Aircraft bleed system and method of controlling an aircraft bleed system
US-9207688-B2 · Dec 8, 2015 · US
US10427795B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10427795-B2 |
| Application number | US-201514674320-A |
| Country | US |
| Kind code | B2 |
| Filing date | Mar 31, 2015 |
| Priority date | Apr 3, 2014 |
| Publication date | Oct 1, 2019 |
| Grant date | Oct 1, 2019 |
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Inter alia, an apparatus including a ramp, the ramp configured to enable variation of a cross section of a ram air passage of the apparatus. The ramp includes a first rigid member, a second rigid member and a flexible member coupled to the first rigid member and the second rigid member. The ramp is movably mounted at two ends. Moreover, a method of varying the cross section of the ram air passage of such an apparatus by moving the ramp of the apparatus is disclosed. Further, an arrangement including such an apparatus and a ram air channel communicating with the ram air passage is disclosed.
Opening claim text (preview).
The invention claimed is: 1. An apparatus comprising: a ramp configured to enable variation of a cross section of a ram air passage of the apparatus, wherein the ramp comprises: a first rigid member; a second rigid member; and a flexible member coupled to the first rigid member and the second rigid member, wherein the ramp is movably mounted at two ends; and an actuator external to the ramp which is configured to act upon the ramp for moving the ramp, wherein the actuator is mechanically coupled only to a center region of the flexible member so that a radius of curvature of the flexible member substantially decreases as the cross section of the ram air passage decreases, and wherein the ramp is configured to entirely close the ram air passage. 2. The apparatus according to claim 1 , wherein the ramp is configured to be continuously movable, and wherein the flexible member is configured to exhibit continuous curvatures. 3. The apparatus according to claim 1 , wherein the apparatus forms part of an intake of a ram air channel. 4. The apparatus according to claim 1 , wherein the apparatus forms part of an outlet of a ram air channel. 5. The apparatus according to claim 1 , wherein the ram air passage is an aircraft ram air channel. 6. The apparatus according to claim 1 , wherein at least one movably mounted end of the ramp is an end of the flexible member. 7. The apparatus according to claim 1 , wherein at least one of the first rigid member and the second rigid member is movably mounted. 8. The apparatus according to claim 1 , wherein at least one end of the ramp is swivel-mounted. 9. An arrangement comprising: an apparatus comprising: a ramp configured to enable variation of a cross section of a ram air passage of the apparatus, wherein the ramp comprises: a first rigid member; a second rigid member; and a flexible member coupled to the first rigid member and the second rigid member, wherein the ramp is movably mounted at two ends; and an actuator external to the ramp which is configured to act upon the ramp for moving the ramp, wherein the actuator is mechanically coupled only to a center region of the flexible member so that a radius of curvature of the flexible member substantially decreases as the cross section of the ram air passage decreases, and wherein the ramp is configured to entirely close the ram air passage; and a ram air channel communicating with the ram air passage. 10. A method for varying a cross section of a ram air passage of an apparatus, comprising: providing an apparatus comprising: a ramp, the ramp being configured to enable variation of a cross section of a ram air passage of the apparatus, the ramp comprising: a first rigid member, a second rigid member, and a flexible member coupled to the first rigid member and the second rigid member, wherein the ramp is movably mounted at two ends, and an actuator external to the ramp which is configured to act upon the ramp, wherein the actuator is mechanically coupled only to a center region of the flexible member so that a radius of curvature of the flexible member substantially decreases as the cross section of the ram air passage decreases, and wherein the ramp is configured to entirely close the ram air passage; and moving the ramp of the apparatus to vary the cross section of the ram air passage of the apparatus by actuating the actuator.
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