[특허]Techniques for articulating a nose member of a guidable projectile

HR Textron, Inc.

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Techniques for articulating a nose member of a guidable projectile

특허상세정보
국가/구분	United States(US) Patent 등록
국제특허분류(IPC7판)	F42B-015/01 F03D-009/00 F42B-015/00
미국특허분류(USC)	244/003.1; 244/003.11; 244/003.15; 290/007; 290/043; 290/044; 102/200; 102/206; 102/207
출원번호	UP-0811831 (2007-06-12)
등록번호	US-7696459 (2010-05-20)
발명자 / 주소	Harnoy, Amir
출원인 / 주소	HR Textron, Inc.
대리인 / 주소	BainwoodHuang
인용정보	피인용 횟수 : 3 인용 특허 : 23

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A guidable projectile has a nose member, a projectile body, and a nose member articulation assembly which couples the nose member to the projectile body. The nose member articulation assembly includes a stator attached to the nose member, a rotor attached to the projectile body, and rotational support hardware interconnecting the stator to the rotor. The stator defines a central axis. The rotational support hardware is constructed and arranged to guide rotation of the rotor around the central axis defined by the stator. Such a guidable projectile enables...

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What is claimed is: 1. A guidable projectile, comprising: a nose member; a projectile body; and a nose member articulation assembly which couples the nose member to the projectile body, the nose member articulation assembly including: a stator attached to the nose member, a rotor attached to the projectile body, and rotational support hardware operatively associating the stator to the rotor, the stator defining a central axis, the rotational support hardware being constructed and arranged to guide rotation of the rotor around the central axis defined by the stator. 2. A guidable projectile as in claim 1 wherein the stator of the nose member articulation assembly includes (i) a stator shaft which extends along the central axis and (ii) motor windings supported by the stator shaft; wherein the rotor of the nose member articulation assembly includes (i) a rotor housing and (ii) a set of magnets supported by the rotor housing; and wherein the nose member articulation assembly further includes a control circuit which is constructed and arranged to control current through the motor windings of the stator to control rotation of the rotor around the stator. 3. A guidable projectile as in claim 2 wherein the nose member articulation assembly further includes: a set of power cells constructed and arranged to provide power to the control circuit; and wherein the stator shaft is constructed and arranged to support the set of power cells at a fixed power cell mounting location on the stator shaft. 4. A guidable projectile as in claim 3 wherein the nose member articulation assembly further includes: a generator circuit constructed and arranged to obtain a charge from the motor windings when the rotor rotates around the stator shaft and store that charge in the set of power cells; and wherein the stator shaft is constructed and arranged to support the generator circuit at a fixed generator circuit mounting location on the stator shaft. 5. A guidable projectile as in claim 2 wherein the nose member articulation assembly further includes a nose member tilt actuator having a base and a crank arm; wherein the stator shaft is constructed and arranged to support the base of the nose member tilt actuator at a fixed nose member tilt actuator mounting location on the stator shaft; and wherein the crank arm of the nose member tilt actuator is constructed and arranged to pivotally attach to the nose member to control tilting of the nose member relative to the stator shaft. 6. A guidable projectile as in claim 5 wherein the nose member articulation assembly further includes a two-channel drive circuit having (i) a first channel constructed and arranged to drive a first motor formed by the stator and the rotor, and (ii) a second channel constructed and arranged to drive the nose member tilt actuator; and wherein the stator shaft is constructed and arranged to support the two channel drive circuit at a fixed drive circuit mounting location on the stator shaft. 7. A guidable projectile as in claim 2 wherein the rotational support hardware of the nose member articulation assembly includes (i) a first set of bearings disposed adjacent a first end of the stator shaft, and (ii) a second set of bearings disposed adjacent a second end of the stator shaft, the first and second sets of bearings being constructed and arranged to control rotation of the rotor around the stator; wherein the stator shaft defines an axial displacement unloading surface; and wherein the axial displacement unloading surface defined by the stator shaft is constructed and arranged to contact a corresponding surface on the rotor housing to prevent overloading of at least one of the first and second sets of bearings when the guidable projectile undergoes acceleration above a predefined threshold in a forward direction along the central axis defined by the stator. 8. A guidable projectile as in claim 7 wherein the rotational support hardware further includes: a set of axial loading springs constructed and arranged to maintain an axial gap between (i) the axial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing to keep (i) the axial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing out of direct contact during times when the guidable projectile undergoes acceleration below the predefined threshold in the forward direction along the central axis defined by the stator. 9. A guidable projectile as in claim 2 wherein the rotational support hardware of the nose member articulation assembly includes (i) a first set of bearings disposed adjacent a first end of the stator shaft, and (ii) a second set of bearings disposed adjacent a second end of the stator shaft, the first and second sets of bearings being constructed and arranged to control rotation of the rotor around the stator; wherein the stator shaft defines a radial displacement unloading surface; and wherein the radial displacement unloading surface defined by the stator shaft is constructed and arranged to contact a corresponding surface on the rotor housing to prevent overloading of at least one of the first and second sets of bearings when the guidable projectile undergoes acceleration above a predefined threshold in a radial direction relative to the central axis defined by the stator. 