FR2683007B1 - Procede pour assembler une premiere piece en materiau sandwich et une seconde piece metallique, et assemblage obtenu. - Google Patents
Procede pour assembler une premiere piece en materiau sandwich et une seconde piece metallique, et assemblage obtenu.Info
- Publication number
- FR2683007B1 FR2683007B1 FR9113258A FR9113258A FR2683007B1 FR 2683007 B1 FR2683007 B1 FR 2683007B1 FR 9113258 A FR9113258 A FR 9113258A FR 9113258 A FR9113258 A FR 9113258A FR 2683007 B1 FR2683007 B1 FR 2683007B1
- Authority
- FR
- France
- Prior art keywords
- piece
- assembling
- sandwich material
- assembly obtained
- metal piece
- 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 - Fee Related
Links
- 239000000463 material Substances 0.000 title 1
- 239000002184 metal Substances 0.000 title 1
Classifications
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
- F02K—JET-PROPULSION PLANTS
- F02K9/00—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof
- F02K9/08—Rocket-engine plants, i.e. plants carrying both fuel and oxidant therefor; Control thereof using solid propellants
- F02K9/32—Constructional parts; Details not otherwise provided for
- F02K9/34—Casings; Combustion chambers; Liners thereof
- F02K9/343—Joints, connections, seals 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B2/00—Friction-grip releasable fastenings
- F16B2/02—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening
- F16B2/14—Clamps, i.e. with gripping action effected by positive means other than the inherent resistance to deformation of the material of the fastening using wedges
-
- 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
- F16B—DEVICES FOR FASTENING OR SECURING CONSTRUCTIONAL ELEMENTS OR MACHINE PARTS TOGETHER, e.g. NAILS, BOLTS, CIRCLIPS, CLAMPS, CLIPS OR WEDGES; JOINTS OR JOINTING
- F16B5/00—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them
- F16B5/01—Joining sheets or plates, e.g. panels, to one another or to strips or bars parallel to them by means of fastening elements specially adapted for honeycomb panels
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B15/00—Self-propelled projectiles or missiles, e.g. rockets; Guided missiles
- F42B15/36—Means for interconnecting rocket-motor and body section; Multi-stage connectors; Disconnecting means
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64G—COSMONAUTICS; VEHICLES OR EQUIPMENT THEREFOR
- B64G1/00—Cosmonautic vehicles
- B64G1/22—Parts of, or equipment specially adapted for fitting in or to, cosmonautic vehicles
- B64G1/64—Systems for coupling or separating cosmonautic vehicles or parts thereof, e.g. docking arrangements
- B64G1/641—Interstage or payload connectors
Landscapes
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Mechanical Engineering (AREA)
- Chemical & Material Sciences (AREA)
- Combustion & Propulsion (AREA)
- Aviation & Aerospace Engineering (AREA)
- Remote Sensing (AREA)
- Connection Of Plates (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9113258A FR2683007B1 (fr) | 1991-10-28 | 1991-10-28 | Procede pour assembler une premiere piece en materiau sandwich et une seconde piece metallique, et assemblage obtenu. |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR9113258A FR2683007B1 (fr) | 1991-10-28 | 1991-10-28 | Procede pour assembler une premiere piece en materiau sandwich et une seconde piece metallique, et assemblage obtenu. |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2683007A1 FR2683007A1 (fr) | 1993-04-30 |
FR2683007B1 true FR2683007B1 (fr) | 1994-01-07 |
Family
ID=9418362
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR9113258A Expired - Fee Related FR2683007B1 (fr) | 1991-10-28 | 1991-10-28 | Procede pour assembler une premiere piece en materiau sandwich et une seconde piece metallique, et assemblage obtenu. |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2683007B1 (fr) |
Families Citing this family (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2821129B1 (fr) * | 2001-02-22 | 2003-05-16 | Eads Airbus Sa | Dispositif d'assemblage d'un panneau et d'une structure, apte a transmettre des efforts importants |
DE102006022272C5 (de) | 2006-05-11 | 2013-07-25 | Repower Systems Ag | Rotorblattanschluss |
Family Cites Families (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
DE2832098C2 (de) * | 1978-07-21 | 1982-06-03 | Messerschmitt-Bölkow-Blohm GmbH, 8000 München | Anordnung zur Zug- bzw. Längskrafteinleitung bei einem Bauteil in Sandwichbauweise |
US4648227A (en) * | 1985-09-23 | 1987-03-10 | The Boeing Company | Low shock explosive joint systems |
-
1991
- 1991-10-28 FR FR9113258A patent/FR2683007B1/fr not_active Expired - Fee Related
Also Published As
Publication number | Publication date |
---|---|
FR2683007A1 (fr) | 1993-04-30 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |