DE1241194B - Schalldaempfende Schubduese fuer Strahltriebwerke - Google Patents

Schalldaempfende Schubduese fuer Strahltriebwerke

Info

Publication number
DE1241194B
DE1241194B DE1960Y0000415 DEY0000415A DE1241194B DE 1241194 B DE1241194 B DE 1241194B DE 1960Y0000415 DE1960Y0000415 DE 1960Y0000415 DE Y0000415 A DEY0000415 A DE Y0000415A DE 1241194 B DE1241194 B DE 1241194B
Authority
DE
Germany
Prior art keywords
wings
nozzle
thrust nozzle
nozzle according
thrust
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.)
Granted
Application number
DE1960Y0000415
Other languages
German (de)
English (en)
Other versions
DE1241194C2 (US08066781-20111129-C00013.png
Inventor
Alec David Young
Current Assignee (The listed assignees may be inaccurate. Google has not performed a legal analysis and makes no representation or warranty as to the accuracy of the list.)
Individual
Original Assignee
Individual
Priority date (The priority date 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 date listed.)
Filing date
Publication date
Application filed by Individual filed Critical Individual
Publication of DE1241194B publication Critical patent/DE1241194B/de
Application granted granted Critical
Publication of DE1241194C2 publication Critical patent/DE1241194C2/de
Granted legal-status Critical Current

Links

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
    • F02K1/46—Nozzles having means for adding air to the jet or for augmenting the mixing region between the jet and the ambient air, e.g. for silencing

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Turbine Rotor Nozzle Sealing (AREA)
  • Nozzles (AREA)
  • Testing Of Engines (AREA)
DE1960Y0000415 1959-05-01 1960-04-27 Schalldaempfende Schubduese fuer Strahltriebwerke Granted DE1241194B (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB1503859A GB885093A (en) 1959-05-01 1959-05-01 Improvements in or relating to jet propulsion nozzles

Publications (2)

Publication Number Publication Date
DE1241194B true DE1241194B (de) 1967-05-24
DE1241194C2 DE1241194C2 (US08066781-20111129-C00013.png) 1967-11-23

Family

ID=10051955

Family Applications (1)

Application Number Title Priority Date Filing Date
DE1960Y0000415 Granted DE1241194B (de) 1959-05-01 1960-04-27 Schalldaempfende Schubduese fuer Strahltriebwerke

Country Status (4)

Country Link
DE (1) DE1241194B (US08066781-20111129-C00013.png)
FR (1) FR1255674A (US08066781-20111129-C00013.png)
GB (1) GB885093A (US08066781-20111129-C00013.png)
NL (1) NL250991A (US08066781-20111129-C00013.png)

Families Citing this family (12)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
FR2053736A5 (US08066781-20111129-C00013.png) * 1969-07-16 1971-04-16 Dassault Aeronautique
US3568794A (en) * 1969-10-02 1971-03-09 Rohr Corp Method and apparatus for suppressing the noise of a fan-jet engine
US3647020A (en) * 1970-02-02 1972-03-07 Rohr Corp Jet propulsion apparatus and operating method
US3664455A (en) * 1971-03-15 1972-05-23 Rohr Corp Twisted vane sound suppressor for aircraft jet engine
US3776363A (en) * 1971-05-10 1973-12-04 A Kuethe Control of noise and instabilities in jet engines, compressors, turbines, heat exchangers and the like
US4685643A (en) * 1983-08-04 1987-08-11 The Boeing Company Nacelle/wing assembly with vortex control device
GB2372780A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise-reducing tabs
GB0105349D0 (en) 2001-03-03 2001-04-18 Rolls Royce Plc Gas turbine engine exhaust nozzle
GB2372779A (en) * 2001-03-03 2002-09-04 Rolls Royce Plc Gas turbine engine nozzle with noise reducing tabs
US7340883B2 (en) 2004-11-12 2008-03-11 The Boeing Company Morphing structure
FR2928183A1 (fr) 2008-02-29 2009-09-04 Aircelle Sa Dispositif de reduction de bruit pour moteur d'aeronef, du type a chevrons mobiles
CN104405530B (zh) * 2014-10-16 2016-03-02 南京航空航天大学 分开排气式涡扇发动机排气降噪系统

Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650752A (en) * 1949-08-27 1953-09-01 United Aircraft Corp Boundary layer control in blowers
GB831152A (en) * 1956-02-07 1960-03-23 Boeing Co Noise suppression nozzles for jet propulsion engines

Patent Citations (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2650752A (en) * 1949-08-27 1953-09-01 United Aircraft Corp Boundary layer control in blowers
GB831152A (en) * 1956-02-07 1960-03-23 Boeing Co Noise suppression nozzles for jet propulsion engines

Also Published As

Publication number Publication date
FR1255674A (fr) 1961-03-10
GB885093A (en) 1961-12-20
DE1241194C2 (US08066781-20111129-C00013.png) 1967-11-23
NL250991A (US08066781-20111129-C00013.png)

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