BR8601586A - Aviao de caca tatico super agil e processo de pilotar o mesmo - Google Patents

Aviao de caca tatico super agil e processo de pilotar o mesmo

Info

Publication number
BR8601586A
BR8601586A BR8601586A BR8601586A BR8601586A BR 8601586 A BR8601586 A BR 8601586A BR 8601586 A BR8601586 A BR 8601586A BR 8601586 A BR8601586 A BR 8601586A BR 8601586 A BR8601586 A BR 8601586A
Authority
BR
Brazil
Prior art keywords
superagile
flight
aircraft
supernormal
tactical
Prior art date
Application number
BR8601586A
Other languages
English (en)
Inventor
Thomas H Strom
Original Assignee
Dei Tech Inc
Priority date (The priority date is an assumption and is not a legal conclusion. Google has not performed a legal analysis and makes no representation as to the accuracy of the date listed.)
Filing date
Publication date
Family has litigation
First worldwide family litigation filed litigation Critical https://patents.darts-ip.com/?family=24898808&utm_source=google_patent&utm_medium=platform_link&utm_campaign=public_patent_search&patent=BR8601586(A) "Global patent litigation dataset” by Darts-ip is licensed under a Creative Commons Attribution 4.0 International License.
Application filed by Dei Tech Inc filed Critical Dei Tech Inc
Publication of BR8601586A publication Critical patent/BR8601586A/pt

Links

Classifications

    • F—MECHANICAL ENGINEERING; LIGHTING; HEATING; WEAPONS; BLASTING
    • F02—COMBUSTION ENGINES; HOT-GAS OR COMBUSTION-PRODUCT ENGINE PLANTS
    • F02K—JET-PROPULSION PLANTS
    • F02K1/00—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto
    • F02K1/002—Plants characterised by the form or arrangement of the jet pipe or nozzle; Jet pipes or nozzles peculiar thereto with means to modify the direction of thrust vector
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C13/00—Control systems or transmitting systems for actuating flying-control surfaces, lift-increasing flaps, air brakes, or spoilers
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C15/00—Attitude, flight direction, or altitude control by jet reaction
    • B64C15/14—Attitude, flight direction, or altitude control by jet reaction the jets being other than main propulsion jets
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C39/00—Aircraft not otherwise provided for
    • B64C39/12—Canard-type aircraft
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/04—Noseplanes
    • B—PERFORMING OPERATIONS; TRANSPORTING
    • B64—AIRCRAFT; AVIATION; COSMONAUTICS
    • B64C—AEROPLANES; HELICOPTERS
    • B64C5/00—Stabilising surfaces
    • B64C5/10—Stabilising surfaces adjustable
    • B64C5/16—Stabilising surfaces adjustable about spanwise axes
BR8601586A 1985-04-09 1986-04-08 Aviao de caca tatico super agil e processo de pilotar o mesmo BR8601586A (pt)

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US72166485A 1985-04-09 1985-04-09

Publications (1)

Publication Number Publication Date
BR8601586A true BR8601586A (pt) 1986-12-30

Family

ID=24898808

Family Applications (1)

Application Number Title Priority Date Filing Date
BR8601586A BR8601586A (pt) 1985-04-09 1986-04-08 Aviao de caca tatico super agil e processo de pilotar o mesmo

Country Status (8)

Country Link
US (1) US4896846A (pt)
EP (1) EP0202020B1 (pt)
JP (1) JP2534666B2 (pt)
AT (1) ATE51368T1 (pt)
BR (1) BR8601586A (pt)
DE (1) DE3669852D1 (pt)
ES (1) ES9100002A1 (pt)
IL (1) IL78454A (pt)

