[특허]Hybrid spin/fin stabilized projectile

Raytheon Company

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특허 상세정보

MyON담기

내보내기 페이스북 공유 트위터 공유 카카오톡 공유

Hybrid spin/fin stabilized projectile

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F42B-010/00
미국특허분류(USC)	102/501; 102/473; 102/490; 244/003.23; 244/003.24
출원번호	UP-0821759 (2007-06-24)
등록번호	US-7849800 (2011-02-10)
발명자 / 주소	Hinsdale, Andrew J. Dryer, Richard
출원인 / 주소	Raytheon Company
대리인 / 주소	Schwegman, Lundberg & Woessner, P.A.
인용정보	피인용 횟수 : 6 인용 특허 : 3

초록
▼

A hybrid spin/fin stabilized projectile. The novel projectile includes a body, a first mechanism for spin stabilizing the body during a first mode, and a second mechanism for fin stabilizing the body during a second mode. In an illustrative embodiment, the projectile includes a rifling band adapted to engage with rifling in a gun during gun launch to impart a spin rate compatible with spin stabilization to the projectile, and a plurality of folding fins attached to an aft end of the body. A fin locking mechanism locks the fins in an undeployed position during the first mode and unlocks to deploy the fins at a predetermined time to switch the projectile to fin stabilization during the second mode. The projectile also includes a mechanism for reducing the spin of the projectile to a rate compatible with guided flight during the second mode.

