WO2012139185A4 - Case for packaging and transporting an aircraft brake assembly - Google Patents
Case for packaging and transporting an aircraft brake assembly Download PDFInfo
- Publication number
- WO2012139185A4 WO2012139185A4 PCT/BR2012/000103 BR2012000103W WO2012139185A4 WO 2012139185 A4 WO2012139185 A4 WO 2012139185A4 BR 2012000103 W BR2012000103 W BR 2012000103W WO 2012139185 A4 WO2012139185 A4 WO 2012139185A4
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- case
- transporting
- packaging
- aircraft brake
- brake assembly
- Prior art date
Links
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64F—GROUND OR AIRCRAFT-CARRIER-DECK INSTALLATIONS SPECIALLY ADAPTED FOR USE IN CONNECTION WITH AIRCRAFT; DESIGNING, MANUFACTURING, ASSEMBLING, CLEANING, MAINTAINING OR REPAIRING AIRCRAFT, NOT OTHERWISE PROVIDED FOR; HANDLING, TRANSPORTING, TESTING OR INSPECTING AIRCRAFT COMPONENTS, NOT OTHERWISE PROVIDED FOR
- B64F5/00—Designing, manufacturing, assembling, cleaning, maintaining or repairing aircraft, not otherwise provided for; Handling, transporting, testing or inspecting aircraft components, not otherwise provided for
- B64F5/50—Handling or transporting aircraft components
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- Braking Arrangements (AREA)
- Packaging Of Machine Parts And Wound Products (AREA)
- Packages (AREA)
Abstract
The present invention relates to a case for packaging and transporting an aircraft brake assembly which comprises two separable pieces which accommodate the brake assembly in its interior, the pieces being assembled to one another by means of a fastening system.
Claims
5
AMENDED CLAIMS
received by the International Bureau on 21 May 2013 (21.05.2013)
A case for packaging and transporting an aircraft brake, the case comprising two separable pieces, the two separable pieces defining a niche inside the case to accommodate the aircraft brake, the two pieces being assembled to one another by means of a fastening system, the case being characterized in that the niche is provided with an internal thermal insulation coating.
A case as claimed in claim 1 , characterized in that the thermal insulation coating is of Celeron.
A case as claimed in claim 1 , characterized in that the internal thermal insulation coating is of silicone.
A case as claimed in claim , characterized in that the case comprises a plurality of inspection windows.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
BRPI1101755-4 | 2011-04-15 | ||
BRPI1101755-4A2A BRPI1101755A2 (en) | 2011-04-15 | 2011-04-15 | aircraft brake set storage and carrying case |
Publications (3)
Publication Number | Publication Date |
---|---|
WO2012139185A2 WO2012139185A2 (en) | 2012-10-18 |
WO2012139185A3 WO2012139185A3 (en) | 2013-06-27 |
WO2012139185A4 true WO2012139185A4 (en) | 2013-10-03 |
Family
ID=46052480
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/BR2012/000103 WO2012139185A2 (en) | 2011-04-15 | 2012-04-13 | Case for packaging and transporting an aircraft brake assembly |
Country Status (2)
Country | Link |
---|---|
BR (1) | BRPI1101755A2 (en) |
WO (1) | WO2012139185A2 (en) |
Family Cites Families (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US4790430A (en) * | 1988-01-19 | 1988-12-13 | Thomas William A | Aircraft brake shipping container |
US5127520A (en) * | 1991-07-30 | 1992-07-07 | Thomas William A | Clamshell aircraft brake assembly shipping container |
US6036007A (en) * | 1996-08-08 | 2000-03-14 | Alejandro; Miriam L. | Transportation case for a heavy object |
US7690506B2 (en) * | 2006-05-12 | 2010-04-06 | Bill Thomas Associates, Inc. | Aircraft brake assembly container and method of using same |
FR2938511B1 (en) * | 2008-11-20 | 2011-01-14 | Messier Bugatti | CONTAINER FOR RECEIVING A BATTERY OF BRAKE DISCS, ESPECIALLY AIRCRAFT BRAKE DISCS |
-
2011
- 2011-04-15 BR BRPI1101755-4A2A patent/BRPI1101755A2/en not_active Application Discontinuation
-
2012
- 2012-04-13 WO PCT/BR2012/000103 patent/WO2012139185A2/en active Application Filing
Also Published As
Publication number | Publication date |
---|---|
WO2012139185A2 (en) | 2012-10-18 |
BRPI1101755A2 (en) | 2013-06-11 |
WO2012139185A3 (en) | 2013-06-27 |
Similar Documents
Publication | Publication Date | Title |
---|---|---|
EP2904254B8 (en) | Geared turbofan engine with high compressor exit temperature | |
IL210520A0 (en) | Turning-stabilized estimation of the attitude angels of an aircraft | |
WO2014007884A3 (en) | Turbomachine thermal management | |
WO2011094635A3 (en) | Nanocomposites with high thermoelectric performance and methods | |
EP2674706B8 (en) | Door for refrigerator and method for manufacturing the same | |
EP3057857A4 (en) | Motor vehicle with captive aircraft | |
PL3059387T3 (en) | Compound engine assembly with coaxial compressor and offset turbine section | |
EP2599719A4 (en) | Aircraft with an integral aerodynamic configuration | |
EP2377235B8 (en) | Electrical system for starting up aircraft engines | |
EP3084310A4 (en) | Gas turbine engine wall assembly with circumferential rail stud architecture | |
PL2525071T3 (en) | Continuous detonation wave engine and aircraft provided with such an engine | |
PL2675712T3 (en) | Aircraft with improved aerodynamic performance. | |
EP2753739A4 (en) | Low bfs composite and process for making the same | |
GB2577844B (en) | Aircraft engine nacelle bulkheads and methods of assembling the same | |
EP2825760A4 (en) | Aerospace engine with augmenting turbojet | |
PL2585369T3 (en) | System for real-time simulation of the environment of an aircraft engine | |
WO2015150419A3 (en) | Connector, connecting method and a production method for same | |
EP2865866A4 (en) | Fan case for aircraft engine | |
EP3049657A4 (en) | Mounting systems for gas turbine engines | |
GB2511440B (en) | Aircraft turbomachine combustion chamber module having improved air distribution within the combustion chamber and method for designing same | |
EP3058233A4 (en) | Supersonic compressor with separator | |
EP3090143A4 (en) | Gas turbine engine component mateface surfaces | |
EP3555446A4 (en) | Air turbine starter with decoupler | |
EP2792182A4 (en) | Classification of the intercepted internet payload | |
PL2874252T3 (en) | Installation assembly, integral framework formed with such installation assembly and method of assembling the integral framework |
Legal Events
Date | Code | Title | Description |
---|---|---|---|
121 | Ep: the epo has been informed by wipo that ep was designated in this application |
Ref document number: 12720073 Country of ref document: EP Kind code of ref document: A2 |
|
NENP | Non-entry into the national phase in: |
Ref country code: DE |
|
122 | Ep: pct application non-entry in european phase |
Ref document number: 12720073 Country of ref document: EP Kind code of ref document: A2 |