Title:
高速滑空標的
Document Type and Number:
Japanese Patent JP4226721
Kind Code:
B2
Abstract:
A glide target comprising a fuselage having forward and aft ends. Movably attached to the fuselage is at least one control surface, while releasably attached to the fuselage is a tow line adaptor. Disposed within the fuselage is a tow line adaptor release mechanism which mechanically couples the tow line adaptor to the control surface in a manner wherein the (control surface is effectively locked into a set position until the tow line adaptor is detached from the fuselage. The glide target further comprises a glide target parachute which is disposed within the fuselage and a parachute launching mechanism which is also disposed within the fuselage and is used for selectively deploying the glide target parachute therefrom. The tow line adaptor, when attached to the fuselage, is cooperatively engaged to the parachute launching mechanism in a manner preventing the deployment of the glide target parachute from within the fuselage.
Inventors:
Roger D. Blum
Brian J. Martin
Brian J. Martin
Application Number:
JP7612699A
Publication Date:
February 18, 2009
Filing Date:
March 19, 1999
Export Citation:
Assignee:
Meggitt Defense Systems, Inc.
International Classes:
F41J9/10; B64D3/02; B64D17/80
Foreign References:
| US4000867 | ||||
| EP0387881A1 | ||||
| US3410559 |
Attorney, Agent or Firm:
Hironobu Onda
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