The present invention relates to latches and, more particularly, to fine-tuned, adjustable load, toggle pressure relief latches.
Removable and moveable elements installed on exterior surfaces of aerospace vehicles, such as hatches, doors, access panels, engine cowlings, nacelles, and radomes employ latches. What is desirable is a latch that has an adjustable, fine-tuned pressure relief load.
In an embodiment, a latch includes a housing having a top end, a bottom end opposite the top end, a front wall extending from the top end to the bottom end, a rear wall opposite the front wall and extending from the top end to the bottom end, a pair of sidewalls, each of which extends from the top end to the bottom end and between the front wall and the rear wall, and a floor located at the bottom end and extending between the front wall, the rear wall, and the sidewalls, the front wall, rear wall, the pair of sidewalls, and the floor forming an interior portion; and a latch mechanism located within the interior portion of the housing, the latch mechanism including an arm, a pair of socket screws, each of which is positioned rotatably within the rear wall of the housing, a pair of torsion springs, each of which is connected rotatably to the arm and engages a corresponding one of the pair of socket screws, a bolt mechanism attached rotatably to the housing proximate to the rear wall and having a first end and a second end opposite the first end, and a link having a first end and a second end opposite the first end of the link, the first end of the link being attached pivotally to the arm, and the second end of the link being attached to the bolt mechanism, wherein each of the pair of socket screws being adapted to adjust a load on a corresponding one of the torsion springs, and wherein the bolt mechanism is movable rotatably between a first position, in which the arm and the link are toggled with one another under the loads from the pair of torsion springs and the first end of the bolt mechanism is adapted to engage an external structure, and a second position, in which the link and the arm are untoggled with one another and the first end of the bolt mechanism is disengaged with the external structure.
In an embodiment, the housing includes a pair of ledges, one of the pair of ledges being located between and extends from a first corner formed by one of the pair of sidewalls, the rear wall, and the floor of the housing, and the other of the pair of ledges being located between and extends from a second corner formed by the other of the pair of sidewalls, the rear wall, and the floor of the housing, and wherein one of the pair of torsion springs rests on one of the pair of ledges, and the other of the pair of torsion springs rests on the other of the pair of ledges. In an embodiment, the housing includes a pair of holes formed within the front wall thereof, one of the pair of holes being located within one of the pair of ledges, and the other of the pair of holes being located within the other of the pair of ledges, and wherein each of the pair of holes being sized and shaped to receive a corresponding one of the pair of socket screws. In an embodiment, the arm includes a middle portion having a pair of side members extending outwardly and opposed to one another and a slot formed between the side members, the slot being sized and shaped to receive the first end of the link.
In an embodiment, the latch mechanism include a pair of bushings, each of the pair of torsion springs being positioned around a corresponding one of the bushings, and wherein the bushings are connected to the middle portion of the arm by a rivet. In an embodiment, each of the pair of torsion springs includes a first leg and a second leg, the first leg of each of the pair of torsion springs engages its corresponding one of the pair of the socket screws, and the second leg of each of the pair of torsion springs engages a corresponding one of side members of the arm. In an embodiment, each of the socket screws includes a periphery and a plurality of holes formed within the periphery, each of the plurality of holes being sized and shaped to receive a lock wire.
In an embodiment, the bolt mechanism includes a bolt positioned at the first end of the bolt mechanism, and a nut engaged threadedly with the bolt for adjusting the position of the bolt. In an embodiment, the second end of the bolt mechanism includes a slot formed therein and sized and shaped to receive an external tool for manually rotating the bolt mechanism. In an embodiment, the housing includes at least one mounting bracket. In an embodiment, the housing includes a pair of mounting brackets. In an embodiment, the housing includes a pair of support brackets, one of which extends obliquely from the rear wall and the bottom end to the top end and one of the mounting brackets proximate to one of the sidewalls, and the other of which extends obliquely from the rear wall and the bottom end to the top end and one of the mounting brackets proximate to other of the sidewalls. In an embodiment, the rear wall includes an opening positioned between the support brackets, the opening being sized and shaped to enable movement of the bolt mechanism between its first position to its second position.
