FR2990415B1 - Ferrure d'un dispositif d'etayage d'un aeronef - Google Patents
Ferrure d'un dispositif d'etayage d'un aeronefInfo
- Publication number
- FR2990415B1 FR2990415B1 FR1254321A FR1254321A FR2990415B1 FR 2990415 B1 FR2990415 B1 FR 2990415B1 FR 1254321 A FR1254321 A FR 1254321A FR 1254321 A FR1254321 A FR 1254321A FR 2990415 B1 FR2990415 B1 FR 2990415B1
- Authority
- FR
- France
- Prior art keywords
- aircraft
- shaping
- fastening
- 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.)
- Active
Links
- 238000007493 shaping process Methods 0.000 title 1
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
- B64F5/10—Manufacturing or assembling aircraft, e.g. jigs therefor
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F16—ENGINEERING ELEMENTS AND UNITS; GENERAL MEASURES FOR PRODUCING AND MAINTAINING EFFECTIVE FUNCTIONING OF MACHINES OR INSTALLATIONS; THERMAL INSULATION IN GENERAL
- F16C—SHAFTS; FLEXIBLE SHAFTS; ELEMENTS OR CRANKSHAFT MECHANISMS; ROTARY BODIES OTHER THAN GEARING ELEMENTS; BEARINGS
- F16C11/00—Pivots; Pivotal connections
- F16C11/04—Pivotal connections
- F16C11/06—Ball-joints; Other joints having more than one degree of angular freedom, i.e. universal joints
-
- 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
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B66—HOISTING; LIFTING; HAULING
- B66C—CRANES; LOAD-ENGAGING ELEMENTS OR DEVICES FOR CRANES, CAPSTANS, WINCHES, OR TACKLES
- B66C1/00—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles
- B66C1/10—Load-engaging elements or devices attached to lifting or lowering gear of cranes or adapted for connection therewith for transmitting lifting forces to articles or groups of articles by mechanical means
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/32—Articulated members
-
- Y—GENERAL TAGGING OF NEW TECHNOLOGICAL DEVELOPMENTS; GENERAL TAGGING OF CROSS-SECTIONAL TECHNOLOGIES SPANNING OVER SEVERAL SECTIONS OF THE IPC; TECHNICAL SUBJECTS COVERED BY FORMER USPC CROSS-REFERENCE ART COLLECTIONS [XRACs] AND DIGESTS
- Y10—TECHNICAL SUBJECTS COVERED BY FORMER USPC
- Y10T—TECHNICAL SUBJECTS COVERED BY FORMER US CLASSIFICATION
- Y10T403/00—Joints and connections
- Y10T403/32—Articulated members
- Y10T403/32606—Pivoted
- Y10T403/32631—Universal ball and socket
Landscapes
- Engineering & Computer Science (AREA)
- Transportation (AREA)
- Manufacturing & Machinery (AREA)
- Aviation & Aerospace Engineering (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Connection Of Plates (AREA)
Priority Applications (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1254321A FR2990415B1 (fr) | 2012-05-11 | 2012-05-11 | Ferrure d'un dispositif d'etayage d'un aeronef |
US13/891,305 US9587670B2 (en) | 2012-05-11 | 2013-05-10 | Fitting for an aircraft bracing device |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR1254321A FR2990415B1 (fr) | 2012-05-11 | 2012-05-11 | Ferrure d'un dispositif d'etayage d'un aeronef |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2990415A1 FR2990415A1 (fr) | 2013-11-15 |
FR2990415B1 true FR2990415B1 (fr) | 2014-06-13 |
Family
ID=46579078
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR1254321A Active FR2990415B1 (fr) | 2012-05-11 | 2012-05-11 | Ferrure d'un dispositif d'etayage d'un aeronef |
Country Status (2)
Country | Link |
---|---|
US (1) | US9587670B2 (fr) |
FR (1) | FR2990415B1 (fr) |
Families Citing this family (8)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US9682429B2 (en) * | 2015-04-22 | 2017-06-20 | The Boeing Company | Reaction tool and method for forming openings in an aircraft fuselage joint |
US10577774B2 (en) * | 2016-05-31 | 2020-03-03 | Caterpillar Inc. | Trunnion and socket assembly |
WO2017222817A1 (fr) * | 2016-06-23 | 2017-12-28 | Hexagon Technology As | Bossage à palier interne |
DE102018112783A1 (de) * | 2018-05-29 | 2019-12-05 | Airbus Operations Gmbh | System zum Verspannen eines Einbauelements in einem Innenraum eines Fahrzeugs |
FR3096597B1 (fr) * | 2019-05-29 | 2021-05-07 | Safran Nacelles | Dispositif pour la fixation d’un outillage de levage sur porte d’inverseur de poussée de nacelle d’aéronef |
US11260954B2 (en) * | 2019-10-09 | 2022-03-01 | The Boeing Company | Apparatus for attaching aircraft wing structural components |
US11105375B2 (en) * | 2020-01-09 | 2021-08-31 | Caterpillar Inc. | Retention system for bearing member |
DE102021205352A1 (de) * | 2020-08-03 | 2022-02-03 | Sacs Aerospace Gmbh | Beschlagteil |
Family Cites Families (4)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US5141357A (en) * | 1991-01-09 | 1992-08-25 | Sundstrand Corp. | Misalignment compensating fastener insert |
US5326206A (en) * | 1993-04-19 | 1994-07-05 | Northrop Corporation | Method for compensating for bolt hole misalignment and bolt assemblies therefor |
US5823588A (en) * | 1995-11-13 | 1998-10-20 | Morghen; Manfred A. | Universal hoist assembly |
US8083175B2 (en) * | 2007-11-09 | 2011-12-27 | The Boeing Company | Loading fitting having intersecting holes in the web side and end |
-
2012
- 2012-05-11 FR FR1254321A patent/FR2990415B1/fr active Active
-
2013
- 2013-05-10 US US13/891,305 patent/US9587670B2/en active Active
Also Published As
Publication number | Publication date |
---|---|
US9587670B2 (en) | 2017-03-07 |
FR2990415A1 (fr) | 2013-11-15 |
US20130302083A1 (en) | 2013-11-14 |
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Legal Events
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