GB836421A - Method of making high frequency power dissipating terminations - Google Patents

Method of making high frequency power dissipating terminations

Info

Publication number
GB836421A
GB836421A GB2137056A GB2137056A GB836421A GB 836421 A GB836421 A GB 836421A GB 2137056 A GB2137056 A GB 2137056A GB 2137056 A GB2137056 A GB 2137056A GB 836421 A GB836421 A GB 836421A
Authority
GB
United Kingdom
Prior art keywords
inlay
high frequency
frequency power
terminations
power dissipating
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
GB2137056A
Inventor
Tore N Anderson
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.)
Airtron Inc
Original Assignee
Airtron Inc
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 Airtron Inc filed Critical Airtron Inc
Priority to GB2137056A priority Critical patent/GB836421A/en
Publication of GB836421A publication Critical patent/GB836421A/en
Expired legal-status Critical Current

Links

Classifications

    • HELECTRICITY
    • H01ELECTRIC ELEMENTS
    • H01PWAVEGUIDES; RESONATORS, LINES, OR OTHER DEVICES OF THE WAVEGUIDE TYPE
    • H01P1/00Auxiliary devices
    • H01P1/24Terminating devices
    • H01P1/26Dissipative terminations

Landscapes

  • Microwave Tubes (AREA)

Abstract

A high frequency power dissipating termination is made by casting a metal, e.g. Al, jacket around a hollow inlay of dissipative material such as silicon carbide, or a ceramic or metal-ceramic. The inlay is formed in a two-part mould, using a frangible or otherwise removable core to produce a wedge shaped cavity in the inlay, which is fired after removal from the mould. The inlay is then inserted in a two-part mould and the metal cast cast. The end of the termination is then machined &c. for connection to a related component. U.S.A. Specification 2,676,307 is referred to.
GB2137056A 1956-07-10 1956-07-10 Method of making high frequency power dissipating terminations Expired GB836421A (en)

Priority Applications (1)

Application Number Priority Date Filing Date Title
GB2137056A GB836421A (en) 1956-07-10 1956-07-10 Method of making high frequency power dissipating terminations

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
GB2137056A GB836421A (en) 1956-07-10 1956-07-10 Method of making high frequency power dissipating terminations

Publications (1)

Publication Number Publication Date
GB836421A true GB836421A (en) 1960-06-01

Family

ID=10161781

Family Applications (1)

Application Number Title Priority Date Filing Date
GB2137056A Expired GB836421A (en) 1956-07-10 1956-07-10 Method of making high frequency power dissipating terminations

Country Status (1)

Country Link
GB (1) GB836421A (en)

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848847A (en) * 1972-07-11 1974-11-19 Toyoda Chuo Kenkyusho Kk Casting method for aluminum or aluminum alloys and a mold therefor

Cited By (1)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US3848847A (en) * 1972-07-11 1974-11-19 Toyoda Chuo Kenkyusho Kk Casting method for aluminum or aluminum alloys and a mold therefor

Similar Documents

Publication Publication Date Title
ATE54848T1 (en) DIE CASTING MACHINE.
ES8100125A1 (en) Casting thixotropic metals
GB585665A (en) Casting metals
GB1522344A (en) Method of manufacture of a roller
GB836421A (en) Method of making high frequency power dissipating terminations
FR1476181A (en) Ingot mold for the continuous casting of metals, and method of manufacturing this mold
IL45616A (en) Mold and process for casting hollow turbine blades of two parts
SE7904425L (en) PROCEDURE FOR STARTING AN EXTENSION PLANT
SE8501622L (en) APPLICATION OF A PROCEDURE FOR PREPARING OR IMPROVING THROUGH MOLDING MOLDING MACHINES
JPS56122659A (en) Production of ceramic insert piston
GB1254215A (en) A process and mould for producing metal refractory composite structures
SU721981A1 (en) Method of centrifugal casting of holloy bands
GB2017550A (en) Casting Aerofoils
GB1191155A (en) Method and Apparatus for Producing Pipe Couplings
GB805451A (en) Improvements in or relating to graphite moulds for foundries
GB596705A (en) Improvements in and relating to the casting of ingots
GB937236A (en) Improvements in the production of ingots
GB795593A (en) Improvements in or relating to the centrifugal casting of tubular metallic bodies in hot, permanent moulds and method of manufacturing such moulds
SU643232A1 (en) Method of removing high-strength ceramic cores from castings
GB907410A (en) Foundry cores
JPS5561368A (en) Casting method of thin-walled casting
JPS55161562A (en) Casting method of double-flanged pipe
JPH0524018A (en) Forming method of hollow ceramic formed body
CA597449A (en) Mold material for casting group ivb metals and method of making same
GB546991A (en) An improved method of producing metallic castings