Canard stowage lock

Patent metadata

Field	Value
Publication number	US-10458764-B2
Application number	US-201615332425-A
Country	US
Kind code	B2
Filing date	Oct 24, 2016
Priority date	Oct 24, 2016
Publication date	Oct 29, 2019
Grant date	Oct 29, 2019

Abstract

A canard deployment mechanism includes a canard connected to a shaft that is hingedly attached to a rotatable hub that is moveable between a stowed and deployed position. The mechanism further includes a locking feature on the canard for restraining the canard in the stowed position. In an embodiment the mechanism further includes a pawl rotatably mounted on a drive gear to contact and restrain the canard in the stowed position.

First claim

The invention claimed is:

1. A canard mechanism comprising:
a canard connected to a shaft that is hingedly attached to a rotatable hub, the canard being moveable between a stowed position and a deployed position; and
a locking feature on the canard for restraining the canard in the stowed position,
wherein the locking feature comprises a locking pocket on the canard, the locking pocket comprising:
first and second lateral sides extending towards a leading edge of the canard and at a location between a trailing edge of the canard and a widest portion of the canard; and
a bottom side extending from the first lateral side to the second lateral side, wherein the first and second lateral sides converge towards and terminate at the bottom side.

2. The canard mechanism of claim 1 , further comprising:
a driven gear on a drive shaft that extends parallel to the stowed canard; and
a moveable pawl connected to one of the driven gear or the drive shaft that is positioned in the locking pocket to prevent the canard from deploying.

3. The canard mechanism of claim 2 , wherein the drive shaft and the rotational axis of the motor and gearbox are perpendicular to the hub.

4. The canard mechanism of claim 2 , wherein the moveable pawl comprises:
a hooking feature having a contact surface that faces towards the leading edge of the canard when the canard is stowed, wherein the contact surface engages the bottom side of the locking pocket when the locking feature is engaged.

5. The canard mechanism of claim 2 , wherein the drive shaft further comprises:
a threaded shaft on the drive shaft positioned on an opposite side of the driven gear from the pawl.

6. The canard mechanism of claim 5 , further comprising:
a lead nut that engages the threaded shaft, the lead nut being configured to move along the drive shaft when the threaded shaft is turned; and
a linkage connected to the lead nut and to the hub that rotates the hub when the lead nut moves in order to change the orientation of the canard when the canard is in the deployed position.

7. The canard mechanism of claim 2 , wherein the driven gear is driven by a drive gear, and wherein the driven gear and the drive shaft are driven by a motor and gearbox to restrain or release the canard, and wherein the motor and the gearbox have a rotational axis parallel to the drive shaft and the stowed canard.

8. The canard mechanism of claim 7 , wherein the pawl rotates in a plane perpendicular to the second drive shaft.

9. A canard mechanism comprising:
a canard extending along a first axis and connected to a shaft that is hingedly attached to a rotatable hub, the canard being moveable between a stowed position and a deployed position, and the canard comprising a locking pocket comprising:
first and second lateral sides extending towards a leading edge of the canard and at a location between a trailing edge of the canard and a widest portion of the canard; and
a bottom side extending from the first lateral side to the second lateral side, wherein the first and second lateral sides converge towards and terminate at the bottom side;

a driven gear mounted on a drive shaft that extends along a second axis; and
a pawl mounted on one of the driven gear or the drive shaft, the pawl being positioned in the locking pocket to restrain the canard in the stowed position;
wherein the first axis is parallel to the second axis when the canard is in the stowed position.

10. The canard mechanism of claim 9 , wherein the pawl rotates in a plane perpendicular to the second axis to lock and unlock the canard.

11. The canard mechanism of claim 9 , further comprising:
a lead nut that engages a threaded shaft on the drive shaft that is distal from the pawl, the lead nut being configured to move along the drive shaft when the threaded shaft is turned; and
a linkage connected to the lead nut and to the hub that rotates the hub when the lead nut moves in order to change the orientation of the canard when the canard is in the deployed position.

12. The canard mechanism of claim 9 , wherein the lead nut is positioned on an opposite side of the driven gear from the pawl.

13. The canard mechanism of claim 9 , further comprising:
a motor and a gearbox rotatable about a third axis parallel to the second axis to rotate a drive gear coupled to the gearbox that engages the driven gear on the drive shaft.

14. The canard mechanism of claim 9 , wherein the first axis is parallel to a hub axis when the canard is in the deployed position.

15. The canard mechanism of claim 9 , wherein the shaft is hingedly connected to the hub by a pin in a slot in the hub.

16. The canard mechanism of claim 9 , wherein the pawl comprises:
a hooking feature having a contact surface that faces towards the leading edge of the canard when the canard is stowed, wherein the contact surface engages the bottom side of the locking pocket when the locking feature is engaged.

17. A mechanism comprising:
a canard connected to a shaft that is hingedly attached to a rotatable hub, the canard being moveable between a stowed position and a deployed position, the canard comprising a locking pocket comprising:
first and second lateral sides extending towards a leading edge of the canard and at a location between a trailing edge of the canard and a widest portion of the canard; and
a bottom side extending from the first lateral side to the second lateral side, wherein the first and second lateral sides converge towards and terminate at the bottom side;

a driven shaft extending along a first axis comprising:
a driven gear;
a pawl mounted on one of the driven shaft or the driven gear for restraining the canard in the stowed position, the pawl positioned on a first side of the driven gear, wherein the pawl comprises:
a hooking feature having a contact surface that faces towards the leading edge of the canard when the canard is stowed, wherein the contact surface engages the bottom side of the locking pocket when the pawl engages the locking pocket; and

a threaded shaft on the driven shaft positioned on a second side of the driven gear, opposite of the first side and distal from the pawl;

a lead nut that engages the threaded shaft, the lead nut being configured to move along the first driven shaft when the threaded shaft is turned; and
a linkage connected to the lead nut and to the hub that rotates the hub when the lead nut moves in order to change the orientation of the canard when the canard is in the deployed position.

18. The mechanism of claim 17 , wherein the pawl rotates in a plane perpendicular to the first axis to fit in a locking pocket in the canard to restrain the canard in the stowed position.

19. The mechanism of claim 17 , wherein a motor and gearbox on a drive shaft drive the driven gear and driven shaft through a drive gear on the drive shaft.

20. The mechanism of claim 19 , wherein the pawl rotates in a plane perpendicular to a second axis of the drive shaft.

Assignees

• Rosemount Aerospace Inc

Inventors

• Willenbring Gary
• Sorensen Steven W

Classifications

• F42B10/14 Primary

  using fins spread or deployed after launch, e.g. after leaving the barrel · CPC title

• F42B10/48

  Range-reducing, destabilising or braking arrangements, {e.g. impact-braking arrangements}; Fall-retarding means, {e.g. balloons, rockets for braking or fall-retarding}(F42B10/34 takes precedence) · CPC title

• F42B10/64

  of fins · CPC title

• F42B10/62

  Steering by movement of flight surfaces · CPC title

• F42B10/20

  deployed by combustion gas pressure, or by pneumatic or hydraulic forces · CPC title