FR2640738A1 - Radome exhibiting properties of strength at high temperature - Google Patents
Radome exhibiting properties of strength at high temperature Download PDFInfo
- Publication number
- FR2640738A1 FR2640738A1 FR8916026A FR8916026A FR2640738A1 FR 2640738 A1 FR2640738 A1 FR 2640738A1 FR 8916026 A FR8916026 A FR 8916026A FR 8916026 A FR8916026 A FR 8916026A FR 2640738 A1 FR2640738 A1 FR 2640738A1
- Authority
- FR
- France
- Prior art keywords
- radome
- core
- matrix materials
- high temperature
- radome according
- 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.)
- Pending
Links
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
- F42B10/32—Range-reducing or range-increasing arrangements; Fall-retarding means
- F42B10/38—Range-increasing arrangements
- F42B10/42—Streamlined projectiles
- F42B10/46—Streamlined nose cones; Windshields; Radomes
Landscapes
- Physics & Mathematics (AREA)
- Fluid Mechanics (AREA)
- Engineering & Computer Science (AREA)
- General Engineering & Computer Science (AREA)
- Laminated Bodies (AREA)
- Reinforced Plastic Materials (AREA)
Abstract
Description
L'invention a pour objet un rad8me pour missiles, présentant des propriétés de résistance a haute température, constitué d'un noyau en matière plastique et d'une couche de couverture intérieure et extérieure mince. The invention relates to a missile rad8me having high temperature resistance properties, consisting of a plastic core and a thin inner and outer covering layer.
Les radômes de ce type sont généralement connus et leur noyau est par exemple en matière syntactique. Ils présentent cet inconvénient qu'a haute température, le matériau du coeur se fissure. En effet, par suite d'un coefficient de dilatation thermique relativement élevé et de propriétés inhérentes au matériau, ce dernier, présente une mauvaise résistance au cisaillement par rapport aux couches de couverture. Radomes of this type are generally known and their nucleus is for example in syntactic matter. They have this disadvantage that at high temperature, the material of the core cracks. Indeed, as a result of a relatively high coefficient of thermal expansion and properties inherent in the material, the latter has poor shear strength compared to the cover layers.
L'invention a donc pour but de réaliser un radôme du type précité dont les caractéristiques mécaniques, thermiques et diélectriques conviennent â une utilisation permanente à haute température, par exemple jusqu'à 320 OC. The invention therefore aims to produce a radome of the aforementioned type whose mechanical, thermal and dielectric characteristics are suitable for permanent use at high temperature, for example up to 320 OC.
Le radôme suivant l'invention a pour avantage de supprimer le collage des couches de couverture sur le noyau. Le noyau en feutre aiguilleté de polyimide est compacté sous l'effet de la température et d'une compression, de manière qu'il en résulte avantageusement un matériau déformé sphériquement, de grande rigidité et de faible poids, présentant de bonnes caractéristiques diélectriques. I1 est avantageux en outre que le feutre aiguilleté de polyimide utilisé comme matériau pour le noyau, permette d'obtenir des propriétés mécaniques orientées, telles que la dureté, l'élasticité et la résistance mécanique, ainsi qu'une faible constante diélectrique S, un angle de pertes tg w réduit et une grande rigidité. The radome according to the invention has the advantage of eliminating the sticking of the covering layers on the core. The core of needled polyimide felt is compacted under the effect of temperature and compression, so that it advantageously results in a spherically deformed material, of high rigidity and low weight, having good dielectric characteristics. It is further advantageous that the needled polyimide felt used as material for the core, makes it possible to obtain oriented mechanical properties, such as hardness, elasticity and mechanical resistance, as well as a low dielectric constant S, a reduced loss angle tg w and high rigidity.
Diverses autres caractéristiques de l'invention ressortent de la description détaillée qui suit. Un mode de réalisation de l'invention est représenté à titre d'exemple non limitatif au dessin annexé. Various other characteristics of the invention will emerge from the detailed description which follows. An embodiment of the invention is shown by way of non-limiting example in the accompanying drawing.
La figure unique est une vue en coupe d'une partie d'un radôme. The single figure is a sectional view of part of a radome.
