1. Field of the Invention
This invention relates generally to store carriers for mounting a releasable store on an aircraft and, more particularly, to a store ejection system capable of ejecting stores of various size and shapes.
2. Background of the Invention
The store referred to herein may be used to contain munitions, or to contain other material to be dropped from an aircraft. Military aircraft used to dispense bombs, rockets, and other stores in flight usually include racks located beneath the wings and fuselage, or in weapon bays designed to release the stores upon command.
At the time of target acquisition, a release mechanism is activated which results in mechanical release and subsequent forcible ejection of that weapon away from the aircraft. Presently, most state of the art bomb ejector racks utilize pyrotechnic (explosive) cartridges which, on ignition, generate high pressure gas for actuating the mechanical release mechanism, as well as for providing high pressure to ejection rams which forcibly eject the store from the aircraft.
Many new stores being developed can not be carried on conventional stores ejection systems because these weapons typically have fins, strakes, or protrusions that may hide or blanket access to the ejector rack once the store is raised into position, especially in weapon bays where access is limited.
Current bomb ejector racks require direct access during the store loading process so that cartridges can be inserted, swaybraces can be tightened, and safety pins can be installed and/or removed. New generation weapon designs have larger fins as compared to previous weapon. Also, newer aircraft are being designed with smaller weapon bays. This combination results in minimal, to no, access being available to physically reach the bomb ejector rack. Loading of weapons has become cumbersome and time consuming. In some cases, the ability to carry certain types of weapons has been lost.
Accordingly, what is needed is a stores ejection system for mounting jettisonable stores on an aircraft, where access to the stores ejection system is not required.
The present invention provides a stores ejection system that can be “blind-loaded” without the need to have physical access to the ejector rack.
The invention provides the ability to carry certain unique weapon shapes that can not be carried on current ejector racks due to the lack of access to the rack once the weapon is raised into position. The present invention incorporates a pneumatic ejection system which eliminates the need for using pyrotechnic cartridges. Moreover, the present invention allows for non-manual tightening of swaybrace arms and eliminates the need to install and remove safety pins.
In one aspect of the invention, a stores ejection system is provided including an adjustable swaybrace configured to be moved between a free hanging position and a store secure position; and a tightening screw for containing movement of the store when the adjustable swaybrace is in the store secure position.
In another aspect of the invention, a stores ejection system is provided including an adjustable swaybrace configured to be moved between a free hanging position and a store secure position; a tightening screw for containing movement of the store when the adjustable swaybrace is in the store secure position; and a hook opening mechanism which secures the store when the adjustable swaybrace is in the store secure position.
In yet another aspect of the invention, a method is provided for mounting a store to an aircraft using a store ejection system. The method includes hoisting a store into contact with a swaybrace; moving the swaybrace between a free hanging position and a store secure position using en electro-mechanical actuation device; and adjusting a tightening screw for containing movement of the store when the swaybrace is in the store secure position.
In one aspect of the invention, all functions of the ejection system may be operated from a remote control panel.
Additional advantages, objects, and features of the invention will be set forth in part in the detailed description which follows. It is to be understood that both the foregoing general description and the following detailed description are merely exemplary of the invention, and are intended to provide an overview or framework for understanding the nature and character of the invention as it is claimed.
The accompanying drawings are included to provide further understanding of the invention, illustrate various embodiments of the invention, and together with the description serve to explain the principles and operation of the invention. In the drawings, the same components have the same reference numerals. The illustrated embodiment is intended to illustrate, but not to limit the invention. The drawings include the following Figures:
A pneumatic ejection system 108 is included in ejector rack 100 to provide energy for forcible ejection of store 110. As previously discussed, most weapon ejection systems now use pyrotechnic cartridges to provide energy for forcible ejection. Pneumatic ejection system 108 eliminates the need for using pyrotechnic cartridges. Instead, energy for forcible ejection is provided by high pressure air which is generated from an on-board compressor. In one embodiment, pressurization is automatic upon application of aircraft power to the ejector rack. An operational embodiment of an exemplary pneumatic ejection system is described in U.S. Pat. No. 5,583,312, which is herein incorporated by reference for all purposes.
In one embodiment, since store 110 typically has a substantially round shape, tightening screw 308 may be mounted at an angle to centerline 304 of ejector rack 100. The angled positioning of tightening screw 308 allows the tightening screw to be directed toward the center of store 110. In this manner, mounting pads 314 may make flush contact with store 110 when store 110 is raised into position. In addition, each mounting pad 314 may include the ability to swivel to further ensure that tightening screw 308 approximates a flush contact onto store 110.
In one embodiment tightening screw 308 is adjustable between a full-up position 310 and a full-down position 312. Accordingly, depending on the type of store 110 to be mounted, tightening screw 308 may be adjusted to accept a given store 110 diameter. For example, if store 110 has a 16 inch diameter, then tightening screws 308 may be adjusted such that each mounting pad 314 contacts the surface of store 110 in a flush manner.
Swaybrace structure 102a also includes a structural housing 318 which defines a bore 320 that is positioned along centerline 304 of ejector rack 100. Bore 320 is configured to receive column 316 within housing 318. Thus, in one embodiment, column 316 may be moved in and out from housing 318 allowing swaybrace arm 302 to be moved vertically along centerline 304 a variable distance represented at 322.
In operation, as illustrated in
Referring to
In one embodiment, as shown in
Referring now to
As shown in
In one embodiment (as illustrated in
In operation, referring again to
Upon further rotation of safety shaft 402 to a second position as shown in
Prior systems typically use a “manual release” system to offload a store 110. This is typically done when an aircraft returns from a mission and store 110 has not been ejected or used over a target. Prior systems use a manual method to release the suspension hooks, which requires physical access to the rack.
The present invention provides a release system 500, shown in
Release system 500 operates to release both forward suspension hook 404a and aft suspension hook 404b (
As shown in
In operation, hook opening striker crank 504 is coupled to shaft 502, using for example, pin 512. Retraction of linear actuator 506 imparts rotation into shaft 502 causing hook opening striker crank 504 to rotate. As hook opening striker crank 504 rotates, a feature 516 on hook opening striker crank 504 contacts boss 514 on hook opening crank 510 and forces hook opening crank 510 to rotate. When hook opening crank 510 rotates it drives hook opening link 508a. Hook opening link 508a is coupled to over-center latching system 408 (see
As shown in
In operation, retraction of linear actuator 506 imparts rotation into hook opening striker crank 530 causing a feature on hook opening striker crank 530 to make contact with linkage pin 512 and impart rotation into hook opening striker crank 530. When hook opening striker crank 530 rotates it moves hook opening link 508b. Hook opening link 508b is coupled to over-center latching system 408 (see
Generally, the electro-mechanical actuators described above as used in the present invention are commanded to function by electrical switch logic from a remote panel. As shown in
In one exemplary embodiment, shown in
Typically, visual inspection of forward and aft suspension hooks 404a and 404b is made to determine if suspension hooks 404a and 404b have closed. As visual inspection may not be possible with certain stores, the present invention provides independent Safety Lock/Unlock mechanisms 400 at each suspension hook. Referring to
It will be apparent to those skilled in the art that various modifications and variations can be made to the present invention without departing from the spirit and scope of the invention. Thus it is intended that the present invention cover the modifications and variations of this invention provided they come within the scope of the appended claims and their equivalents.
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