In an embodiment, the latch is a fine-tuned/adjustable load, toggle-pressure relief latch which provides a fine-tuned load-range capability. The latch ensures a door of a structure can be opened when a high pressure is built up so as to prevent any loss of an internal component housed within the structure, such as an aircraft engine. The latch can be fine-tuned to a required load at an assembly level. In an embodiment, the latch is adapted for use in the aerospace field, such as aerospace doors, nacelles, etc. In other embodiments, the latch can be used in other fields and applications.
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It should be understood that the embodiments described herein are merely exemplary and that a person skilled in the art may make many variations and modifications without departing from the spirit and scope of the invention. All such variations and modifications are intended to be included within the scope of the invention as defined in the appended claims.
This application is a § 111(a) application that relates to and claims the benefit of commonly-owned, co-pending U.S. Provisional Patent Application Ser. No. 62/248,355, filed Oct. 30, 2015, entitled “FINE-TUNED, ADJUSTABLE LOAD, TOGGLE PRESSURE RELIEF LATCH,” the entirety of which is incorporated herein by reference.
Number | Name | Date | Kind |
---|---|---|---|
1206342 | Linborg | Nov 1916 | A |
2712955 | Andrews | Jul 1955 | A |
2726889 | Lawson | Dec 1955 | A |
2904141 | Henrichs | Sep 1959 | A |
2927812 | Smith | Mar 1960 | A |
2944848 | Mandolf | Jul 1960 | A |
3070395 | Morrison et al. | Dec 1962 | A |
3214207 | Swanson | Oct 1965 | A |
3259411 | Griffiths | Jul 1966 | A |
3259412 | Wheeler | Jul 1966 | A |
3341239 | Wheeler | Sep 1967 | A |
3347578 | Sheehan et al. | Oct 1967 | A |
3473693 | Fritz | Oct 1969 | A |
3571977 | Abeel | Mar 1971 | A |
3743335 | Reilhac | Jul 1973 | A |
3917327 | Plasko | Nov 1975 | A |
4053177 | Stammreich et al. | Oct 1977 | A |
4099751 | Poe et al. | Jul 1978 | A |
4116479 | Poe | Sep 1978 | A |
4130307 | Poe et al. | Dec 1978 | A |
4159137 | Richter | Jun 1979 | A |
4183564 | Poe | Jan 1980 | A |
4220364 | Poe | Sep 1980 | A |
4230352 | Sealey | Oct 1980 | A |
RE31935 | Poe | Jul 1985 | E |
4530529 | Poe et al. | Jul 1985 | A |
4538843 | Harris | Sep 1985 | A |
4602812 | Bourne | Jul 1986 | A |
4641868 | Miron | Feb 1987 | A |
4826221 | Harmon | May 1989 | A |
4828299 | Poe | May 1989 | A |
4858970 | Tedesco | Aug 1989 | A |
4911488 | Brackmann et al. | Mar 1990 | A |
4925221 | Carmody | May 1990 | A |
5152926 | Brown | Oct 1992 | A |
5228730 | Gokcebay et al. | Jul 1993 | A |
5341752 | Hambleton | Aug 1994 | A |
5609373 | Gromotka | Mar 1997 | A |
5620212 | Bourne et al. | Apr 1997 | A |
5660295 | Hroma et al. | Aug 1997 | A |
5664813 | Gromotka | Sep 1997 | A |
5984382 | Bourne | Nov 1999 | A |
6042156 | Jackson | Mar 2000 | A |
6123370 | Rozema et al. | Sep 2000 | A |
6343815 | Poe | Feb 2002 | B1 |
6361090 | Fan | Mar 2002 | B1 |
6755448 | Jackson et al. | Jun 2004 | B2 |
6913297 | Jackson et al. | Jul 2005 | B2 |
7029038 | Kobrehel | Apr 2006 | B2 |
7156429 | Eriksson | Jan 2007 | B2 |
7504601 | Belmond et al. | Mar 2009 | B2 |
7857362 | Deblock | Dec 2010 | B2 |
8479543 | Yang et al. | Jul 2013 | B2 |
8646819 | Do et al. | Feb 2014 | B2 |
8727390 | Do | May 2014 | B2 |
8864185 | Do | Oct 2014 | B2 |
9353559 | Fabre et al. | May 2016 | B2 |
20020000726 | Zintler | Jan 2002 | A1 |
20020060459 | Zintler | May 2002 | A1 |
20050087996 | Jackson et al. | Apr 2005 | A1 |
20060214431 | Helsley | Sep 2006 | A1 |
