BR7408722A - Sistema aperfeicoado de aumento de intuicao de boas condicoes de voo sem consulta a aparelho de medida - Google Patents

Sistema aperfeicoado de aumento de intuicao de boas condicoes de voo sem consulta a aparelho de medida

Info

Publication number: BR7408722A
Authority: BR; Brazil
Prior art keywords: intuition; consulting; increasing; measuring device; improved system
Prior art date: 1973-10-23

Application number

BR8722/74A

Other languages

English (en)

Inventor

H Heiney

Original Assignee

United Aircraft Corp

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.)

1973-10-23

Filing date

1974-10-18

Publication date

1975-11-04

1974-10-18 Application filed by United Aircraft Corp filed Critical United Aircraft Corp

1975-11-04 Publication of BR7408722A publication Critical patent/BR7408722A/pt

Classifications

- 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
- B64C13/24—Transmitting means
- B64C13/38—Transmitting means with power amplification
- B64C13/40—Transmitting means with power amplification using fluid pressure
- B64C13/46—Transmitting means with power amplification using fluid pressure with artificial feel

Landscapes

Engineering & Computer Science (AREA)
Physics & Mathematics (AREA)
Fluid Mechanics (AREA)
Automation & Control Theory (AREA)
Aviation & Aerospace Engineering (AREA)
Fluid-Pressure Circuits (AREA)
Mechanical Control Devices (AREA)

BR8722/74A 1973-10-23 1974-10-18 Sistema aperfeicoado de aumento de intuicao de boas condicoes de voo sem consulta a aparelho de medida BR7408722A (pt)

Applications Claiming Priority (1)

Application Number	Priority Date	Filing Date	Title
US408876A US3862730A (en)	1973-10-23	1973-10-23	Fas actuation system

Publications (1)

Publication Number	Publication Date
BR7408722A true BR7408722A (pt)	1975-11-04

Family

ID=23618138

Family Applications (1)

Application Number	Title	Priority Date	Filing Date
BR8722/74A BR7408722A (pt)	1973-10-23	1974-10-18	Sistema aperfeicoado de aumento de intuicao de boas condicoes de voo sem consulta a aparelho de medida

Country Status (10)

Country	Link
US (1)	US3862730A (pt)
JP (1)	JPS5072400A (pt)
BR (1)	BR7408722A (pt)
CA (1)	CA993851A (pt)
DE (1)	DE2450158A1 (pt)
FR (1)	FR2248194B1 (pt)
GB (1)	GB1478524A (pt)
IL (1)	IL45617A (pt)
IT (1)	IT1025111B (pt)
MY (1)	MY7800298A (pt)

Families Citing this family (31)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3960348A (en) *	1975-08-04	1976-06-01	United Technologies Corporation	Aerodynamic surface control feel augmentation system
US4477043A (en) *	1982-12-15	1984-10-16	The United States Of America As Represented By The Secretary Of The Air Force	Biodynamic resistant control stick
US4477044A (en) *	1983-01-17	1984-10-16	The Boeing Company	Elevator feel actuator
JP2536508Y2 (ja) *	1990-11-22	1997-05-21	三菱農機株式会社	移動農機
US6293497B1 (en)	1996-10-22	2001-09-25	The Boeing Company	Airplane with unswept slotted cruise wing airfoil
JP3995752B2 (ja) *	1997-03-14	2007-10-24	アビックス株式会社	マンマシン・インタフェースの入力装置
US7258308B2 (en) *	2002-07-02	2007-08-21	The Boeing Company	Method and apparatus for controlling airflow with a gapped trailing edge device having a flexible flow surface
US7059563B2 (en) *	2003-06-03	2006-06-13	The Boeing Company	Systems, apparatuses, and methods for moving aircraft control surfaces
US7243881B2 (en)	2003-06-03	2007-07-17	The Boeing Company	Multi-function trailing edge devices and associated methods
US6799739B1 (en) *	2003-11-24	2004-10-05	The Boeing Company	Aircraft control surface drive system and associated methods
US7424350B2 (en)	2004-02-02	2008-09-09	The Boeing Company	Vehicle control systems and corresponding sizing methods
US7357358B2 (en) *	2004-02-27	2008-04-15	The Boeing Company	Aircraft leading edge device systems and corresponding sizing methods
US7270305B2 (en) *	2004-06-15	2007-09-18	The Boeing Company	Aircraft leading edge apparatuses and corresponding methods
US6978971B1 (en) *	2004-06-15	2005-12-27	The Boeing Company	Methods and apparatuses for controlling airflow proximate to engine/airfoil systems
US7494094B2 (en) *	2004-09-08	2009-02-24	The Boeing Company	Aircraft wing systems for providing differential motion to deployable lift devices
US7264206B2 (en) *	2004-09-30	2007-09-04	The Boeing Company	Leading edge flap apparatuses and associated methods
US7322547B2 (en) *	2005-01-31	2008-01-29	The Boeing Company	Aerospace vehicle leading edge slat devices and corresponding methods
US7338018B2 (en) *	2005-02-04	2008-03-04	The Boeing Company	Systems and methods for controlling aircraft flaps and spoilers
US7309043B2 (en) *	2005-04-27	2007-12-18	The Boeing Company	Actuation device positioning systems and associated methods, including aircraft spoiler droop systems
US7721999B2 (en) *	2005-05-20	2010-05-25	The Boeing Company	Aerospace vehicle fairing systems and associated methods
US7300021B2 (en) *	2005-05-20	2007-11-27	The Boeing Company	Aerospace vehicle fairing systems and associated methods
US7367530B2 (en) *	2005-06-21	2008-05-06	The Boeing Company	Aerospace vehicle yaw generating systems and associated methods
US7500641B2 (en) *	2005-08-10	2009-03-10	The Boeing Company	Aerospace vehicle flow body systems and associated methods
US7611099B2 (en) *	2005-09-07	2009-11-03	The Boeing Company	Seal assemblies for use with drooped spoilers and other control surfaces on aircraft
US7708231B2 (en) *	2005-11-21	2010-05-04	The Boeing Company	Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods
US7475854B2 (en)	2005-11-21	2009-01-13	The Boeing Company	Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods
US7578484B2 (en) *	2006-06-14	2009-08-25	The Boeing Company	Link mechanisms for gapped rigid krueger flaps, and associated systems and methods
US7954769B2 (en)	2007-12-10	2011-06-07	The Boeing Company	Deployable aerodynamic devices with reduced actuator loads, and related systems and methods
US7766282B2 (en) *	2007-12-11	2010-08-03	The Boeing Company	Trailing edge device catchers and associated systems and methods
US8382045B2 (en) *	2009-07-21	2013-02-26	The Boeing Company	Shape-changing control surface
US10196131B2 (en) *	2016-02-16	2019-02-05	The Boeing Company	Hydraulic system and method for an aircraft flight control system

