This disclosure relates generally to devices which join a payload to a helicopter, and allow the payload to be easily disconnected. More particularly, this disclosure relates to a cargo hook assembly.
In cargo hook technology, to which the present disclosure relates, devices which are employed for payload releases are typically complex structures that require multiple user inputs to secure and detach the payload. Current designs all employ a load beam with or without a keeper. In terms of payload to weight ratios, cargo hooks are inefficient in comparison to other aircraft release devices, for example personnel parachute releases.
An opportunity exists to significantly reduce the weight of cargo hooks, while maintaining a large payload, using a link-less parachute release concept. The link-less cargo hook requires similar functionality while allowing for automatic engagement. Operative reliability while minimizing complexity of the assembly is a constraint that cannot be compromised in any cargo hook assembly.
Briefly stated, a cargo hook assembly comprises connector strap and a frame attached to a lower kicker, a clamp, an upper kicker, and a shaft assembly.
The connector strap has a transverse flange and a tip. The lower kicker has a ledge complementary to the transverse flange, a clip extending from the ledge, and a gap that accommodates the tip. The frame extends from a first end to a second end. The clamp pivots about a lower post of the frame adjacent the first end. The clamp contains a latch bar parallel to the lower post and a tongue extending from the end opposite the engagement with the lower post. The upper kicker is pivotally attached to the frame adjacent the second end. The shaft assembly is disposed adjacent the second end and comprises a rotatable shaft with a clamp groove complementary to the tongue and a kicker groove complementary to the upper kicker. The shaft assembly is operatively connected to a remote electrical module, a remote mechanical module, and a local mechanical release.
The transverse flange engages the ledge and propels the lower kicker towards the second end of the frame and the clip rotates the clamp towards the second end. The second kicker rotatably engages the shaft assembly at the kicker groove and the tongue engages the shaft assembly at the tongue groove. The remote electrical module, the remote mechanical module, and the local mechanical release independently rotate the rotatable shaft to engage or disengage the shaft assembly from the upper kicker and tongue.
With reference to the drawings wherein like numerals represent like parts throughout the figures, a link-less cargo hook assembly is generally designated by the numeral 10. With reference to
With reference to
The upper kicker 30 preferably comprises a pair of pivotal clamp arms 31, 32 having a J-shaped configuration. Other shapes of the pivotal clamp arms 31, 32 do not significantly depart from the scope of the present disclosure. In the depicted embodiment, the arms 31, 32 are transversely spaced at opposite ends of the pivot rod 28. The arms 31, 32 rotate about pivot rod 28 and engage shaft assembly 40 on the opposite side of frame 20. The depicted shaft assembly 40 comprises a remote electrical module 42, a remote mechanical module 44, and a local mechanical release 46. The shaft assembly 40 is depicted in greater detail in
The clamp 50 includes a latch bar 52 and a tongue 54. The clamp 50 pivots about two spaced lower posts 21 at the lower end 26 of frame 20. The tongue 54 engages a complementary support structure in shaft assembly 40. The latch bar 52 engages tip 13 of connector strap 12 to fully secure the connector strap 12 to the link-less cargo hook assembly 10.
Lower kicker 60 is retained in casing sleeve 15 of casing 14 and is movable towards the lower end 26 of frame 20. The depicted lower kicker 60 contains a ledge 64 surrounding a central gap 62 at a lower end and extends to a clip 66 at the opposite end. The clip 66 extends from the ledge 64 towards the clamp 50. The shape of the clip 66 may vary, but it is designed to close clamp 50 as the lower kicker 60 is pushed towards clamp 50. The lower kicker 60 may be retained in the casing sleeve 15 when the link-less cargo hook assembly 10 is not in use by contact with either the ledge 64 or the clip 66 with complementary structures in the casing sleeve 15 or casing 14.
As best illustrated in
Referring to
Referring to
The remote electrical module 42 is depicted in greater detail in
The remote mechanical module 44 and local mechanical release 46 are depicted in greater detail in
While a preferred embodiment has been set forth for purposes of illustration, the foregoing description should not be deemed a limitation of the invention herein. Accordingly, various modifications, adaptations and alternatives may occur to one skilled in the art without departing from the spirit of the invention and scope of the claimed coverage.
Number | Name | Date | Kind |
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2121413 | Strong | Jun 1938 | A |
3766611 | Gaylord | Oct 1973 | A |
4026594 | Kumpulainen | May 1977 | A |
4609219 | Go | Sep 1986 | A |
5273333 | Hatfield | Dec 1993 | A |
Number | Date | Country | |
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20170190549 A1 | Jul 2017 | US |
Number | Date | Country | |
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62272913 | Dec 2015 | US |