Patent US4736669A successfully refreshed from Google Patents.
US4736669A
Expired / Lapsed
US
⏱️ 0.0 years remaining
Aircraft missile launcher mounting apparatus
Assignee: Varo Inc
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Filing: 1987-02-20
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Granted: 1988-04-12
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Expires: 2007-02-20
Abstract
Abstract A missile launcher is disclosed having an elongate planar platform (28) formed integral with the body of the launcher (26). Plural bomb rack fasteners (34, 36) and pylon mounting lugs (38, 40) are fixed to the platform surface (28) to accommodate different aircraft types. Plural sway braces (46) are removably fixed to the side edges of the platform surface (28). Each sway brace (46) can be fixed to desired positions along the side edges of the platform surface (28) to also accommodate different aircraft type mounting apparatus.
Inventors
- 👤 Kenneth R. Long
- 👤 Gary D. Poole
- 👤 David A. Witt
- 👤 Ronald L. Dale
Bibliographic Details
Application Number
—
Jurisdiction
US
Data Source
google_patents
Last Synchronized
2026-11-01 07:15
CPC Classifications
B; B64; B64D; B64D7/00; B64D7/08; F; F41; F41F; F41F3/00; F41F3/04; F41F3/06
Claims Analysis
Total Claims: 13
Claim 1
Independent Claim
94 words
A missile launcher of the type adapted to be attached to an aircraft, comprising: an elongate body forming a housing of said launcher; an elongate platform having opposing side edges, and formed integral with said launcher body for strengthening said launcher; a pair of elongate recessed areas formed in said launcher body located adjacent said paltform on opposing sides thereof; and a plurality of sway braces removably fixed to said opposing side edges of said platform and engageable within said recessed areas to provide sway stability to said launcher when fixed to the aircraft.
Claim 2
Dependent Claim
94 words
A missile launcher of the type adapted to be attached to an aircraft, comprising: an elongate body forming a housing of said launcher; an elongate platform having opposing side edges, and formed integral with said launcher body for strengthening said launcher; a pair of elongate recessed areas formed in said launcher body located adjacent said paltform on opposing sides thereof; and a plurality of sway braces removably fixed to said opposing side edges of said platform and engageable within said recessed areas to provide sway stability to said launcher when fixed to the aircraft.
Claim 3
Dependent Claim
20 words
The missile launcher of claim 1 further including plural fastening means for fastening said launcher to different types of aircrafts.
Claim 4
Dependent Claim
30 words
The missile launcher of claim 1 wherein said platform is of the type having a side edge with a plurality of threaded holes for removably fixing said sway braces thereto.
Claim 5
Dependent Claim
32 words
The missile launcher of claim 3 wherein said platform includes a plurality of threaded holes spaced along another side edge thereof so as to fix other sway braches at desired positions therealong.
Claim 6
Dependent Claim
13 words
The missile launcher of claim 1 wherein said sway braces are generally hollow.
Claim 7
Dependent Claim
23 words
The missile launcher of claim 1 wherein said sway braces each include a foot for flush engagement with the body of the launcher.
Claim 8
Dependent Claim
27 words
The missile launcher of claim 6 further including means on said launcher body for abutting each said foot to thereby provide load support to said sway braces.
Claim 9
Dependent Claim
115 words
A missile launcher of the type adapted to be attached to an aircraft, comprising: an elongate body forming a housing of said launcher; an elongate platform having opposing side edges, and formed integral with said launcher body for strengthening said launcher; a pair of elongate recessed areas formed in said launcher body located adjacent said platform on opposing sides thereof; a plurality of sway braces removably fixed to said opposing side edges of said platform and engageable within said recessed areas to provide sway stability to said launcher when fixed to the aircraft; and said platform including in each said side edge thereof a plurality of dovetail mortises for removably fixing said sway braces thereto.
Claim 10
Dependent Claim
115 words
A missile launcher of the type adapted to be attached to an aircraft, comprising: an elongate body forming a housing of said launcher; an elongate platform having opposing side edges, and formed integral with said launcher body for strengthening said launcher; a pair of elongate recessed areas formed in said launcher body located adjacent said platform on opposing sides thereof; a plurality of sway braces removably fixed to said opposing side edges of said platform and engageable within said recessed areas to provide sway stability to said launcher when fixed to the aircraft; and said platform including in each said side edge thereof a plurality of dovetail mortises for removably fixing said sway braces thereto.
Claim 11
Dependent Claim
17 words
The missile launcher of claim 8 wherein each said sway brace includes a plurality of dovetail tenons.
Claim 12
Dependent Claim
21 words
The missile launcher of claim 9 wherein said sway braces each include means for abutting engagement body portion of the launcher.
Claim 13
Dependent Claim
40 words
The missile launcher of claim 10 wherein said sway braces each include a support foot for providing said abutting engagement with the body of the launcher, and further including means for fixing each said support foot to the launcher body.
References Cited (Backward Citations)
USPTO Annuity & Maintenance Windows
| Annuity Stage | Window Opens | Payment Deadline | Surcharge Period Until | Estimated Fee | Status |
|---|---|---|---|---|---|
| 3.5 Years (Year 4) | 1991-04-12 | 1991-10-12 | 1992-04-12 | $2000.00 | Window Closed / Lapsed |
| 7.5 Years (Year 8) | 1995-04-12 | 1995-10-12 | 1996-04-12 | $3760.00 | Window Closed / Lapsed |
| 11.5 Years (Year 12) | 1999-04-12 | 1999-10-12 | 2000-04-12 | $7700.00 | Window Closed / Lapsed |