How the rotating target inside a medical tube insert is joined and finished · brazes that keep TZM below its recrystallisation temperature, barrier layers against brittle carbide, and emissive coatings outside the focal track
A medical X-ray tube anode assembly is the spinning target inside the vacuum insert: a disc of molybdenum alloy carrying a tungsten-rhenium focal track, a block of graphite brazed behind it to store heat, a stem, and the rotor that the stator drives. Since only about 1% of the electrical energy reaching the anode leaves as X-rays and the rest is heat, how the layers are chosen, joined and coated decides how much load the target accepts and how long the joint survives thermal cycling.
The joined construction of rotating anode assemblies for medical X-ray tube inserts (CT, radiography and fluoroscopy): the braze joint between the graphite heat-storage back and the TZM or other molybdenum-alloy plate, barrier and intermediate layers, emissive coatings outside the focal track, and the stem and rotor as a built subassembly. Choosing a target disc by tube load, anode angle, rotation speed and the IEC tests the tube faces is covered on the Tungsten-rhenium target disk page. Complete rotating-anode tubes, inserts and tube housing assemblies are covered on the X-ray tubes and tube assemblies page; generators, collimators, detectors and complete X-ray systems are outside this page.
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GE Medical Systems' US 6,421,423 explains the conflict: the TZM substrate is forged for strength, but brazing the graphite heat sink can need up to 1900 °C, while TZM recrystallises near or above 1400 °C and loses its elevated-temperature yield strength. [2]
Its answer for CT targets is two brazes. First a thin molybdenum alloy sheet, preferably about 0.5 mm thick, is brazed to the graphite disc with pure zirconium or pure titanium. Then this plated graphite is brazed to the TZM cap with either a Ti-Cr-Be alloy (about 72 parts titanium, 25 chromium and 3 beryllium by weight, liquidus about 1110 °C) or a Ti-Si alloy (about 91.5 parts titanium and 8.5 silicon, liquidus about 1200 °C). Molybdenum diffusing into the joint raises its remelt temperature to approximately 1700 °C, above the TZM recrystallisation point. [2]
Philips tackles a different failure: conventional joints form a Ti+TiC eutectic layer that initiates cracks. Its method puts a barrier layer such as niobium, tantalum or platinum between the graphite and the braze; the barrier must melt above the brazing temperature (for example above 1700 °C) and not form a brittle carbide. With titanium, which melts at about 1600 °C, the result is a thicker ductile pure-titanium layer and no eutectic layer subject to void formation. [1]
Editorial calculation: GE's braze liquidus of about 1110 °C sits roughly 290 °C below the stated 1400 °C recrystallisation temperature, and the Ti-Si alloy at about 1200 °C roughly 200 °C below it. [2]
Ask which braze system joins the graphite to the plate, the brazing temperature the TZM sees, whether a barrier or intermediate sheet is used, and what thermal-cycling or bond tests the joint has passed.
02
Philips' US 9,053,898 describes X-ray anodes made on a molybdenum alloy substrate such as TZM, with a tungsten-alloy focal track that it puts at 90–95% tungsten and 5–10% rhenium, and states that the targets are brazed to a graphite back for additional heat storage. For CT, the anode plate is about 8 inches in diameter and about ¾ inch thick, and the annular graphite piece, of similar diameter, is between ½ inch and 2 inches thick. [1]
In the same patent, electrons accelerated across 200,000 volts heat the anode assembly to between 1100 °C and 1400 °C, and part of the beam reflects from the focal spot and scatters inside the evacuated chamber. [1] Schwarzkopf Technologies' US 4,516,255 puts the energy balance at about 1% converted to X-rays and 99% to heat, and defines TZM as about 0.5 to 1.5% titanium, about 0.5% zirconium and optionally about 0.3% carbon by weight, the rest molybdenum. [3]
Editorial calculation: 8 inches is about 203 mm and ¾ inch about 19 mm; a graphite back of ½ to 2 inches is about 12.7 to 50.8 mm, so on the dimensions Philips gives, the graphite can be up to roughly 2.7 times as thick as the metal plate it supports (2 / 0.75).
