FR1176983A - Improvements to jet thrusters - Google Patents

Improvements to jet thrusters

Info

Publication number
FR1176983A
FR1176983A FR1176983DA FR1176983A FR 1176983 A FR1176983 A FR 1176983A FR 1176983D A FR1176983D A FR 1176983DA FR 1176983 A FR1176983 A FR 1176983A
Authority
FR
France
Prior art keywords
jet thrusters
thrusters
jet
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.)
Expired
Application number
Other languages
French (fr)
Inventor
Hans Rosskopf
Michel Lhenri
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.)
Safran Aircraft Engines SAS
Original Assignee
Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
SNECMA SAS
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 Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA, SNECMA SAS filed Critical Societe Nationale dEtude et de Construction de Moteurs dAviation SNECMA
Application granted granted Critical
Publication of FR1176983A publication Critical patent/FR1176983A/en
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
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C9/00—Adjustable control surfaces or members, e.g. rudders
    • B64C9/38—Jet 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
    • F02K1/48—Corrugated nozzles
FR1176983D 1957-05-23 1957-05-23 Improvements to jet thrusters Expired FR1176983A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
FR1176983T 1957-05-23

Publications (1)

Publication Number Publication Date
FR1176983A true FR1176983A (en) 1959-04-17

Family

ID=9660001

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1176983D Expired FR1176983A (en) 1957-05-23 1957-05-23 Improvements to jet thrusters

Country Status (1)

Country Link
FR (1) FR1176983A (en)

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3161257A (en) * 1959-05-01 1964-12-15 Young Alec David Jet pipe nozzle silencers
DE1294394B (en) * 1963-08-02 1969-05-08 Snecma Silencer for supersonic jet engines
FR2000785A1 (en) * 1968-01-26 1969-09-12 United Aircraft Corp THRUST DEVIATOR WITH PROVISIONS FOR LACED CONTROL
FR2597157A1 (en) * 1986-04-15 1987-10-16 Snecma Multi-lobe flow mixer with a variable flow cross-section for bypass or multi-bypass jet engines
US5761900A (en) * 1995-10-11 1998-06-09 Stage Iii Technologies, L.C. Two-stage mixer ejector suppressor
US5884472A (en) * 1995-10-11 1999-03-23 Stage Iii Technologies, L.C. Alternating lobed mixer/ejector concept suppressor

Cited By (6)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3161257A (en) * 1959-05-01 1964-12-15 Young Alec David Jet pipe nozzle silencers
DE1294394B (en) * 1963-08-02 1969-05-08 Snecma Silencer for supersonic jet engines
FR2000785A1 (en) * 1968-01-26 1969-09-12 United Aircraft Corp THRUST DEVIATOR WITH PROVISIONS FOR LACED CONTROL
FR2597157A1 (en) * 1986-04-15 1987-10-16 Snecma Multi-lobe flow mixer with a variable flow cross-section for bypass or multi-bypass jet engines
US5761900A (en) * 1995-10-11 1998-06-09 Stage Iii Technologies, L.C. Two-stage mixer ejector suppressor
US5884472A (en) * 1995-10-11 1999-03-23 Stage Iii Technologies, L.C. Alternating lobed mixer/ejector concept suppressor

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