FR1167038A - Improvements relating to variable section nozzles - Google Patents

Improvements relating to variable section nozzles

Info

Publication number
FR1167038A
FR1167038A FR1167038DA FR1167038A FR 1167038 A FR1167038 A FR 1167038A FR 1167038D A FR1167038D A FR 1167038DA FR 1167038 A FR1167038 A FR 1167038A
Authority
FR
France
Prior art keywords
improvements relating
variable section
section nozzles
nozzles
variable
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)
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.)
Raytheon Technologies Corp
Original Assignee
United Aircraft Corp
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 United Aircraft Corp filed Critical United Aircraft Corp
Application granted granted Critical
Publication of FR1167038A publication Critical patent/FR1167038A/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
    • F02K1/06—Varying effective area of jet pipe or nozzle
    • F02K1/12—Varying effective area of jet pipe or nozzle by means of pivoted flaps
    • F02K1/1261—Varying effective area of jet pipe or nozzle by means of pivoted flaps of one series of flaps hinged at their upstream ends on a substantially axially movable structure
    • Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
    • Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
    • Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
    • Y10T74/00—Machine element or mechanism
    • Y10T74/18—Mechanical movements
    • Y10T74/18888—Reciprocating to or from oscillating
    • Y10T74/1892—Lever and slide
    • Y10T74/1896—Cam connections

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Nozzles (AREA)
FR1167038D 1952-10-25 1955-03-16 Improvements relating to variable section nozzles Expired FR1167038A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US316912A US2932161A (en) 1952-10-25 1952-10-25 Variable area nozzle

Publications (1)

Publication Number Publication Date
FR1167038A true FR1167038A (en) 1958-11-19

Family

ID=23231248

Family Applications (1)

Application Number Title Priority Date Filing Date
FR1167038D Expired FR1167038A (en) 1952-10-25 1955-03-16 Improvements relating to variable section nozzles

Country Status (2)

Country Link
US (1) US2932161A (en)
FR (1) FR1167038A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3132565A (en) * 1961-12-26 1964-05-12 Gen Electric Control system
DE1936800C3 (en) * 1969-07-19 1975-08-07 Motoren- Und Turbinen-Union Muenchen Gmbh, 8000 Muenchen Convergent thrust nozzle for a gas turbine jet engine that can be changed with regard to its outlet cross section

Family Cites Families (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB506714A (en) * 1938-01-25 1939-06-02 Arado Flugzeugwerke Ges Mit Be Means for shifting flaps on aircraft
US2352062A (en) * 1940-01-13 1944-06-20 Edward F Zap Upper surface flap
GB607686A (en) * 1945-02-01 1948-09-03 Power Jets Res & Dev Ltd Improvements relating to duct inlets for use in supersonic conditions
US2502315A (en) * 1946-02-26 1950-03-28 Beech Aircraft Corp Operating mechanism for high lift devices for airplanes
US2634578A (en) * 1949-02-19 1953-04-14 Mcdonnell Aircraft Corp Device for varying the effective area of discharge orifices of jet engines or afterburners therefor
US2693078A (en) * 1949-03-18 1954-11-02 Westinghouse Electric Corp Exhaust orifice control for jet engines
US2603060A (en) * 1949-09-30 1952-07-15 Westinghouse Electric Corp Cooling means for variable area nozzles
US2603062A (en) * 1949-09-30 1952-07-15 Westinghouse Electric Corp Variable area jet nozzle
US2778190A (en) * 1950-06-08 1957-01-22 Republic Aviat Corp Variable area nozzle for jet engines
US2637163A (en) * 1951-04-26 1953-05-05 Westinghouse Electric Corp Jet engine variable area exhaust nozzle

Also Published As

Publication number Publication date
US2932161A (en) 1960-04-12

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