대표
청구항
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What is claimed is: 1. A projectile comprising: a body; first means for spin stabilizing the body during a first mode; second means for fin stabilizing the body during a second mode; and means for reducing a spin rate of the projectile during the first mode prior to deployment of fins for the second mode, wherein the second means includes a plurality of folding fins attached to an aft end of the body, wherein the projectile also includes third means for switching from the first mode to the second mode after the spin rate is reduced, and wherein the third means includes means for locking the fins in an undeployed position during the first mode, the means for locking using centrifugal force to lock the fins in the undeployed position. 2. The projectile of claim 1 wherein the third means includes fourth means for deploying the fins to a deployed position at a predetermined time after the spin rate is reduced. 3. The projectile of claim 2 including means for deploying the fins when a predetermined environment or flight condition is satisfied. 4. The projectile of claim 2 wherein the third means includes fifth means for reducing the spin rate of the projectile. 5. The projectile of claim 4 including means for deploying the fins when the projectile is de-spun to a predetermined spin rate. 6. The projectile of claim 4 wherein the fifth means includes a rocket motor adapted to provide a counter-torque to de-spin the projectile as the rocket motor burns. 7. The projectile of claim 6 wherein the rocket motor includes a swirl nozzle. 8. The projectile of claim 6 wherein the rocket motor includes two or more nozzles angled to produce the counter-torque. 9. The projectile of claim 6 wherein the fourth means includes a fin lock adapted to lock the fins in an undeployed position during the first mode and unlock to deploy the fins in response to a pressure in the rocket motor. 10. The projectile of claim 4 wherein the fourth means includes a fin lock response to centrifugal force adapted to lock the fins in an undeployed position during the first mode and unlock to deploy the fins in response to a bias force when the bias force overcomes the centrifugal force. 11. The projectile of claim 4 wherein the projectile also includes a guidance system for controlling navigation of the projectile during the second mode. 12. The projectile of claim 11 including means for reducing the spin rate to a rate compatible with the guidance system. 13. The projectile of claim 12 wherein the fourth means includes a fin lock adapted to lock the fins in an undeployed position during the first mode and unlock to deploy the fins in response to an electrical signal provided by the guidance system. 14. A projectile comprising: a body; a rifling band adapted to engage with rifling in a gun to impart a spin rate compatible with spin stabilization to the body during gun fire; a plurality of folding fins attached to an aft end of the body; a fin locking mechanism adapted to lock the fins in an undeployed position during an initial spin stabilized mode and unlock to deploy the fins to switch the projectile to a fin stabilized mode; and a mechanism for reducing the spin rate of the projectile during the spin stabilized mode prior to deployment of the fins to enter the fin stabilized mode. 15. A projectile comprising: a body; a rifling band adapted to engage with rifling in a gun to impart a spin rate compatible with spin stabilization to the body during gun fire; a plurality of folding fins attached to an aft end of the body; a fin locking mechanism adapted to lock the fins in an undeployed position during an initial spin stabilized mode and unlock to deploy the fins to switch the projectile to a fin stabilized mode; and a mechanism for reducing the spin rate of the projectile during the spin stabilized mode prior to deployment of the fins to enter the fin stabilized mode, wherein the fin locking mechanism is adapted to deploy the fins either after a predetermined time or when a predetermined environment or flight condition is satisfied, wherein the fin locking mechanism uses centrifugal force to lock the fins in the undeployed position. 16. The projectile of claim 15 wherein the mechanism for reducing the spin rate comprises a rocket motor adapted to provide a counter-torque to de-spin the projectile as the rocket motor burns. 17. The projectile of claim 16 wherein the fin locking mechanism is responsive to a pressure in the rocket motor. 18. The projectile of claim 15 wherein the fin locking mechanism is responsive to a bias force to unlock the fins when the bias force overcomes a centrifugal force. 19. The projectile of claim 15 wherein the projectile also includes a guidance system for controlling navigation of the projectile during the fin stabilized mode. 20. The projectile of claim 19 wherein the spin rate is reduced to a rate compatible with the guidance system. 21. The projectile of claim 19 wherein the fin locking mechanism is responsive to an electrical signal provided by the guidance system. 22. A system for controlling deployment of a folding fin on a projectile comprising: first means responsive to centrifugal force for locking the fin against rotation; second means for applying a bias force on the fin such that the fin moves to an unlocked position in which it is free to rotate when the bias force overcomes the centrifugal force; and wherein the second means includes means for reducing a spin rate of the projectile while the projectile is spin stabilized prior to the fin moving to the unlocked position. 23. The system of claim 22 wherein the system includes a pivot pin placed through a pivot hole in the fin and attached to the projectile such that the fin can rotate about the pivot pin, the pivot pin having two opposing flat sides. 24. The system of claim 23 wherein the first means includes a notch in the fin next to the pivot hole adapted to engage the flat sides on the pivot pin, locking the fin against rotation, when a centrifugal force greater than the bias force is applied to the fin. 25. The system of claim 24 wherein the second means includes a bias spring adapted to apply a bias force on the fin such that pivot pin is within the pivot hole and out of the notch when the bias force is greater than the centrifugal force. 26. The system of claim 25 wherein the bias spring is adapted to provide a bias force that overcomes the centrifugal force when the projectile is at a predetermined spin rate. 27. The system of claim 26 wherein the pivot hole is positioned such that centrifugal force rotates the fin into a deployed position when the centrifugal force is less than the bias force. 28. The system of claim 27 wherein the pivot hole is positioned such that setback acceleration loads on the fin during gun launch rotate the fin into an undeployed position. 29. A lock for a folding fin on a projectile comprising: a pivot pin placed through a pivot hole in the fin and attached to the projectile such that the fin can rotate about the pivot pin, the pivot pin having two opposing flat sides; a notch in the fin next to the pivot hole adapted to engage the flat sides on the pivot pin, locking the fin against rotation, when a centrifugal force greater than a bias force is applied to the fin; and a bias spring adapted to apply a bias force on the fin such that the fin is in an unlocked position in which it is free to rotate when the bias force is greater than the centrifugal force, wherein a spin rate of the projectile is reduced while the projectile is spin stabilized prior to the fin moving to the unlocked position. 30. A method for stabilizing a guided projectile including the steps of: imparting a high spin rate compatible with spin stabilization on the projectile during launch; reducing the spin rate of the projectile to a spin rate compatible with guided flight; deploying tail fins after the spin rate is reduced to switch the projectile to fin stabilization; and applying a bias force to overcome a centrifugal force to unlock and deploy the tail fins, the centrifugal force holding the tail fins in a locked position during spin stabilization.

이 특허에 인용된 특허 (3)

이 특허를 인용한 특허 (6)

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특허 상세정보

Hybrid spin/fin stabilized projectile

초록
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대표
청구항
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이 특허에 인용된 특허 (3)

이 특허를 인용한 특허 (6)

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특허 상세정보

Hybrid spin/fin stabilized projectile

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대표청구항 ▼

이 특허에 인용된 특허 (3)

이 특허를 인용한 특허 (6)

IPC 상위 출원인

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IPC 상세정보(version : 201201)

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