20080129056 | Hernandez | Jun 2008 | A1 |
20110109103 | Huston et al. | May 2011 | A1 |
20120102842 | Fournie et al. | May 2012 | A1 |
20120151724 | DeFrance et al. | Jun 2012 | A1 |
20150184543 | Fabre et al. | Jul 2015 | A1 |
20150184544 | Fabre et al. | Jul 2015 | A1 |
20150232189 | Hernandez | Aug 2015 | A1 |
Number | Date | Country |
---|---|---|
102191876 | Sep 2011 | CN |
104929449 | Sep 2015 | CN |
206174718 | May 2017 | CN |
202220 | Sep 1908 | DE |
29807738 | Jul 1998 | DE |
1091059 | Apr 2001 | EP |
1270406 | Jan 2003 | EP |
2031157 | Mar 2009 | EP |
2907946 | Aug 2015 | EP |
2397503 | Feb 1979 | FR |
2852049 | Sep 2004 | FR |
191493 | Jan 1923 | GB |
1497982 | Jan 1978 | GB |
1537410 | Dec 1978 | GB |
2006100654 | Sep 2006 | WO |
2006100654 | Sep 2006 | WO |
2010033026 | Mar 2010 | WO |
2010149905 | Dec 2010 | WO |
Entry |
---|
International Search Report and Written Opinion issued by the European Patent Office in International Patent Application No. PCT/US2016/059313 filed Oct. 28, 2016. |
Aerospace Latching Systems, Alcoa Fastening Systems, http://www.alcoa.com/fastening_systems/aerospace/en/product.asp?cat_id=213&prod_id=500,pp. I1-2, 159-60, and i-iii (8 pages). |
Fairchild Fasteners, Aerospace Mechanisms, “RAM™ Aerospace Latch Mechanism”, 2000 (4 pages). |
Rotary Latch #TL18261, Alcoa Fastening Systems, Mar. 2005 (1 page). |
English-language translation of WO 2010/149905 A1 (8 pages). |
International Search Report and Written Opinion dated Jul. 20, 2012, issued by the European Patent Office in connection with International Patent Application No. PCT/US2012/028418 entitled “Pin Latch Having Intermediate Position” (13 pages). |
International Search Report and Written Opinion dated Jan. 18, 2013, issued by the European Patent Office in connection with International Patent Application No. PCT/US2012/059206 entitled “Rotary-Handle Latch” (9 pages). |
International Search Report and Written Opinion dated Feb. 25, 2013, issued by the European Patent Office in connection with International Patent Application No. PCT/US2012/066039 entitled “Pin Latch With Detection Device and Movable Catch-Pin and Intermediate Position With Automatic Return Mechanism” (15 pages). |
International Search Report and Written Opinion dated Dec. 29, 2011, issued by the European Patent Office in connection with International Patent Application No. PCT/US2011/027871 entitled “Latch With Adjustable Handle” (17 pages). |
International Search Report and Written Opinion dated Jul. 15, 2011, issued by the European Patent Office in connection with International Patent Application No. PCT/US2011/027671 entitled “Latch With Adjustable Handle” (8 pages). |
International Search Report and Written Opinion dated Jun. 7, 2011, issued by the European Patent Office in connection with International Patent Application No. PCT/US2011/024031 entitled “Side-Driven Action Pin Latch” (9 pages). |
International Search Report and Written Opinion dated Jun. 9, 2016, issued by the European Patent Office in connection with International Patent Application No. PCT/US2016/024836 (13 pages). |
Alcoa Fastening Systems, Document TL22028 Rev. P, dated Jun. 18, 2015 (2 pages). |
Alcoa Fastening Systems, Document TL18356 Rev. D, dated Jul. 7, 2015 (2 pages). |
Alcoa Fastening Systems, Document TL22013 Rev. K, dated Jul. 13, 2015 (4 pages). |
Number | Date | Country | |
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20170122015 A1 | May 2017 | US |
Number | Date | Country | |
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62248355 | Oct 2015 | US |