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• 15 United States
• 10 France
• 8 Japan
• 7 China
• 5 Korea
• 2 Other

Patent Owner(s)

Patent Owner	Address
INSTITUT FRANCO-ALLEMAND DE RECHERCHES DE SAINT-LOUIS	68301 SAINT-LOUIS CEDEX

International Classification(s)

• F42B:EXPLOSIVE CHARGES, e.g. FOR BLASTING; FIREWORKS; A....

• 2016 Application Filing Year
• F42B Class
• 451 Applications Filed
• 354 Patents Issued To-Date
• 78.50 % Issued To-Date

Inventor(s)

Inventor Name	Address	# of filed Patents	Total Citations
Chargelegue, Dominique	Saint-Louis, FR	1	2
# of filed Patents : 1 Total Citations : 2
Decrocq, Cedric	Saint-Louis, FR	1	2
# of filed Patents : 1 Total Citations : 2
Martinez, Bastien	Saint-Louis, FR	1	2
# of filed Patents : 1 Total Citations : 2
Theodoulis, Spilios	Saint-Louis, FR	1	2
# of filed Patents : 1 Total Citations : 2
Wernert, Philippe	Saint-Louis, FR	1	2
# of filed Patents : 1 Total Citations : 2

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Patent Citation Ranking

• 2 Citation Count
• F42B Class

• 22.10 % this patent is cited more than
• 8 Age

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Maintenance Fees

Fee	Large entity fee	small entity fee	micro entity fee	due date
11.5 Year Payment	$7400.00	$3700.00	$1850.00	Oct 27, 2028

Fee	Large entity fee	small entity fee	micro entity fee
Surcharge - 11.5 year - Late payment within 6 months	$160.00	$80.00	$40.00
Surcharge after expiration - Late payment is unavoidable	$700.00	$350.00	$175.00
Surcharge after expiration - Late payment is unintentional	$1,640.00	$820.00	$410.00

Full Text

US Patent Application No: 2017/0115,103

FULL-CALIBER, SPIN-STABILIZED GUIDED PROJECTILE WITH LONG RANGE

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Abstract

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An increased range guided projectile includes overcaliber lateral moment reducing wings (10) that can be deployed. The lateral moment reducing wings (10) are designed and arranged behind the center of gravity (S) in the tail direction on the guided projectile (1) so that the pitching moment derivative coefficient (C_mα) of the guided projectile (1) is in the range of ±0.5, if the guided projectile (1) has a speed that is in the speed range of Mach 0.4 to 0.8; the lateral moment reducing wings (10) are in their deployed position; and, the canard guide device (20) does not exert any guiding moments.

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Description

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Claims

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