active Expired
Also Published As
| Publication number | Publication date |
|---|---|
| FR2115475A1 (enExample) | 1972-07-07 |
| FR2115475B1 (enExample) | 1976-07-23 |
| US3706353A (en) | 1972-12-19 |
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Legal Events
| Date | Code | Title | Description |
|---|---|---|---|
| OHB | Non-payment of the publication fee (examined application) |