FR2613474A1 - Element de voilure gonflable, notamment pour un engin volant - Google Patents
Element de voilure gonflable, notamment pour un engin volant Download PDFInfo
- Publication number
- FR2613474A1 FR2613474A1 FR8704724A FR8704724A FR2613474A1 FR 2613474 A1 FR2613474 A1 FR 2613474A1 FR 8704724 A FR8704724 A FR 8704724A FR 8704724 A FR8704724 A FR 8704724A FR 2613474 A1 FR2613474 A1 FR 2613474A1
- Authority
- FR
- France
- Prior art keywords
- wing element
- machine
- wing
- foam
- rigid
- 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.)
- Granted
Links
- 239000006260 foam Substances 0.000 claims abstract description 23
- 238000002347 injection Methods 0.000 claims description 9
- 239000007924 injection Substances 0.000 claims description 9
- 239000012528 membrane Substances 0.000 claims description 6
- 125000006850 spacer group Chemical group 0.000 claims description 5
- 238000006116 polymerization reaction Methods 0.000 claims description 3
- 230000008961 swelling Effects 0.000 claims description 3
- 101100205313 Caenorhabditis elegans nars-1 gene Proteins 0.000 claims 1
- 239000000463 material Substances 0.000 description 11
- 239000002131 composite material Substances 0.000 description 2
- 229920000728 polyester Polymers 0.000 description 2
- 241000446313 Lamella Species 0.000 description 1
- 239000011521 glass Substances 0.000 description 1
- 239000000203 mixture Substances 0.000 description 1
- 230000002787 reinforcement Effects 0.000 description 1
- 238000010008 shearing Methods 0.000 description 1
- 239000007787 solid Substances 0.000 description 1
- 239000000243 solution Substances 0.000 description 1
- 238000005507 spraying Methods 0.000 description 1
Classifications
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/146—Fabric fins, i.e. fins comprising at least one spar and a fin cover made of flexible sheet material
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/16—Wrap-around fins
-
- F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
- F42—AMMUNITION; BLASTING
- F42B—EXPLOSIVE CHARGES, e.g. FOR BLASTING, FIREWORKS, AMMUNITION
- F42B10/00—Means for influencing, e.g. improving, the aerodynamic properties of projectiles or missiles; Arrangements on projectiles or missiles for stabilising, steering, range-reducing, range-increasing or fall-retarding
- F42B10/02—Stabilising arrangements
- F42B10/14—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel
- F42B10/20—Stabilising arrangements using fins spread or deployed after launch, e.g. after leaving the barrel deployed by combustion gas pressure, or by pneumatic or hydraulic forces
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Toys (AREA)
Priority Applications (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8704724A FR2613474A1 (fr) | 1987-04-03 | 1987-04-03 | Element de voilure gonflable, notamment pour un engin volant |
Applications Claiming Priority (1)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR8704724A FR2613474A1 (fr) | 1987-04-03 | 1987-04-03 | Element de voilure gonflable, notamment pour un engin volant |
Publications (2)
Publication Number | Publication Date |
---|---|
FR2613474A1 true FR2613474A1 (fr) | 1988-10-07 |
FR2613474B1 FR2613474B1 (es) | 1993-02-26 |
Family
ID=9349774
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8704724A Granted FR2613474A1 (fr) | 1987-04-03 | 1987-04-03 | Element de voilure gonflable, notamment pour un engin volant |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2613474A1 (es) |
Cited By (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2639105A1 (fr) * | 1988-11-15 | 1990-05-18 | Diehl Gmbh & Co | Projectile a ailes deployables |
FR2647892A1 (fr) * | 1989-06-05 | 1990-12-07 | Diehl Gmbh & Co | Aileron deployable de missile |
FR2765676A1 (fr) * | 1989-05-23 | 1999-01-08 | Bodenseewerk Geraetetech | Engin volant avec ailes deployables |
EP1564521A1 (de) * | 2004-02-14 | 2005-08-17 | Diehl BGT Defence GmbH & Co.KG | Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln |
WO2011002530A3 (en) * | 2009-03-18 | 2011-02-24 | Raytheon Company | Reinforced inflatable wings for fitment-constrained air vehicles |
Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3633846A (en) * | 1970-05-28 | 1972-01-11 | Us Navy | Expandable aerodynamic fin |
FR2365776A1 (fr) * | 1976-09-24 | 1978-04-21 | Thomson Brandt | Empennage deployant et projectile equipe d'un tel empennage, notamment projectile pour mortier |
GB1597351A (en) * | 1971-06-10 | 1981-09-09 | British Aerospace | Missiles |
-
1987
- 1987-04-03 FR FR8704724A patent/FR2613474A1/fr active Granted
Patent Citations (3)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US3633846A (en) * | 1970-05-28 | 1972-01-11 | Us Navy | Expandable aerodynamic fin |
GB1597351A (en) * | 1971-06-10 | 1981-09-09 | British Aerospace | Missiles |
FR2365776A1 (fr) * | 1976-09-24 | 1978-04-21 | Thomson Brandt | Empennage deployant et projectile equipe d'un tel empennage, notamment projectile pour mortier |
Cited By (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
FR2639105A1 (fr) * | 1988-11-15 | 1990-05-18 | Diehl Gmbh & Co | Projectile a ailes deployables |
FR2765676A1 (fr) * | 1989-05-23 | 1999-01-08 | Bodenseewerk Geraetetech | Engin volant avec ailes deployables |
FR2647892A1 (fr) * | 1989-06-05 | 1990-12-07 | Diehl Gmbh & Co | Aileron deployable de missile |
EP1564521A1 (de) * | 2004-02-14 | 2005-08-17 | Diehl BGT Defence GmbH & Co.KG | Geschoss mit vom Geschoss-Rumpf wegklappbaren Flügeln |
WO2011002530A3 (en) * | 2009-03-18 | 2011-02-24 | Raytheon Company | Reinforced inflatable wings for fitment-constrained air vehicles |
US8104713B2 (en) | 2009-03-18 | 2012-01-31 | Raytheon Company | Reinforced inflatable wings for fitment-constrained air vehicles |
Also Published As
Publication number | Publication date |
---|---|
FR2613474B1 (es) | 1993-02-26 |
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Legal Events
Date | Code | Title | Description |
---|---|---|---|
ST | Notification of lapse |
Effective date: 20051230 |