Reinforced plastic locking dogs

1. A lockable hold open rod comprising:

an outer tube and an inner tube, the inner tube configured to slide in and out of an open end of the outer tube along a longitudinal axis;

a locking mechanism configured to selectively lock the inner tube with the outer tube;

a locking groove in an outer surface of the inner tube;

a locking dog having an inclined surface and a flat surface, the flat surface configured to slide along the outer surface of the inner tube when the locking dog is in an outer radial position and fit in the locking groove when the locking dog is in an inner radial position;

an outer housing covering the locking dog and at least part of the locking mechanism, the outer housing defining a cavity to contain the locking dog when the locking dog is in the outer radial position and also having an angled inner wall configured to engage the inclined surface of the locking dog to move the locking dog to the inner radial position when the outer housing is moved to a locking position; and

a spring biasing the outer housing to the locked position,

wherein the hold open rod is configured to be attached to access structure of an aircraft; and

wherein the outer housing is arranged on the outer tube and extends past the open end of the outer tube along the longitudinal axis.

2. The hold open rod of claim 1 , wherein the locking groove is located at a position near an end of the inner tube.

3. The hold open rod of claim 1 , further comprising multiple locking dogs.

4. The hold open rod of claim 3 , wherein there are two opposing locking dogs.

5. The hold open rod of claim 1 , wherein the locking dog is made of a reinforced plastic material.

6. The hold open rod of claim 5 , wherein the reinforced plastic material comprises a reinforcing material comprising glass fiber.

7. The hold open rod of claim 5 , wherein the reinforced plastic material is a carbon reinforced material comprising Polyamide-imide (PAI).

8. The hold open rod of claim 1 , further comprising multiple locking grooves on the inner tube thereby allowing multiple locking positions.

9. The hold open rod of claim 1 , wherein the outer housing is actuated to place the locking mechanism in the locking position by twisting the housing and then pushing the outer housing against the force of the spring.

10. A method of actuating a locking rod comprising:

arranging an outer tube and an inner tube, the inner tube configured to slide in and out of an open end of the outer tube along a longitudinal axis;

moving a lock collar axially along the outer tube;

sliding the inner tube with respect to an outer tube to align a locking groove with a locking dog, the locking dog having an inclined surface and a flat surface; and

moving the flat surface of the locking dog radially inward into the locking groove by sliding an inclined surface on the lock collar against the inclined surface on the locking dog wherein the locking dog is a reinforced plastic material,

wherein the locking rod is configured to be attached to access structure of an aircraft; and

wherein the lock collar is arranged on the outer tube and extends past the open end of the outer tube along the longitudinal axis.

11. The method of claim 10 , wherein the reinforced plastic material comprises a reinforcing material comprising glass fiber.

12. The method of claim 10 , wherein the locking dog is a carbon reinforced material comprising Polyamide-imide (PAI).

13. The method of claim 10 , further comprising sliding the locking dog along the inner tube when aligning the locking groove with the locking dog.

14. The method of claim 10 , further comprising moving a second locking dog into the locking groove.

15. The method of claim 14 , wherein the two locking dogs are oriented in opposition to each other.

16. A lockable hold open rod comprising:

an outer tube and an inner tube, the inner tube configured to slide in and out of an open end of the outer tube along a longitudinal axis;

a locking mechanism configured to selectively lock the inner tube with the outer tube;

a locking groove in an outer surface of the inner tube;

a means for radially engaging the inner tube having an inclined surface and a flat surface, the flat surface configured to slide along the outer surface of the inner tube when the means for radially engaging the inner tube is in an outer radial position and fit in the locking groove when the means for radially engaging the inner tube is in an inner radial position; and

an outer housing covering the means for radially engaging the inner tube and at least part of the locking mechanism, the outer housing defining a cavity to contain the means for radially engaging the inner tube when the means for radially engaging the inner tube is in the outer radial position and also having an angled inner wall configured to engage the inclined surface of the means for radically engaging the inner tube to move the means for radially engaging the inner tube to the inner radial position when the outer housing is moved to a locking position,

wherein the hold open rod is configured to be attached to access structure of an aircraft; and

wherein the outer housing is arranged on the outer tube and extends past the open end of the outer tube along the longitudinal axis.

17. The rod of claim 16 , wherein the means for radially engaging is made of a reinforced plastic material.