초록 ▼

A ram air channel (10) for the supply of ambient air in an aircraft includes a first air inlet (12) and a main flow channel (16) which extends downstream of the first air inlet (12). In order to guarantee that the systems on board the aircraft are supplied, in a simple and reliable way, with the req

A ram air channel (10) for the supply of ambient air in an aircraft includes a first air inlet (12) and a main flow channel (16) which extends downstream of the first air inlet (12). In order to guarantee that the systems on board the aircraft are supplied, in a simple and reliable way, with the required ambient air in any operational state of the aircraft, i.e. both during the flight and on the ground, the ram air channel (10) has a second air inlet (24) which is independent from the first air inlet (12).

대표청구항 ▼

The invention claimed is: 1. Ram air channel for supplying ambient air to a system on board an aircraft, comprising: a first air inlet; a main flow channel extending downstream of the first air inlet; a second air inlet independent from the first air inlet; a movable element located in the air flow

The invention claimed is: 1. Ram air channel for supplying ambient air to a system on board an aircraft, comprising: a first air inlet; a main flow channel extending downstream of the first air inlet; a second air inlet independent from the first air inlet; a movable element located in the air flow path of the second air inlet for setting a flow cross-section of the second air inlet, the movable element being movable between a first at least partially open position and a second closed position; and a device for creating low pressure in the second air inlet, the device including at least one of: a blower and a pump each fluidly coupled and adjacent to the second air inlet and operable to cause low pressure in the second air inlet proximate to the movable element, so as to move the movable element into the first position to at least partially open the flow cross-section of the second air inlet. 2. Ram air channel in accordance with claim 1 wherein the second air inlet is connected to the main flow channel of the ram air channel by a side channel which extends at a predetermined angle to the main flow channel. 3. Ram air channel in accordance with claim 1 wherein the first air inlet has a constant flow cross-section. 4. Ram air channel in accordance with claim 1 wherein the movable element is in the form of a flap which rotates about an axis. 5. Ram air channel in accordance with claim 1, further comprising: an electro-mechanical control device operable to assist the device in moving the movable element between the first position to at least partially open the flow cross-section of the second air inlet, and a second position to close the flow cross-section of the second air inlet. 6. Ram air channel in accordance with claim 1, further comprising: a mechanical device operable to hold the movable element in the first position to at least partially open the flow cross-section of the second air inlet, or in a second position to shut the flow cross-section of the second air inlet. 7. Ram air channel in accordance with claim 1, wherein the system on board the aircraft to be supplied with ambient air is a cooling system. 8. Process for the operation of a ram air channel for supplying ambient air a system on board an aircraft, comprising: controlling a movable element so as to set a flow cross-section of a second air inlet, the movable element being located in the air flow path of the second air inlet and being movable between a first at least partially open position and a second closed position, the aircraft having a first air inlet and a main flow channel extending downstream of the first air inlet, the controlling further including, during flight, positioning the movable element in the second position to close the flow cross-section of the second air inlet so that ambient air is supplied to the aircraft by the first air inlet only, and when the aircraft is on the ground, positioning the movable element into the first position by low pressure created by a device, thereby to at least partially open the flow cross-section of the second air inlet so that ambient air is supplied to the aircraft by the first and the second air inlets, the device including at least one of a blower and a pump each fluidly coupled and adjacent to the second air inlet and operable to cause low pressure in the second air inlet proximate to the movable element. 9. Process in accordance with claim 8, wherein the system on board the aircraft to be supplied with ambient air is a cooling system.