GB870855A - Compound ram jet turbo-rocket engines - Google Patents

Compound ram jet turbo-rocket engines

Info

Publication number
GB870855A
GB870855A GB2746557A GB2746557A GB870855A GB 870855 A GB870855 A GB 870855A GB 2746557 A GB2746557 A GB 2746557A GB 2746557 A GB2746557 A GB 2746557A GB 870855 A GB870855 A GB 870855A
Authority
GB
United Kingdom
Prior art keywords
shaft
compressor
sleeve
turbine
aug
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
GB2746557A
Inventor
Bryn Leslie Belcher
Jack Vallis Blyth
David Edwin James Buckingham
Alan Leslie Davies
Reginald Henry Doug Chamberlin
Alan Leslie Roy Fletcher
Ronald Edward Morris
Geoffrey Charley Ger Mansfield
George Frank Upton
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.)
Napier Turbochargers Ltd
Original Assignee
D Napier and Son Ltd
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 D Napier and Son Ltd filed Critical D Napier and Son Ltd
Priority to GB2746557A priority Critical patent/GB870855A/en
Publication of GB870855A publication Critical patent/GB870855A/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
    • 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
    • F02K7/10—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 characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/18—Composite ram-jet/rocket engines
    • 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
    • F02K7/10—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 characterised by having ram-action compression, i.e. aero-thermo-dynamic-ducts or ram-jet engines
    • F02K7/16—Composite ram-jet/turbo-jet engines

Landscapes

  • Engineering & Computer Science (AREA)
  • Chemical & Material Sciences (AREA)
  • Combustion & Propulsion (AREA)
  • Mechanical Engineering (AREA)
  • General Engineering & Computer Science (AREA)
  • Structures Of Non-Positive Displacement Pumps (AREA)
  • Control Of Turbines (AREA)

Abstract

870,855. Ratchet clutches. NAPIER & SON Ltd., D. Aug. 28, 1958 [Aug. 30, 1957], No. 27465/57. Class 80 (2). [Also in Group XXVI] A free-wheeling clutch 28, provided in the shaft connecting the compressor of a jet propulsion enging (see Group XXVI) with its turbine, comprises an internally-threaded sleeve 133 engaging with a quick pitch thread on the turbine shaft 29. A series of resilient members 140 on the sleeve bear against the face of the flange 141 of a sleeve 142 keyed or splined on the compressor shaft 27 and urged towards the turbine by a spring 143. When the speed of the turbine shaft exceeds that of the compressor the frictional drag due to the members 140 rotates the sleeve 133 on the shaft 29 to advance it towards the compressor, until dogs 134 on the sleeve engage with corresponding dogs 135 on the compressor shaft to establish a driving connection. Specifications 835,293, 835,294, 837,497, 870,853 and 870,854 are referred to.
GB2746557A 1957-08-30 1957-08-30 Compound ram jet turbo-rocket engines Expired GB870855A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2746557A GB870855A (en) 1957-08-30 1957-08-30 Compound ram jet turbo-rocket engines

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2746557A GB870855A (en) 1957-08-30 1957-08-30 Compound ram jet turbo-rocket engines

Publications (1)

Publication Number Publication Date
GB870855A true GB870855A (en) 1961-06-21

Family

ID=10260038

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2746557A Expired GB870855A (en) 1957-08-30 1957-08-30 Compound ram jet turbo-rocket engines

Country Status (1)

Country Link
GB (1) GB870855A (en)

Cited By (3)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114426101A (en) * 2022-01-29 2022-05-03 中国航发湖南动力机械研究所 Cross-medium power device
CN114439646A (en) * 2022-01-27 2022-05-06 西北工业大学 Air turbine rocket stamping combined propulsion system
CN116291953A (en) * 2023-05-22 2023-06-23 北京大学 Full-continuous detonation mode turbine rocket ram combined cycle engine and operation method

Cited By (5)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
CN114439646A (en) * 2022-01-27 2022-05-06 西北工业大学 Air turbine rocket stamping combined propulsion system
CN114426101A (en) * 2022-01-29 2022-05-03 中国航发湖南动力机械研究所 Cross-medium power device
CN114426101B (en) * 2022-01-29 2023-11-17 中国航发湖南动力机械研究所 Cross-medium power device
CN116291953A (en) * 2023-05-22 2023-06-23 北京大学 Full-continuous detonation mode turbine rocket ram combined cycle engine and operation method
CN116291953B (en) * 2023-05-22 2023-07-25 北京大学 Full-continuous detonation mode turbine rocket ram combined cycle engine and operation method

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