Aircraft brake and cooling methods therefor
US-2017227079-A1 · Aug 10, 2017 · US
US2021381568A1 · US · A1
| Field | Value |
|---|---|
| Publication number | US-2021381568-A1 |
| Application number | US-202117410740-A |
| Country | US |
| Kind code | A1 |
| Filing date | Aug 24, 2021 |
| Priority date | Mar 22, 2019 |
| Publication date | Dec 9, 2021 |
| Grant date | — |
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Official abstract text for this publication.
A system, and associated method, for reducing oxidation of a friction disk may include a braking assembly comprising the friction disk and a coolant loop coupled to the braking assembly, with the coolant loop being configured to circulate liquid coolant from the braking assembly. That is, the coolant loop may be configured to reduce the temperature of the braking assembly, thus reducing the rate/extent of oxidation of the friction disks and potentially enabling the concentration of oxygen around the braking assembly to be reduced.
Opening claim text (preview).
What is claimed is: 1 . A method for reducing oxidation of a friction disk of a braking assembly of an aircraft, the method comprising: determining a status of the braking assembly, wherein the status pertains to a likelihood of oxidation of the friction disk of the braking assembly; and based on the status of the braking assembly, circulating a liquid coolant to the braking assembly to transfer heat from the friction disk to the liquid coolant. 2 . The method of claim 1 , further comprising, based on the status of the braking assembly, delivering an inert fluid to the braking assembly to reduce oxidation of the friction disk. 3 . The method of claim 2 , wherein the determining the status comprises at least one: comparing an aircraft speed to a threshold aircraft speed; comparing an aircraft deceleration to a threshold aircraft deceleration; comparing a temperature of the braking assembly to a threshold temperature of the braking assembly; comparing a braking force of the braking assembly to a threshold braking force; and determining if an aircraft landing event is occurring. 4 . The method of claim 3 , wherein the inert fluid comprises a nitrogen-enriched air stream. 5 . The method of claim 4 , further comprising configuring a membrane of an inert fluid source to separate the nitrogen-enriched air stream from air. 6 . The method of claim 1 , wherein circulating the liquid coolant to the braking assembly comprises routing the liquid coolant through a liquid coolant line defined, at least partially, by a torque tube of the braking assembly. 7 . The method of claim 6 , further comprising configuring at least one of a heat shield of the braking assembly or a wheel of the braking assembly to limit ambient airflow around the friction disk. 8 . The method of claim 6 , further comprising thermally coupling a heat exchanger to the liquid coolant line. 9 . The method of claim 8 , further comprising operably coupling a liquid coolant pump to the liquid coolant line, wherein the liquid coolant line comprises a coolant loop, and wherein the liquid coolant pump is configured to drive circulation of the liquid coolant through the coolant loop. 10 . The method of claim 9 , wherein the coolant loop comprises: a first line configured to deliver the liquid coolant to the braking assembly; a second line configured to deliver the liquid coolant from the braking assembly to the heat exchanger; and a third line configured to deliver the liquid coolant from the heat exchanger to the liquid coolant pump.
with closed cooling system · CPC title
Brakes with a plurality of rotating discs all lying side by side · CPC title
cooling control or adjustment · CPC title
Carbon · CPC title
Fully lined, i.e. braking surface extending over the entire disc circumference · CPC title
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