GB742771A - A maintenance platform for aircraft - Google Patents
A maintenance platform for aircraftInfo
- Publication number
- GB742771A GB742771A GB31590/53A GB3159053A GB742771A GB 742771 A GB742771 A GB 742771A GB 31590/53 A GB31590/53 A GB 31590/53A GB 3159053 A GB3159053 A GB 3159053A GB 742771 A GB742771 A GB 742771A
- Authority
- GB
- United Kingdom
- Prior art keywords
- aircraft
- extend
- maintenance platform
- platform
- workmens
- Prior art date
- Legal status (The legal status is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the status listed.)
- Expired
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
- B64F5/60—Testing or inspecting aircraft components or systems
Landscapes
- Engineering & Computer Science (AREA)
- Manufacturing & Machinery (AREA)
- Transportation (AREA)
- Aviation & Aerospace Engineering (AREA)
- Earth Drilling (AREA)
Abstract
742,771. Scaffolding for aircraft. BLACKBURN & GENERAL AIRCRAFT, Ltd., and HALL, J. Nov. 13, 1953, No. 31590/53. Class 20(2). Two cantilever workmens' platforms A and B are temporarily attached to an aircraft and extend in opposite directions. Each platform comprises two parallel tapered girders 1 connected by braces. Four tubes 6 extend through the aircraft fuselage and are connected to the ends of the girder booms. Jacks 10 at the corners of the platform may release the load on the aircraft. Apertures are provided to accommodate propellers and engines.
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB31590/53A GB742771A (en) | 1953-11-13 | 1953-11-13 | A maintenance platform for aircraft |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
GB31590/53A GB742771A (en) | 1953-11-13 | 1953-11-13 | A maintenance platform for aircraft |
Publications (1)
Publication Number | Publication Date |
---|---|
GB742771A true GB742771A (en) | 1956-01-04 |
Family
ID=10325403
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
GB31590/53A Expired GB742771A (en) | 1953-11-13 | 1953-11-13 | A maintenance platform for aircraft |
Country Status (1)
Country | Link |
---|---|
GB (1) | GB742771A (en) |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2922498A1 (en) * | 2007-10-23 | 2009-04-24 | Aircelle Sa | AIRCRAFT AIR INLET MAINTENANCE TROLLEY FOR AIRCRAFT TURBOJET AIRCRAFT |
WO2009135975A3 (en) * | 2008-05-06 | 2010-01-28 | Eads Construcciones Aeronauticas, S.A | Device for removing and installing aircraft components |
-
1953
- 1953-11-13 GB GB31590/53A patent/GB742771A/en not_active Expired
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2922498A1 (en) * | 2007-10-23 | 2009-04-24 | Aircelle Sa | AIRCRAFT AIR INLET MAINTENANCE TROLLEY FOR AIRCRAFT TURBOJET AIRCRAFT |
WO2009053539A1 (en) * | 2007-10-23 | 2009-04-30 | Aircelle | Aircraft turbojet engine nacelle air intake maintenance trolley |
CN101835687A (en) * | 2007-10-23 | 2010-09-15 | 埃尔塞乐公司 | The maintenance trolley of aircraft turbojet engine nacelle air intake |
US9027708B2 (en) | 2007-10-23 | 2015-05-12 | Aircelle | Aircraft turbojet engine nacelle air intake maintenance trolley |
CN101835687B (en) * | 2007-10-23 | 2016-03-30 | 埃尔塞乐公司 | The maintenance trolley of aircraft turbojet engine nacelle air intake |
WO2009135975A3 (en) * | 2008-05-06 | 2010-01-28 | Eads Construcciones Aeronauticas, S.A | Device for removing and installing aircraft components |
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