Effector with ejectable stealth shell

US9950781B2 · US · B2

Patent metadata
FieldValue
Publication numberUS-9950781-B2
Application numberUS-201514676047-A
CountryUS
Kind codeB2
Filing dateApr 1, 2015
Priority dateApr 2, 2014
Publication dateApr 24, 2018
Grant dateApr 24, 2018

How to read this patent

A practical reading order for non-experts. Skip the full description unless you need deep technical detail.

  1. Title

    What the patent document calls the invention.

  2. Abstract

    A short plain-language summary of the technical disclosure.

  3. Assignees and inventors

    Who owns or filed the patent and who is credited as inventor.

  4. Key dates

    Filing, priority, publication, and grant dates set the timeline.

  5. First independent claim

    The legal scope of protection — read this for what is actually claimed.

  6. CPC / IPC classifications

    Technology tags used to group this patent with similar filings.

  7. Citations and related patents

    Prior art links and similar publications in this corpus.

Abstract

Official abstract text for this publication.

An effector for an aircraft has an effector body and a stealth sheath enclosing the effector body at least in part. The stealth shell is attached to the effector body and embodied so as to be separated from the aircraft and from the effector body during flight of the aircraft carrying the effector.

First claim

Opening claim text (preview).

What is claimed is: 1. An effector for an aircraft, the effector comprising: an effector body; and a stealth shell enclosing the effector body at least in part, wherein the stealth shell is attached to the effector body, wherein the stealth shell is configured so as to be separated from the aircraft and from the effector body during flight of the aircraft carrying the effector, wherein the effector body comprises a plurality of wing-like extensions, wherein the stealth shell has a plurality of shell elements each arranged between two of the plurality of wing-like extensions and comprising recesses or indentations on each lateral edge of each respective shell element, such that the plurality of wing-like extensions are receivable between two adjacent ones of the plurality of shell elements, and wherein each of the shell elements has an angled outer contour on a side facing away from the effector body such that the stealth shell has a circumferential edge running around a direction of longitudinal extension of the entire effector body, thereby reducing a radar backscatter cross-section of the effector. 2. The effector of claim 1 , wherein the stealth shell is attached in a form-fitting manner to the effector body. 3. The effector of claim 1 , wherein the stealth shell has at least one circumferential edge running around a direction of longitudinal extension of the effector body. 4. The effector of claim 1 , wherein the stealth shell has an outer surface facing away from the effector body, and the outer surface is electrically conductive or has a radar absorber. 5. The effector of claim 1 , wherein the stealth shell has a radar-absorbing structure. 6. The effector of claim 1 , wherein the stealth shell has a separating device that is configured so as to separate the stealth shell from the effector body. 7. The effector of claim 1 , wherein the stealth shell is made at least in part of a shattering material. 8. The effector of claim 1 , wherein the stealth shell is made at least in part of a foam-like material. 9. An aircraft, comprising: a fuselage wings; and an effector, which comprises an effector body comprising a plurality of wing-like extensions; and a stealth shell enclosing the effector body at least in part, wherein the stealth shell is attached to the effector body, wherein the stealth shell is configured so as to be separated from the aircraft and from the effector body during flight of the aircraft carrying the effector, wherein the stealth shell has a plurality of shell elements each arranged between two of the plurality of wing-like extensions and comprising recesses or indentations on each lateral edge of each respective shell element, such that the plurality of wing-like extensions are receivable between two adjacent ones of the plurality of shell elements, and wherein each of the shell elements has an angled outer contour on a side facing away from the effector body such that the stealth shell has a circumferential edge running around a direction of longitudinal extension of the entire effector body, thereby reducing a radar backscatter cross-section of the effector body.

Assignees

Inventors

Classifications

  • fixedly mounted · CPC title

  • Camouflage, i.e. means or methods for concealment or disguise (for vessels B63G8/34, B63G13/02 {; sound camouflage, i.e. simulating gun fire noise, F41A33/04; dummy or decoy targets F41J; chaff per se F41J2/00; ammunition for dispensing chaff F42B5/15, F42B12/70; radar absorbing fabrics H01Q17/005}) · CPC title

  • movably mounted · CPC title

  • the armaments being firearms · CPC title

  • B64C7/00Primary

    Structures or fairings not otherwise provided for · CPC title

Patent family

Related publications grouped by family.

External sources

Frequently asked questions

Answers are generated from the same data shown on this page.

What does patent US9950781B2 cover?
An effector for an aircraft has an effector body and a stealth sheath enclosing the effector body at least in part. The stealth shell is attached to the effector body and embodied so as to be separated from the aircraft and from the effector body during flight of the aircraft carrying the effector.
Who is the assignee on this patent?
Airbus Defence & Space Gmbh
What technology area does this patent fall under?
Primary CPC classification B64C7/00. Mapped technology areas include Operations & Transport.
When was this patent published?
Publication date Tue Apr 24 2018 00:00:00 GMT+0000 (Coordinated Universal Time) (B2). Legal status and post-grant events are not shown on this page.
What related patents are in patentsdb?
We list 8 related publications on this page (citations in our corpus or others sharing the same primary CPC).