Title: Revolving-cylinder jettison device for transporting and releasing buoys on and from aircraft

What we claim is:

1. A buoy jettison device having an ejection passage for transporting and ejecting buoys on and from aircraft, which comprises:

(a) a revolver cylinder mounted to rotate about a fixed central axis rigid with the aircraft, said revolver cylinder comprising a plurality of angularly spaced tubes disposed on a circle and each adapted to receive one of a long buoy or two short buoys,

(b) drive means adapted to rotate said revolver cylinder about said central axis and to place the bottom of a selected tube of said revolver cylinder to register with said ejection passage of said device,

(c) two retaining means associated with each tube of the revolver cylinder and comprising a lower retaining means disposed at the bottom of the tube and adapted to retain one of a long buoy or a lower short buoy and an upper retaining means adapted to retain an upper short buoy, each retaining means comprising a two-armed lever pivoted to the tube and adapted to take one of a working position in which one arm of the lever projects through the tube or a release position in which said lever arm does not project through the tube, spring means to maintain said lever in one of its working position or release position, and control means to selectively release one of the lower or upper retaining means of the tube registering with said ejection passage for jettisoning one of a long buoy or a short buoy,

(d) two wedging means associated with each tube of the revolver cylinder and comprising an upper wedging means disposed at the top of the tube and adapted to engage one of the top surface of a long buoy or of an upper short buoy and a lower wedging means disposed under the upper retaining means and adapted to engage the top surface of a lower short buoy, each wedging means comprising a lever pivoted to the tube and selectively urged by spring means in one of an operative buoy engaging position or an inoperative position in which it does not engage the buoy, and

(e) a laterally opening door provided on each tube for the loading thereof with one of a long buoy or with two short buoys.

2. A buoy jettison device as claimed in claim 1 further including a pivoting-bell crank lever wherein the two-armed lever of each retaining means co-acts with one end of said pivoting bell-crank lever of which the other end co-acts, when the tube carrying said retaining means registers with the ejection passage, with the movable rod of a cylinder rigid with the central axis of the device so that when the retaining lever is in its working position said bell-crank lever co-acts therewith under a spring action to maintain said retaining lever in its retaining position while, after actuation of said cylinder rod, said bent lever frees the retaining lever allowing it to take its release position under the load action and then engages again said retaining lever to lock it in its release position.

3. A buoy jettison device as claimed in claim 1 or claim 2 wherein two ejection devices responsive to pneumatic cylinders are provided, one ejection device controlling one of the long buoys or the upper short buoys, the other ejection device controlling the lower short buoys, said other ejection device retracting automatically at the end of its ejection stroke to permit one of the jettisoning and ejection of the upper short buoy associated therewith, or the possible use of the long buoy.

4. The buoy jettison device as claimed in claim 1 wherein an electric motor is provided for rotatably driving said revolver-cylinder through transmission means, means being provided for accurately positioning said revolver-cylinder in successive buoy-jettisoning positions corresponding to the selected buoy to be brought in axial alignment with a single firing barrel provided in the aircraft.


Other info:


Inventors: Guitaut, Philippe P. (Savigny sur Orge, FR)
Coutin, Pierre F. (Paris, FR)

Application Number: 06/243403
Filing Date: 1981-03-13
Publication_date: 1983-08-09
Assignee: ALKAN R & CIE (FR)

Primary Class(es): 244/137.400 244/118.100, 89/1.510, 89/1.801
Other Classes: B64D1/02; B64D1/00; B64D1/02
US Patent Ref:

1721883	July, 1929	Monteith et al.	89/15R	Flare-releasing mechanism for aircraft
2587690	March, 1952	Brereton	89/46	Hoist for conveying loads to moving platforms
2723093	November, 1955	Price et al.	244/137R	Ram-air powered, tandem rear launching system
2971731	February, 1961	Graw	244/137R	Ejection container for radio probes
3808941	May, 1974	Biggs	89/15R	DISPENSER FOR FLARES AND THE LIKE
4164887	August, 1979	Ouellette	89/15R	Multiple buoy launcher
4263835	April, 1981	Dragmuk	89/15R	Sonobuoy launcher system
4313363	February, 1982	Schreckenberg	89/46	Device for feeding of ammunition for a top mounted gun

Other Refs: DE2272835GB201004GB559725

April, 1914	89/15H
July, 1923	89/15R
March, 1944	89/15R

Primary Examiner: Barefoot, Galen L.
Assistant Examiner:
Attorney: Drucker, William A.