Families Citing this family (27)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
US4767085A (en) * 1986-10-27 1988-08-30 Grumman Aerospace Corporation Synthetic speed stability flight control system
US5050819A (en) * 1990-08-10 1991-09-24 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Rotatable non-circular forebody flow controller
US5249762A (en) * 1990-08-21 1993-10-05 Eidetics Internation, Inc. Strakes for landing speed reduction
US5176338A (en) * 1991-03-08 1993-01-05 The United States Of America As Represented By The Secretary Of The Air Force N-dimensional fighter aircraft
US5273237A (en) * 1992-11-02 1993-12-28 The United States Of America As Represented By The Secretary Of The Air Force Forebody nozzle for aircraft directional control
US5398888A (en) * 1993-05-12 1995-03-21 Northrop Grumman Corporation Skewed hinge control surface
US5454530A (en) * 1993-05-28 1995-10-03 Mcdonnell Douglas Helicopter Company Canard rotor/wing
FR2719548B1 (fr) * 1994-05-03 1996-07-05 Aerospatiale Avion de transport à empennage avant.
US7240878B2 (en) * 1996-05-13 2007-07-10 Andrew James Towne High wing monoplane aerospace plane based fighter
US5899410A (en) * 1996-12-13 1999-05-04 Mcdonnell Douglas Corporation Aerodynamic body having coplanar joined wings
US5984229A (en) * 1997-06-02 1999-11-16 Boeing North American, Inc. Extremely short takeoff and landing of aircraft using multi-axis thrust vectoring
US5927645A (en) * 1998-01-15 1999-07-27 Northrop Grumman Corporation Shovel nose pneumatic vortex control
GB2341155A (en) * 1998-03-25 2000-03-08 British Aerospace V/STOL aircraft
DE10145284A1 (de) * 2001-08-06 2003-03-06 Astrium Gmbh Vorrichtung zum Überschalltransport
US6561456B1 (en) * 2001-12-06 2003-05-13 Michael Thomas Devine Vertical/short take-off and landing aircraft
US6685143B1 (en) * 2003-01-03 2004-02-03 Orbital Research Inc. Aircraft and missile forebody flow control device and method of controlling flow
US7108230B2 (en) * 2003-06-06 2006-09-19 Northrop Grumman Corporation Aircraft with topside only spoilers
US8511609B2 (en) * 2004-05-14 2013-08-20 The Boeing Company Structural mode shape alignment
US7997528B2 (en) * 2006-01-18 2011-08-16 Aereon Corporation Reducing runway requirement for aircraft
CN102009743B (zh) * 2010-07-01 2013-06-05 北京航空航天大学 基于吹气的机身大迎角俯仰力矩控制方法
KR101132841B1 (ko) * 2011-03-07 2012-04-02 김영재 봉합사
US9944383B2 (en) * 2015-09-29 2018-04-17 Illinois Institute Of Technology Pneumatic yaw control effector for aircraft
ITUA20164302A1 (it) * 2016-05-24 2017-11-24 Simone Bianchi Metodo per controllare la separazione del flusso aerodinamico su un aeromobile tramite correzione diretta dell'assetto.
US20190185127A1 (en) * 2017-12-18 2019-06-20 Freedom Aircraft Ventures Llc Aircraft design and technology
US11167836B2 (en) 2018-06-21 2021-11-09 Sierra Nevada Corporation Devices and methods to attach composite core to a surrounding structure
CN109335004B (zh) * 2018-11-30 2024-04-26 福建星图智控科技有限公司 一种配置混合动力的微型无人机
CN109466745A (zh) * 2018-12-29 2019-03-15 河北天启通宇航空器材科技发展有限公司 一种旋翼机尾翼结构

Family Cites Families (13)

* Cited by examiner, † Cited by third party
Publication number Priority date Publication date Assignee Title
GB522296A (en) * 1938-12-08 1940-06-13 Jacques Marie Paul Joseph Hube Improvements in or relating to aerodynes
GB959405A (en) * 1960-07-21 1964-06-03 Dornier Werke Gmbh Aircraft for forward and vertical take-off and landing
US4010920A (en) * 1971-09-17 1977-03-08 Farner Hans U Apparatus and method to control forward control surface type aircraft in flight
US3926389A (en) * 1972-05-24 1975-12-16 Messerschmitt Boelkow Blohm Aircraft of a controllable stability
SE381016B (sv) * 1973-05-04 1975-11-24 S E Larson Inbordes geometrisk placering av nosvinge och huvudvinge vid flygplan eller annan farkost
DE2327612A1 (de) * 1973-05-30 1974-12-19 Messerschmitt Boelkow Blohm Flugsicherheitsregelung und fluglagesteuerung, insbesondere auch fuer v/stolflugzeuge
US4012013A (en) * 1976-02-05 1977-03-15 The Boeing Company Variable camber inlet for supersonic aircraft
US4099687A (en) * 1976-07-22 1978-07-11 Roberts Lawrence T All-axis control of aircraft in deep stall
US4261533A (en) * 1978-06-26 1981-04-14 Dynamic Engineering, Inc. All-axis control of aircraft in ultra deep stall
DE2833771C2 (de) * 1978-08-02 1985-12-19 Messerschmitt-Bölkow-Blohm GmbH, 8000 München Verstellbarer Lufteinlauf, insbesondere zweidimensionaler Schrägstoßdiffusor für Gasturbinenstrahltriebwerke zum Antrieb von Hochleistungsflugzeugen
US4281810A (en) * 1979-04-19 1981-08-04 Office National D'etudes Et De Recherches Aerospatiales Process and an installation for the control of the efficiency of the aerodynamic surfaces of an aircraft
JPS5973395A (ja) * 1982-10-20 1984-04-25 三菱重工業株式会社 カナ−ド付き航空機
US4569493A (en) * 1983-03-14 1986-02-11 Grumman Aerospace Corporation Integrated multi-role variable sweep wing aircraft

Also Published As

Publication number Publication date
ES553775A0 (es) 1991-01-01
JPS621695A (ja) 1987-01-07
US4896846A (en) 1990-01-30
ES9100002A1 (es) 1991-01-01
DE3669852D1 (de) 1990-05-03
JP2534666B2 (ja) 1996-09-18
ATE51368T1 (de) 1990-04-15
IL78454A (en) 1992-05-25
EP0202020B1 (en) 1990-03-28
EP0202020A1 (en) 1986-11-20
IL78454A0 (en) 1986-08-31

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Legal Events

Date Code Title Description
B21A Patent or certificate of addition expired [chapter 21.1 patent gazette]

Free format text: PATENTE EXTINTA EM 08/04/2001