State the tube type the assembly is for, plate diameter and thickness, focal track alloy and thickness, graphite grade and thickness, and the heat storage the tube maker specifies for the target.
03
Schwarzkopf Technologies' patent notes that oxide coatings added to TZM anodes to raise thermal emissivity lose their good emission after a short time in operation, which it attributes probably to carbon diffusing from the carbon-containing substrate into the oxide layer. [3]
Its patent places a layer of molybdenum and/or tungsten between the TZM and the oxide coating outside the focal path. The abstract and detailed description give 10 to 200 µm, preferably 40 to 50 µm, applied by flame or plasma spraying after sand blasting, with less than 10 µm ineffective and more than 200 µm uneconomical; the summary states 10 to 100 µm, so confirm which range a supplier works to. Coatings named include TiO2, Al2O3 and ZrO2, and an anneal in hydrogen at 1600 °C for about half an hour is preferred after each coating. In its comparison, two anodes of like dimensions, one with a 10 µm molybdenum interlayer under TiO2 and one without, were each run for 500 exposures on an X-ray tube test stand. [3]
Ask for the coating material and area, interlayer metal and thickness, spraying method and post-anneal, and emissivity data after a stated number of exposures.
04
| Layer | Material in the patents | Published figure |
|---|---|---|
| Focal track | Tungsten alloy, 90–95% W and 5–10% Re [1] | Focal spot region heated with the assembly to 1100–1400 °C [1] |
| Anode plate | TZM: 0.5–1.5% Ti, about 0.5% Zr, optional 0.3% C, rest Mo [3] | About 8 in diameter, ¾ in thick for CT [1]; recrystallises near 1400 °C [2] |
| Intermediate sheet | Molybdenum alloy, brazed to graphite with pure Zr or Ti [2] | About 0.5 mm [2] |
| Braze to plate | Ti-Cr-Be or Ti-Si [2]; Ti with Nb, Ta or Pt barrier [1] | Liquidus about 1110 or 1200 °C, remelt about 1700 °C [2]; Ti melts about 1600 °C [1] |
| Graphite back | Annular graphite for heat storage [1] | ½ to 2 in thick, about 8 in diameter for CT [1] |
| Emissive coating | TiO2, Al2O3 or ZrO2 over Mo or W interlayer [3] | Interlayer 10–200 µm, preferably 40–50 µm [3] |
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Paste it into your enquiry below or into an email to a maker, then replace every bracket.
Tube: [CT, radiography or fluoroscopy; tube or insert model the target fits] Plate: [alloy; diameter; thickness] Focal track: [W-Re ratio; thickness; track angle] Graphite back: [grade; thickness; diameter] Joint: [braze alloy; barrier or intermediate sheet; brazing temperature] Coating: [oxide; interlayer; area] Stem and rotor: [materials; balancing grade] Tests: [bond tests; thermal cycling; emissivity; balancing record]
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Philips' patent gives a tungsten alloy track of 90–95% tungsten and 5–10% rhenium on a molybdenum alloy (TZM) substrate. [1]
For additional heat storage capacity; Philips gives a graphite piece ½ to 2 inches thick behind an 8-inch CT anode plate. [1]
GE notes that brazing can reach 1900 °C while TZM recrystallises near 1400 °C and loses strength; its brazes melt at about 1110 or 1200 °C and remelt near 1700 °C after molybdenum diffusion. [2]
Schwarzkopf Technologies found that oxide coatings on TZM lose emissivity in service; a 10–200 µm molybdenum or tungsten interlayer is its remedy. [3]
Sources checked 2026-10-12. All three sources are granted US patents from anode and tube makers: Philips on niobium-barrier brazing, GE Medical Systems on two-step brazing for CT targets, and Schwarzkopf Technologies on emissive coatings over a metal interlayer.
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