Composite pressure bulkhead
US-9776704-B1 · Oct 3, 2017 · US
US10464691B2 · US · B2
| Field | Value |
|---|---|
| Publication number | US-10464691-B2 |
| Application number | US-201816210430-A |
| Country | US |
| Kind code | B2 |
| Filing date | Dec 5, 2018 |
| Priority date | Jun 12, 2013 |
| Publication date | Nov 5, 2019 |
| Grant date | Nov 5, 2019 |
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A pressure bulkhead for a vehicle disclosed. The pressure bulkhead is configured to separate a pressurized interior from an unpressurized interior of the vehicle. The pressure bulkhead includes a bulkhead wall having a radially inner disk and a radially outer compression ring. The radially inner disk has a surface and a first thickness and the radially outer compression ring having a second thickness that is greater than the first thickness. The radially outer compression ring defines a periphery of the bulkhead wall and the second thickness of the radially outer compression ring is effective to provide a strength to oppose meridional and hoop stresses across the surface of the radially inner disk in response to a pressure differential across the bulkhead wall. The pressure bulkhead also includes an attachment ring that is affixed to the periphery of the bulkhead wall.
Opening claim text (preview).
What is claimed is: 1. A pressure bulkhead for a vehicle, wherein the pressure bulkhead is configured to separate a pressurized interior from an unpressurized interior of the vehicle, the pressure bulkhead comprising: a bulkhead wall having a periphery, a radially inner disk, and a radially outer compression ring having a thickness that is effective to provide a strength to oppose meridional and hoop stresses across the radially inner disk in response to a pressure differential across the bulkhead wall; and an attachment ring that is affixed to the periphery of the bulkhead wall, the attachment ring having an inner band and an outer band, wherein the outer band defines a concave surface that is configured to face towards the unpressurized interior of the vehicle. 2. The pressure bulkhead of claim 1 , wherein the attachment ring is composed of at least one of carbon fiber reinforced plastic and metal. 3. The pressure bulkhead of claim 1 , wherein the radially inner disk and the radially outer compression ring are composed of the same material. 4. The pressure bulkhead of claim 1 , wherein the radially inner disk and the radially outer compression ring are both composed of at least one of carbon fiber reinforced plastic and metal. 5. The pressure bulkhead of claim 1 , further comprising a plurality of attachment clips that are located along the concave surface of the outer band of the attachment ring. 6. The pressure bulkhead of claim 5 , wherein the attachment clips are configured to affix the attachment ring to a wall of the vehicle. 7. The pressure bulkhead of claim 1 , wherein the attachment ring is affixed to the bulkhead wall by mounting the periphery of the bulkhead wall on the concave surface of the attachment ring. 8. The pressure bulkhead of claim 1 , wherein the attachment ring is affixed to the bulkhead wall by mounting the radially outer compression ring on the concave surface of the attachment ring. 9. A vehicle, comprising: a pressurized interior and an unpressurized interior; and a pressure bulkhead separating the pressurized interior from the unpressurized interior of the vehicle, the pressure bulkhead comprising: a bulkhead wall having a radially inner disk and a radially outer compression ring, the radially inner disk having a surface and a first thickness and the radially outer compression ring having a second thickness that is greater than the first thickness, wherein the radially outer compression ring defines a periphery of the bulkhead wall and the second thickness of the radially outer compression ring is effective to provide a strength to oppose meridional and hoop stresses across the surface of the radially inner disk in response to a pressure differential across the bulkhead wall; and an attachment ring that is affixed to the periphery of the bulkhead wall, the attachment ring having an inner band and an outer band, wherein the outer band defines a concave surface that is configured to face towards the unpressurized interior of the vehicle. 10. The vehicle of claim 9 , wherein the attachment ring is composed of at least one of carbon fiber reinforced plastic and metal. 11. The vehicle of claim 9 , wherein the radially inner disk and the radially outer compression ring are composed of the same material. 12. The vehicle of claim 9 , wherein the radially inner disk and the radially outer compression ring are both composed of at least one of carbon fiber reinforced plastic and metal. 13. The vehicle of claim 9 , further comprising a plurality of attachment clips that are located along the concave surface of the outer band of the attachment ring. 14. The vehicle of claim 13 , wherein the attachment clips are configured to affix the attachment ring to a wall of the vehicle. 15. The vehicle of claim 9 , wherein the attachment ring is affixed to the bulkhead wall by mounting the periphery of the bulkhead wall on the concave surface of the attachment ring. 16. The vehicle of claim 9 , wherein the attachment ring is affixed to the bulkhead wall by mounting the radially outer compression ring on the concave surface of the attachment ring. 17. The vehicle of claim 9 , wherein the vehicle is one of an aircraft, a spacecraft, a marine vessel, and a land vehicle. 18. A method for mounting a bulkhead wall in an aircraft, the method comprising: affixing an attachment ring to a fuselage skin of the aircraft, wherein the attachment ring includes an inner band and an outer band, the outer band defining a concave surface; directing the concave surface of the outer band towards an unpressurized interior of the aircraft; separating the unpressurized interior from a pressurized interior of the aircraft by attaching an outer periphery of the bulkhead wall to the attachment ring, wherein the bulkhead wall has a radially inner disk and a radially outer compression ring and the radially inner disk has a first thickness and the radially outer compression ring has a second thickness that is greater than the first thickness, and wherein the radially outer compression ring defines a periphery of the bulkhead wall; and in response to experiencing a pressure differential across the bulkhead wall, providing, by the radially outer compression ring, a strength to oppose meridional and hoop stresses across the surface of the radially inner disk. 19. The method of claim 18 , further comprising: locating a plurality of attachment clips along the concave surface of the outer band of the attachment ring; and affixing the attachment ring to a wall of the aircraft by the attachment clips. 20. The method of claim 18 , further comprising: affixing the attachment ring to the bulkhead wall by mounting the periphery of the bulkhead wall on the concave surface of the attachment ring.
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