Family Cites Families (3)

* Cited by examiner, † Cited by third party
Publication number	Priority date	Publication date	Assignee	Title
US3450375A (en) *	1967-02-02	1969-06-17	Bertea Corp	Load feel computer
US3438306A (en) *	1967-02-07	1969-04-15	Lear Siegler Inc	Preloaded servo actuator controls for redundant systems
US3733039A (en) *	1971-05-20	1973-05-15	United Aircraft Corp	Feel augmentation control system for helicopters

1973
- 1973-10-23 US US408876A patent/US3862730A/en not_active Expired - Lifetime
1974
- 1974-06-05 CA CA201,747A patent/CA993851A/en not_active Expired
- 1974-06-09 IL IL45617A patent/IL45617A/xx unknown
- 1974-09-03 FR FR7429880A patent/FR2248194B1/fr not_active Expired
- 1974-10-18 BR BR8722/74A patent/BR7408722A/pt unknown
- 1974-10-21 GB GB45455/74A patent/GB1478524A/en not_active Expired
- 1974-10-22 JP JP49121884A patent/JPS5072400A/ja active Pending
- 1974-10-22 DE DE19742450158 patent/DE2450158A1/de not_active Ceased
- 1974-10-23 IT IT28683/74A patent/IT1025111B/it active
1978
- 1978-12-30 MY MY298/78A patent/MY7800298A/xx unknown

Also Published As

Publication number	Publication date
JPS5072400A (pt)	1975-06-14
IL45617A0 (en)	1975-03-13
US3862730A (en)	1975-01-28
IT1025111B (it)	1978-08-10
FR2248194B1 (pt)	1981-11-20
IL45617A (en)	1977-06-30
AU7295174A (en)	1976-03-11
MY7800298A (en)	1978-12-31
DE2450158A1 (de)	1975-09-04
GB1478524A (en)	1977-07-06
FR2248194A1 (pt)	1975-05-16
CA993851A (en)	1976-07-27

Publication	Publication Date	Title
BR7408722A (pt)	1975-11-04	Sistema aperfeicoado de aumento de intuicao de boas condicoes de voo sem consulta a aparelho de medida
BR7504984A (pt)	1976-08-03	Sistema de foco-deteccao optoeletronico
SE392199B (sv)	1977-03-14	Anordning for uppvermning medelst mikrovagor
SE399200B (sv)	1978-02-06	Anordning for avgivande av slag
BR7410464D0 (pt)	1975-09-16	Sistema aperfeicoado de fotocontrole
SE397043B (sv)	1977-10-17	Anordning for fileing av fiskar
SE418675B (sv)	1981-06-22	Anordning for fastsettning av festorgan
NL7413008A (nl)	1975-04-22	Stelsel voor snelheidsmeting.
DK329576A (da)	1977-01-23	Overvagningssystem
BR7503053A (pt)	1976-04-13	Sistema de linha de montagem
BR7403520D0 (pt)	1974-12-03	Sistema de elevador
BR7408742D0 (pt)	1975-09-23	Sistema de elevador
BR7404162D0 (pt)	1975-01-07	Sistema de elevador
IT1026640B (it)	1978-10-20	Sistema di visualizzazione perfezionato
SE394983B (sv)	1977-07-25	Anordning for overvakning av funktionen av ett antilasningsreglersystem
NO138481C (no)	1978-09-13	Anlegg for utporsjonering av vaeske
SE389743B (sv)	1976-11-15	Anordning for provning av dioder
IT1025299B (it)	1978-08-10	Dispositivo per armare l otturatore
BR7403425D0 (pt)	1974-12-03	Conexao de cano
SE399983B (sv)	1978-03-06	Anordning for uttagning av brenslet ur ett kapslat kernbrensleelement
SE385498B (sv)	1976-07-05	Anordning vid terrenggaende artilleripjes
SE388970B (sv)	1976-10-18	Avbojningsdon for katodstraleror
SE387556B (sv)	1976-09-13	Anordning for instellning av skerhallare
SU514273A1 (ru)	1976-05-15	Устройство дл контрол состо ний объекта управлени
BR7403429D0 (pt)	1974-12-03	Conexao de cano