DE2211710A1 - Verbrennungsmotor - Google Patents

Verbrennungsmotor

Info

Publication number
DE2211710A1
DE2211710A1 DE19722211710 DE2211710A DE2211710A1 DE 2211710 A1 DE2211710 A1 DE 2211710A1 DE 19722211710 DE19722211710 DE 19722211710 DE 2211710 A DE2211710 A DE 2211710A DE 2211710 A1 DE2211710 A1 DE 2211710A1
Authority
DE
Germany
Prior art keywords
foam
gases
internal combustion
combustion engine
engine
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
Application number
DE19722211710
Other languages
German (de)
English (en)
Inventor
Harland L. Tarzana; Rodewald Newell Charles Manhattan Beach; Calif. Bürge jun. (V.StA.). FOIn 3-04
Original Assignee
TRW Inc., Redondo Beach, Calif. (V.StA.)
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 TRW Inc., Redondo Beach, Calif. (V.StA.) filed Critical TRW Inc., Redondo Beach, Calif. (V.StA.)
Publication of DE2211710A1 publication Critical patent/DE2211710A1/de
Pending legal-status Critical Current

Links

Classifications

    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K9/00Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
    • F02K9/42Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using liquid or gaseous propellants
    • F02K9/60Constructional parts; Details not otherwise provided for
    • F02K9/62Combustion or thrust chambers
    • F02K9/64Combustion or thrust chambers having cooling arrangements
    • FMECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02KJET-PROPULSION PLANTS
    • F02K1/00Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/28Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto using fluid jets to influence the jet flow

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Exhaust Silencers (AREA)
DE19722211710 1971-03-10 1972-03-10 Verbrennungsmotor Pending DE2211710A1 (de)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US12285871A 1971-03-10 1971-03-10

Publications (1)

Publication Number Publication Date
DE2211710A1 true DE2211710A1 (de) 1972-09-14

Family

ID=22405229

Family Applications (1)

Application Number Title Priority Date Filing Date
DE19722211710 Pending DE2211710A1 (de) 1971-03-10 1972-03-10 Verbrennungsmotor

Country Status (5)

Country Link
US (1) US3782116A (enExample)
CA (1) CA945384A (enExample)
DE (1) DE2211710A1 (enExample)
FR (1) FR2128867B1 (enExample)
IT (1) IT957461B (enExample)

Families Citing this family (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US5269132A (en) * 1992-10-29 1993-12-14 E-Systems, Inc. Method and apparatus for controlling infrared emissions
FR2805008B1 (fr) * 2000-02-16 2002-05-31 Joseph Haiun Compresseur termocinetique
US20050022500A1 (en) * 2003-07-28 2005-02-03 Buehler David Benjamin Rocket engine passivation system
DE102004018725B4 (de) * 2004-04-17 2015-02-12 Astrium Gmbh Dämpfung von Schwingungen einer Brennkammer durch Resonatoren
US8015819B2 (en) * 2006-09-29 2011-09-13 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Wet active chevron nozzle for controllable jet noise reduction
US8453997B2 (en) * 2010-11-20 2013-06-04 Fisonic Holding Limited Supersonic nozzle
US8505577B2 (en) * 2010-11-30 2013-08-13 The United States Of America As Represented By The Secretary Of The Army Pnumatically actuated bi-propellant valve (PABV) system for a throttling vortex engine
US10081091B2 (en) * 2015-06-12 2018-09-25 Postech Academy-Industry Foundation Nozzle, device, and method for high-speed generation of uniform nanoparticles

Family Cites Families (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US1144193A (en) * 1910-08-23 1915-06-22 Lambert Haas Process of deodorizing waste gases.
US2648196A (en) * 1947-03-18 1953-08-11 Experiment Inc Ram jet burner with aqueous injection to promote smooth burning
US3169368A (en) * 1961-02-07 1965-02-16 Bolkow Entwicklungen Kg Combustion chamber for liquid fuels
FR1391927A (fr) * 1964-01-29 1965-03-12 Monsieur Le Ministre Des Armee Chambre de combustion avec tuyère pour moteurs fusées à liquides
US3365889A (en) * 1964-05-27 1968-01-30 United Aircraft Corp Propellant aeration system
US3358456A (en) * 1964-11-13 1967-12-19 Astrosystems Internat Inc Pulsed rocket engine
US3383854A (en) * 1966-11-28 1968-05-21 John H. White Internal combustion engine exhaust cleaner
US3534555A (en) * 1968-03-06 1970-10-20 Webb James E Laminar flow enhancement

Also Published As

Publication number Publication date
US3782116A (en) 1974-01-01
FR2128867A1 (enExample) 1972-10-20
IT957461B (it) 1973-10-10
FR2128867B1 (enExample) 1976-10-29
CA945384A (en) 1974-04-16

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