A passive airflow regulation system for controlling temperature of a heat-absorbing subassembly is disclosed. The passive airflow regulation system includes a duct configured to provide a conduit for an incident ambient airflow to the heat-absorbing subassembly. The duct is arranged proximate to the heat-absorbing subassembly. The airflow regulation system includes a valve configured to control passage of the incident ambient airflow through the duct. The airflow regulation system also includes an actuator employing a phase-change element configured to selectively store and release energy in response to changes in temperature and stress. The actuator is arranged at the heat-absorbing subassembly and configured to select a position for the valve between and inclusive of fully-opened and fully-closed in response to a temperature of the heat-absorbing subassembly. The airflow regulation system can be arranged on a vehicle having a vehicle body including a first body end configured to face the incident ambient airflow.

Disclosed is a method for capturing particles ejected by friction braking elements (2) of a braking system (1, 2) with disk brakes (1) of a vehicle. The braking system is equipped with a capture conduit (3) taking a form adapted to accommodate the friction braking elements (2) and to conduct, while the vehicle is moving, an air flow for cooling the friction braking elements, the conduit integrating a shutter (6) with a plate (6a) positioned upstream of the friction braking elements (2), and a unit (5) for capturing particles ejected by the friction braking elements (2). Furthermore, the shutter (6) is controlled so as to move the plate (6a) between a position of closing the conduit (3), set for vehicle travel speeds lower than a predefined threshold speed Vs, and at least one position of at least partially opening the conduit (3), for vehicle travel speeds higher than the threshold speed Vs.

Systems and methods for estimating the cooling time of a brake assembly are disclosed. Systems are provided comprising a processor, a tangible, non-transitory memory configured to communicate with the processor, the tangible, non-transitory memory having instructions stored thereon that, in response to execution by the processor, cause the processor to perform operations comprising receiving, by the processor, a first temperature of a brake assembly at a first time, receiving, by the processor, a second temperature of a brake assembly at a second time, wherein the second time occurs a fixed period after the first time, determining, by the processor, a temperature decay coefficient (“α”) of the brake assembly based on the first temperature and the second temperature and calculating, by the processor, an estimated total time to cool the brake assembly to a predetermined temperature based on the first temperature, the predetermined temperature and α.

A method of cooling an aircraft brake including a brake pack and a reservoir in the form of a removable cartridge containing a coolant. The method includes vaporizing the coolant using heat energy from the brake pack.

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.

An aircraft brake temperature control system (BTCS) 100 for controlling a temperature of a brake 220 of a landing gear 201 of the aircraft 200. The BTCS 100 includes a controller 110 configured to cause a thermal management system 2000 to regulate the temperature of the brake 220, on the basis of a selection of an objective for regulating the temperature of brake from a plurality of objectives 121, 122 for regulating the temperature of the brake. An aircraft 200 includes the BTCS; and a method 300 controls a temperature of a brake of a landing gear of an aircraft.

An aircraft brake temperature control system (BTCS) 100 for controlling a temperature of a brake 220 of a landing gear 201 of the aircraft 200. The BTCS 100 includes a controller 110 configured to cause at least one fluid moving device 230, 231, 232 to drive a flow of fluid onto the brake 220, selectively in one of a plurality of modes, to control the temperature of the brake 220. The BTCS 100 may be incorporated into an aircraft system 1000 with at least one fluid moving device 230, 231, 232, wherein the aircraft system is on an aircraft 200.

In some examples, a cooling system includes a brake assembly defining a plurality of cooling channels. The brake assembly is configured to be positioned within a wheel cavity of a wheel. The cooling system includes a distributor configured to receive a flow of cooling fluid and supply the cooling fluid to the plurality of cooling channels. One or more cooling channels are configured to receive the cooling fluid and discharge the cooling fluid into the wheel cavity of the wheel. The cooling system may include a fan configured to provide the cooling fluid to the distributor.

A brake cooling system uses a pair of subsystems to efficiently provide brake cooling and operation of the system. A first subsystem uses an axle assembly to drive one or more pumps to drive a variable speed cooling flow pump motor and a variable speed fan motor. A second subsystem includes one or more cooling flow pumps that are driven by variable speed cooling flow pump motor to supply a cooling fluid to an air-fluid heat exchanger for cooling and then supply the cooled fluid from the heat exchanger to brakes of the axle assembly. The variable speed fan motor drives a fan for the air-fluid heat exchanger for cooling of fluid passing therethrough. The system also includes a means for controlling the speed of the motors to regulate the heat exchanger operation and cooling flow through the heat exchanger and brakes of the axle assembly.

A filter device collects and stores brake particles generated by a friction brake. The filter device can be regenerated. The filter device determines that at least one boundary condition that makes it possible and/or permits the execution of regeneration of the filter device is met. In response to the determination, brake particles stored in the filter device are to be removed from the filter device.