GB593070A - Improvements in or relating to aircraft propulsion - Google Patents

Improvements in or relating to aircraft propulsion

Info

Publication number
GB593070A
GB593070A GB30140/46A GB3014046A GB593070A GB 593070 A GB593070 A GB 593070A GB 30140/46 A GB30140/46 A GB 30140/46A GB 3014046 A GB3014046 A GB 3014046A GB 593070 A GB593070 A GB 593070A
Authority
GB
United Kingdom
Prior art keywords
relating
jet
propulsion
aircraft propulsion
nozzle areas
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
GB30140/46A
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.)
Westinghouse Electric International Co
Original Assignee
Westinghouse Electric International Co
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 Westinghouse Electric International Co filed Critical Westinghouse Electric International Co
Publication of GB593070A publication Critical patent/GB593070A/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
    • F02K1/1207—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 fixed structure
    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K7/00—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof
    • F02K7/08—Plants in which the working fluid is used in a jet only, i.e. the plants not having a turbine or other engine driving a compressor or a ducted fan; Control thereof the jet being continuous
    • 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
    • Y02—TECHNOLOGIES OR APPLICATIONS FOR MITIGATION OR ADAPTATION AGAINST CLIMATE CHANGE
    • Y02T—CLIMATE CHANGE MITIGATION TECHNOLOGIES RELATED TO TRANSPORTATION
    • Y02T50/00—Aeronautics or air transport
    • Y02T50/60—Efficient propulsion technologies, e.g. for aircraft

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Control Of Turbines (AREA)
  • Transmission Devices (AREA)

Abstract

593,070. Jet - propulsion plant. WESTINGHOUSE ELECTRIC INTERNATIONAL CO. April 5, 1944, No. 30140/46. Convention date, July 25, 1941. Divided out of 593,022. [Class 110 (iii)] A propulsion jet for aircraft as described in Specification 593,022 has the inlet and exhaust nozzle areas adjustable. In one form, Fig. 5, hinged plates 16, 18 slide between fixed side plates. In a further form the nozzles are made elliptical in section and deformable. The nozzle areas can be adjusted separately or jointly. Specification 593,071 also is referred to.
GB30140/46A 1941-07-25 1944-04-05 Improvements in or relating to aircraft propulsion Expired GB593070A (en)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US593070XA 1941-07-25 1941-07-25

Publications (1)

Publication Number Publication Date
GB593070A true GB593070A (en) 1947-10-07

Family

ID=22022145

Family Applications (2)

Application Number Title Priority Date Filing Date
GB30140/46A Expired GB593070A (en) 1941-07-25 1944-04-05 Improvements in or relating to aircraft propulsion
GB30141/46A Expired GB593071A (en) 1941-07-25 1944-04-05 Improvements in or relating to aircraft propulsion

Family Applications After (1)

Application Number Title Priority Date Filing Date
GB30141/46A Expired GB593071A (en) 1941-07-25 1944-04-05 Improvements in or relating to aircraft propulsion

Country Status (1)

Country Link
GB (2) GB593070A (en)

Families Citing this family (2)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US2608820A (en) * 1948-08-30 1952-09-02 Engineering & Res Corp Variable area tail pipe for jet engines
US2625788A (en) * 1948-12-15 1953-01-20 Mcdonnell Aircraft Corp Flame holder and fuel nozzle supporting mechanism for ram jet engines

Also Published As

Publication number Publication date
GB593071A (en) 1947-10-07

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