Cowling with structural hand holds operating also as maintenance position bumpers
An example cowling for a rotorcraft is hinged on a stationary part of an airframe of the rotorcraft and is pivotable from a closed position into a first partially open position and thereafter into a second fully open position. The example cowling includes a rod articulated on the cowling and having a free end configured to releasably engage with the airframe to hold the cowling in the first position; and at least one handhold attached to an exterior surface of the cowling, wherein the at least one handhold has a substantially straight section that in the fully open position rests on a top portion of the airframe so as to more evenly distribute the weight of the cowling on the airframe.
1. A cowling for a rotorcraft, wherein the cowling is hinged on a stationary part of an airframe of the rotorcraft and pivotable from a closed position into a first partially open position and into a second fully open position, the cowling comprising:
a rod articulated on the cowling and having a free end configured to releasably engage with the airframe to hold the cowling in the first position; and
at least one handhold attached to an exterior surface of the cowling, wherein the at least one handhold is configured to rest on a top portion of the airframe in the fully open position.
2. The cowling of claim 1 , wherein the airframe comprises a key slot configured to engage with the free end of the rod in the first position.
3. The cowling of claim 1 , wherein the at least one handhold comprises an elongated, substantially straight section that is shaped and angled with respect to an exterior contact surface of the cowling such that a tangent extending through the straight section extends through a hinge connecting the cowling to the top portion of the airframe.
4. The cowling of claim 1 , wherein in the closed position, the cowling covers a component of the rotorcraft.
5. The cowling of claim 4 , further comprising an opening aligned with an air inlet of the component of the rotorcraft.
6. The cowling of claim 5 , wherein the at least one handhold bridges the opening in a lengthwise direction of the rotorcraft.
7. The cowling of claim 5 , wherein the opening is arranged to seal against a filter of the air inlet.
8. The cowling of claim 1 , wherein the component comprises an auxiliary power unit (APU) of the rotorcraft.
9. The cowling of claim 1 , further comprising one or more latches to secure the cowling on the airframe in the closed position.
10. The cowling of claim 1 , wherein the cowling is constructed of a composite material.
11. A rotorcraft comprising
a cowling hinged on a stationary part of an airframe of the rotorcraft and pivotable from a closed position into a first partially open position and into a second fully open position, the cowling comprising
a rod articulated on the cowling and having a free end configured to releasably engage with the airframe to hold the cowling in the first position; and
at least one handhold attached to an exterior surface of the cowling, wherein the at least one handhold is configured to rest on a top portion of the airframe in the fully open position.
12. The rotorcraft of claim 11 , wherein the free end of the rod releasably engages with a key slot.
13. The rotorcraft of claim 11 , wherein the at least one handhold comprises an elongated, substantially straight section that is shaped and angled with respect to an exterior surface of the cowling such that a tangent extending through the straight section extends through a hinge connecting the cowling to the top portion of the airframe.
14. The rotorcraft of claim 11 , wherein the at least one handhold bridges in a lengthwise direction of the rotorcraft an opening disposed in the cowling.
15. The rotorcraft of claim 14 , wherein the opening is configured to provide an air inlet of the component of the rotorcraft.
16. The rotorcraft of claim 11 , further comprising a plurality of latches configured to secure the cowling on the airframe in the closed position.
17. The rotorcraft of claim 11 , wherein the cowling is constructed of a composite material.
18. A method for facilitating access to a component of a rotorcraft disposed underneath a cowling, the method comprising:
allowing maintenance personnel to grasp at least one handhold attached to an exterior surface of the cowling and climb up to a platform;
opening the cowling to a first partially open position and supporting the cowling on an airframe of the rotorcraft in the first partially open position; and
opening the cowling from the first position to a second fully open position, wherein in the second position the at least one handhold rests on a top portion of the airframe.
19. The method of claim 18 , wherein the cowling is supported on the airframe in the first partially open position by a rod articulated on the cowling and engaging with a key slot disposed on the airframe.
20. The method of claim 18 , wherein the at least one handhold comprises an elongated, substantially straight section that is shaped and angled with respect to an exterior contact surface of the cowling such that a tangent extending through the straight section extends through a hinge connecting the cowling to the top portion of the airframe.