Le radôme que l'on ne voit qu'en partie et qui est un radôme hybride, comporte un noyau 1 en feutre aiguilleté de polyimide ainsi qu'une couche de couverture intérieure 2 et une couche de couverture extérieure 3 en matériaux de matrice thermodurcissables ou thermoplastiques ou polymères pouvant être renforcés par des fibres, le renforcement par des fibres pouvant être constitué de fibres continues. Les couches de couverture 2 et 3 qui sont solidement assemblées au noyau en feutre aiguilleté de polyimide, sans apport extérieur de colle, par un procédé thermique et de compression, peuvent être réalisées dans des matières de matrice polyimide thermodurcissables, par exemple à base de résine maléinimides, en matières de matrice polyimide thermoplastiques ou on peut utiliser des résines bimaléinimides ou des polyimides aromatiques. Les matières de matrice peuvent être réalisées de préférence avec un renforcement de fibres. The radome which is only partially seen and which is a hybrid radome, comprises a core 1 of needled polyimide felt as well as an inner covering layer 2 and an outer covering layer 3 made of thermosetting matrix materials or thermoplastics or polymers which can be reinforced by fibers, the reinforcement by fibers which can consist of continuous fibers. The covering layers 2 and 3 which are securely assembled to the core of needled polyimide felt, without external glue, by a thermal and compression process, can be produced in thermosetting polyimide matrix materials, for example based on resin maleinimides, in thermoplastic polyimide matrix materials or bimalinimide resins or aromatic polyimides can be used. The matrix materials can preferably be made with fiber reinforcement.
Claims (9)
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
DE3641162 | 1988-12-07 | ||
DE19893938230 DE3938230A1 (en) | 1989-11-17 | 1989-11-17 | Radome cover esp. for missile |
Publications (1)
Publication Number | Publication Date |
---|---|
FR2640738A1 true FR2640738A1 (en) | 1990-06-22 |
Family
ID=25849941
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
FR8916026A Pending FR2640738A1 (en) | 1988-12-07 | 1989-12-05 | Radome exhibiting properties of strength at high temperature |
Country Status (1)
Country | Link |
---|---|
FR (1) | FR2640738A1 (en) |
Cited By (1)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016146716A1 (en) * | 2015-03-16 | 2016-09-22 | Daher Aerospace | Method and device for fireproofing a composite material part |
Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB908336A (en) * | 1959-01-23 | 1962-10-17 | Fmc Corp | Improvements in and relating to polymers |
US3200750A (en) * | 1962-03-15 | 1965-08-17 | Dale L Burrows | Insulating device |
US4389268A (en) * | 1980-08-06 | 1983-06-21 | Tokyo Shibaura Denki Kabushiki Kaisha | Production of laminate for receiving chemical plating |
US4706912A (en) * | 1985-12-16 | 1987-11-17 | The United States Of America As Represented By The Secretary Of The Army | Structural external insulation for hypersonic missiles |
US4732803A (en) * | 1986-10-07 | 1988-03-22 | Smith Novis W Jr | Light weight armor |
EP0323612A2 (en) * | 1988-01-07 | 1989-07-12 | General Electric Company | Interleafed fiber-reinforced thermoplastic composite |
-
1989
- 1989-12-05 FR FR8916026A patent/FR2640738A1/en active Pending
Patent Citations (6)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
GB908336A (en) * | 1959-01-23 | 1962-10-17 | Fmc Corp | Improvements in and relating to polymers |
US3200750A (en) * | 1962-03-15 | 1965-08-17 | Dale L Burrows | Insulating device |
US4389268A (en) * | 1980-08-06 | 1983-06-21 | Tokyo Shibaura Denki Kabushiki Kaisha | Production of laminate for receiving chemical plating |
US4706912A (en) * | 1985-12-16 | 1987-11-17 | The United States Of America As Represented By The Secretary Of The Army | Structural external insulation for hypersonic missiles |
US4732803A (en) * | 1986-10-07 | 1988-03-22 | Smith Novis W Jr | Light weight armor |
EP0323612A2 (en) * | 1988-01-07 | 1989-07-12 | General Electric Company | Interleafed fiber-reinforced thermoplastic composite |
Cited By (2)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
WO2016146716A1 (en) * | 2015-03-16 | 2016-09-22 | Daher Aerospace | Method and device for fireproofing a composite material part |
US10239601B2 (en) | 2015-03-16 | 2019-03-26 | Daher Aerospace | Method and device for fireproofing a part in composite material |
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