FR2053736A5 - - Google Patents

Info

Publication number
FR2053736A5
FR2053736A5 FR6924196A FR6924196A FR2053736A5 FR 2053736 A5 FR2053736 A5 FR 2053736A5 FR 6924196 A FR6924196 A FR 6924196A FR 6924196 A FR6924196 A FR 6924196A FR 2053736 A5 FR2053736 A5 FR 2053736A5
Authority
FR
France
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
Application number
FR6924196A
Other languages
French (fr)
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.)
Dassault Aviation SA
Original Assignee
Dassault Aviation SA
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 Dassault Aviation SA filed Critical Dassault Aviation SA
Priority to FR6924196A priority Critical patent/FR2053736A5/fr
Priority to US53224A priority patent/US3613827A/en
Priority to GB3353570A priority patent/GB1307867A/en
Priority to NL7010373A priority patent/NL7010373A/xx
Priority to DE2035403A priority patent/DE2035403C3/de
Application granted granted Critical
Publication of FR2053736A5 publication Critical patent/FR2053736A5/fr
Expired 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
    • F02K1/54—Nozzles having means for reversing jet thrust
    • F02K1/56—Reversing jet main flow
    • F02K1/62—Reversing jet main flow by blocking the rearward discharge by means of flaps
    • 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
FR6924196A 1969-07-16 1969-07-16 Expired FR2053736A5 (xx)

Priority Applications (5)

Application Number Priority Date Filing Date Title
FR6924196A FR2053736A5 (xx) 1969-07-16 1969-07-16
US53224A US3613827A (en) 1969-07-16 1970-07-08 Device for attenuating noise emitted by the jet of a jet engine
GB3353570A GB1307867A (en) 1969-07-16 1970-07-10 Device for attenuating noise emitted by the jet of a jet engine
NL7010373A NL7010373A (xx) 1969-07-16 1970-07-14
DE2035403A DE2035403C3 (de) 1969-07-16 1970-07-16 Schalldämpfungseinrichtung für die Schubdüse eines Strahltriebwerkes

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR6924196A FR2053736A5 (xx) 1969-07-16 1969-07-16

Publications (1)

Publication Number Publication Date
FR2053736A5 true FR2053736A5 (xx) 1971-04-16

Family

ID=9037526

Family Applications (1)

Application Number Title Priority Date Filing Date
FR6924196A Expired FR2053736A5 (xx) 1969-07-16 1969-07-16

Country Status (5)

Country Link
US (1) US3613827A (xx)
DE (1) DE2035403C3 (xx)
FR (1) FR2053736A5 (xx)
GB (1) GB1307867A (xx)
NL (1) NL7010373A (xx)

Families Citing this family (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3830431A (en) * 1973-03-23 1974-08-20 Nasa Abating exhaust noises in jet engines
US4175640A (en) * 1975-03-31 1979-11-27 Boeing Commercial Airplane Company Vortex generators for internal mixing in a turbofan engine
US4298089A (en) * 1976-12-23 1981-11-03 The Boeing Company Vortex generators for internal mixing in a turbofan engine
US4439104A (en) * 1981-06-15 1984-03-27 The Garrett Corporation Compressor inlet guide vane and vortex-disturbing member assembly
US4844695A (en) * 1988-07-05 1989-07-04 Pratt & Whitney Canada Inc. Variable flow radial compressor inlet flow fences
US5203164A (en) * 1990-06-06 1993-04-20 Paulson Allen E Method and apparatus for quieting a turbojet engine
US5517865A (en) * 1991-06-13 1996-05-21 General Electric Company Vortex suppression for an eductor
US5197855A (en) * 1991-07-01 1993-03-30 United Technologies Corporation Engine exhaust/blade interaction noise suppression
US5373691A (en) * 1993-06-23 1994-12-20 Allied-Signal Inc. Inlet guide vane dewhistler
WO2000040851A1 (en) * 1999-01-04 2000-07-13 Allison Advanced Development Company Exhaust mixer and apparatus using same
US7293401B2 (en) * 2002-03-20 2007-11-13 The Regents Of The University Of California Jet engine noise suppressor
US7926256B2 (en) * 2008-10-27 2011-04-19 General Electric Company Inlet system for an EGR system
FR3092145A1 (fr) * 2019-01-24 2020-07-31 Airbus Operations Turboreacteur double flux comportant une serie de lames rotatives pour obturer la veine du flux secondaire

Family Cites Families (4)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3153319A (en) * 1952-07-25 1964-10-20 Young Alec David Jet noise suppression means
US2944623A (en) * 1955-09-02 1960-07-12 Jr Albert G Bodine Jet engine noise reducer
US2934889A (en) * 1956-02-14 1960-05-03 United Aircraft Corp Noise abatement means
NL250991A (xx) * 1959-05-01

Also Published As

Publication number Publication date
DE2035403B2 (de) 1979-10-25
DE2035403A1 (de) 1971-02-04
US3613827A (en) 1971-10-19
GB1307867A (en) 1973-02-21
NL7010373A (xx) 1971-01-19
DE2035403C3 (de) 1980-07-17

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Legal Events

Date Code Title Description
ST Notification of lapse