10. A guidable projectile as in claim 9 wherein the rotational support hardware further includes: a first set of tolerance rings adjacent to the first set of bearings, and a second set of tolerance rings adjacent to the second set of bearings, the first and second sets of tolerance rings being constructed and arranged to maintain a radial gap between (i) the radial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing to keep (i) the radial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing out of direct contact during times when the guidable projectile undergoes acceleration below the predefined threshold in the radial direction relative to the central axis defined by the stator. 11. A nose member articulation assembly, comprising: a stator constructed and arranged to attach to a nose member; a rotor constructed and arranged to attach to a projectile body; and rotational support hardware operatively associating the stator to the rotor, the stator defining a central axis, the rotational support hardware being constructed and arranged to guide rotation of the rotor around the central axis defined by the stator. 12. A nose member articulation assembly as in claim 11 wherein the stator includes (i) a stator shaft which extends along the central axis and (ii) motor windings supported by the stator shaft; wherein the rotor includes (i) a rotor housing and (ii) a set of magnets supported by the rotor housing; and wherein the nose member articulation assembly further comprises a control circuit which is constructed and arranged to control current through the motor windings of the stator to control rotation of the rotor around the stator. 13. A nose member articulation assembly as in claim 12, further comprising: a set of power cells constructed and arranged to provide power to the control circuit; and wherein the stator shaft is constructed and arranged to support the set of power cells at a fixed power cell mounting location on the stator shaft. 14. A nose member articulation assembly as in claim 13, further comprising: a generator circuit constructed and arranged to obtain a charge from the motor windings when the rotor rotates around the stator shaft and store that charge in the set of power cells; and wherein the stator shaft is constructed and arranged to support the generator circuit at a fixed generator circuit mounting location on the stator shaft. 15. A nose member articulation assembly as in claim 12, further comprising a nose member tilt actuator having a base and a crank arm; wherein the stator shaft is constructed and arranged to support the base of the nose member tilt actuator at a fixed nose member tilt actuator mounting location on the stator shaft; and wherein the crank arm of the nose member tilt actuator is constructed and arranged to pivotally attach to the nose member to control tilting of the nose member relative to the stator shaft. 16. A nose member articulation assembly as in claim 15, further comprising a two-channel drive circuit having (i) a first channel constructed and arranged to drive a first motor formed by the stator and the rotor, and (ii) a second channel constructed and arranged to drive the nose member tilt actuator; and wherein the stator shaft is constructed and arranged to support the two channel drive circuit at a fixed drive circuit mounting location on the stator shaft. 17. A nose member articulation assembly as in claim 12 wherein the rotational support hardware includes (i) a first set of bearings disposed adjacent a first end of the stator shaft, and (ii) a second set of bearings disposed adjacent a second end of the stator shaft, the first and second sets of bearings being constructed and arranged to control rotation of the rotor around the stator; wherein the stator shaft defines an axial displacement unloading surface; and wherein the axial displacement unloading surface defined by the stator shaft is constructed and arranged to contact a corresponding surface on the rotor housing to prevent overloading of at least one of the first and second sets of bearings when the nose member articulation assembly undergoes acceleration above a predefined threshold in a forward direction along the central axis defined by the stator. 18. A nose member articulation assembly as in claim 17 wherein the rotational support hardware further includes: a set of axial loading springs constructed and arranged to maintain an axial gap between (i) the axial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing to keep (i) the axial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing out of direct contact during times when the nose member articulation assembly undergoes acceleration below the predefined threshold in the forward direction along the central axis defined by the stator. 19. A nose member articulation assembly as in claim 12 wherein the rotational support hardware includes (i) a first set of bearings disposed adjacent a first end of the stator shaft, and (ii) a second set of bearings disposed adjacent a second end of the stator shaft, the first and second sets of bearings being constructed and arranged to control rotation of the rotor around the stator; wherein the stator shaft defines a radial displacement unloading surface; and wherein the radial displacement unloading surface defined by the stator shaft is constructed and arranged to contact a corresponding surface on the rotor housing to prevent overloading of at least one of the first and second sets of bearings when the nose member articulation assembly undergoes acceleration above a predefined threshold in a radial direction relative to the central axis defined by the stator. 20. A nose member articulation assembly as in claim 19 wherein the rotational support hardware further includes: a first set of tolerance rings adjacent to the first set of bearings, and a second set of tolerance rings adjacent to the second set of bearings, the first and second sets of tolerance rings being constructed and arranged to maintain a radial gap between (i) the radial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing to keep (i) the radial displacement unloading surface defined by the stator shaft and (ii) the corresponding surface on the rotor housing out of direct contact during times when the nose member articulation assembly undergoes acceleration below the predefined threshold in the radial direction relative to the central axis defined by the stator.

이 특허에 인용된 특허 (23)

이 특허를 인용한 특허 피인용횟수: 3

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Techniques for articulating a nose member of a guidable projectile

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Techniques for articulating a nose member of a guidable projectile

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이 특허에 인용된 특허 (23)

이 특허를 인용한 특허 피인용횟수: 3

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