GB920079A - Improvements in or relating to apparatus for producing a high velocity gaseous stream - Google Patents

Improvements in or relating to apparatus for producing a high velocity gaseous stream

Info

Publication number
GB920079A
GB920079A GB3521860A GB3521860A GB920079A GB 920079 A GB920079 A GB 920079A GB 3521860 A GB3521860 A GB 3521860A GB 3521860 A GB3521860 A GB 3521860A GB 920079 A GB920079 A GB 920079A
Authority
GB
United Kingdom
Prior art keywords
arc
chamber
nozzle
cathode
liquid
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
GB3521860A
Inventor
Anthony William Thomas Mottram
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.)
Bristol Siddeley Engines Ltd
Original Assignee
Bristol Siddeley Engines 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 Bristol Siddeley Engines Ltd filed Critical Bristol Siddeley Engines Ltd
Priority to GB3521860A priority Critical patent/GB920079A/en
Publication of GB920079A publication Critical patent/GB920079A/en
Expired legal-status Critical Current

Links

Classifications

    • GPHYSICS
    • G01MEASURING; TESTING
    • G01MTESTING STATIC OR DYNAMIC BALANCE OF MACHINES OR STRUCTURES; TESTING OF STRUCTURES OR APPARATUS, NOT OTHERWISE PROVIDED FOR
    • G01M9/00Aerodynamic testing; Arrangements in or on wind tunnels
    • G01M9/02Wind tunnels
    • G01M9/04Details

Landscapes

  • Physics & Mathematics (AREA)
  • Fluid Mechanics (AREA)
  • General Physics & Mathematics (AREA)
  • Plasma Technology (AREA)
  • Physical Vapour Deposition (AREA)

Abstract

920,079. Arc plasma generators. BRISTOL SIDDELEY ENGINES Ltd. Sept. 29, 1961 [Oct. 14, 1960], No. 35218/60. Class 39 (3). [Also in Group XXXIII] A pair of concentric electrodes together form an annular convergent-divergent nozzle through the throat of which a working fluid axially flows, and across which a radial arc can be maintained, the arc heated working fluid being discharged from the nozzle into a chamber, which chamber is itself provided with an outlet nozzle for the discharge of the high velocity hot gas, which may be supplied to a hypersonic wind tunnel. Hollow cathode 4 and anode 3 define an arc chamber 1, into which a liquid oxygen/nitrogen mixture is introduced tangentially via spaced peripheral holes 6, to be evaporated by the arc maintained across the throat 12, the resultant gas being ejected into chamber 8 and thence from nozzle 9. The liquid is pumped, to act as coolant, via inlet pipe 13 and the hollow wall of nozzle 9 and chamber 8, through the helical passage formed by the partition 10 in the hollow wall of the anode 5 to the gallery 7, and thence to holes 6 and, via pipe 14, down the interior of the cathode 4; the pump 14 may have a bleed to the pump inlet for the control of the liquid supply. Further cooling of the cathode 4 and the throat of nozzle 9 is provided by the continuous evaporation of films of the liquid produced on their surface by the fine holes 15 and 17 respectively. Alternatively, by the use for these parts of the apparatus of porous walls, or of inserts formed of porous material or of fine metal tubes, sweat cooling may be employed; or those ports may be interchangeable with similar ports to permit either film or sweat cooling. A coil 20 may be connected in series with the electrodes; and several arc chambers may feed a single chamber 8, permitting a greater gas blow, and control of the gas temperature by the supply of cold air from one of the chambers the arc of which has been extinguished. In a modified method of use, compressed air may be fed directly to the arc chamber to constitute the source of gas. A modified cathode construction (Fig. 2, not shown) permits the use of a liquid metal, instead of the working fluid, as coolant, and enhances the Peltier cooling of the cathode. Specification 897,577 is referred to.
GB3521860A 1960-10-14 1960-10-14 Improvements in or relating to apparatus for producing a high velocity gaseous stream Expired GB920079A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB3521860A GB920079A (en) 1960-10-14 1960-10-14 Improvements in or relating to apparatus for producing a high velocity gaseous stream

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB3521860A GB920079A (en) 1960-10-14 1960-10-14 Improvements in or relating to apparatus for producing a high velocity gaseous stream

Publications (1)

Publication Number Publication Date
GB920079A true GB920079A (en) 1963-03-06

Family

ID=10375216

Family Applications (1)

Application Number Title Priority Date Filing Date
GB3521860A Expired GB920079A (en) 1960-10-14 1960-10-14 Improvements in or relating to apparatus for producing a high velocity gaseous stream

Country Status (1)

Country Link
GB (1) GB920079A (en)

Cited By (8)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3359734A (en) * 1964-11-19 1967-12-26 Snecma Electrothermal propulsion unit of the electric arc type
GB2116810A (en) * 1982-02-15 1983-09-28 Ceskoslovenska Akademie Ved Method for stabilization of low-temperature plasma of an arc burner, and the arc burner for carrying out said method
US4995231A (en) * 1988-02-01 1991-02-26 Olin Corporation Performance arcjet thruster
CN104596723A (en) * 2015-01-28 2015-05-06 中誉远发国际建设集团有限公司 Production method of diffuser used in aerodynamic experiments
CN106840580A (en) * 2016-12-07 2017-06-13 中国航天空气动力技术研究院 A kind of diaphragm positioning clamping device
CN107741313A (en) * 2017-11-29 2018-02-27 中国航空工业集团公司沈阳空气动力研究所 A kind of low wide Mach number wind-tunnel laminar flow double venturi of disturbance
CN113390600A (en) * 2021-07-26 2021-09-14 中国空气动力研究与发展中心计算空气动力研究所 Shock tunnel test simulation device and method for pneumatic thermal effect of pyrolysis gas
CN115596897A (en) * 2022-11-23 2023-01-13 中国空气动力研究与发展中心超高速空气动力研究所(Cn) Liquid oxygen supply pipeline for hypersonic high-temperature wind tunnel and precooling method thereof

Cited By (10)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3359734A (en) * 1964-11-19 1967-12-26 Snecma Electrothermal propulsion unit of the electric arc type
GB2116810A (en) * 1982-02-15 1983-09-28 Ceskoslovenska Akademie Ved Method for stabilization of low-temperature plasma of an arc burner, and the arc burner for carrying out said method
GB2157139A (en) * 1982-02-15 1985-10-16 Ceskoslovenska Akademie Ved Stabilising the arc of an arc burner
US4995231A (en) * 1988-02-01 1991-02-26 Olin Corporation Performance arcjet thruster
CN104596723A (en) * 2015-01-28 2015-05-06 中誉远发国际建设集团有限公司 Production method of diffuser used in aerodynamic experiments
CN106840580A (en) * 2016-12-07 2017-06-13 中国航天空气动力技术研究院 A kind of diaphragm positioning clamping device
CN106840580B (en) * 2016-12-07 2019-01-15 中国航天空气动力技术研究院 A kind of diaphragm positioning clamping device
CN107741313A (en) * 2017-11-29 2018-02-27 中国航空工业集团公司沈阳空气动力研究所 A kind of low wide Mach number wind-tunnel laminar flow double venturi of disturbance
CN113390600A (en) * 2021-07-26 2021-09-14 中国空气动力研究与发展中心计算空气动力研究所 Shock tunnel test simulation device and method for pneumatic thermal effect of pyrolysis gas
CN115596897A (en) * 2022-11-23 2023-01-13 中国空气动力研究与发展中心超高速空气动力研究所(Cn) Liquid oxygen supply pipeline for hypersonic high-temperature wind tunnel and precooling method thereof

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