WO2010136572A3 - Head-up display - Google Patents
Head-up display Download PDFInfo
- Publication number
- WO2010136572A3 WO2010136572A3 PCT/EP2010/057433 EP2010057433W WO2010136572A3 WO 2010136572 A3 WO2010136572 A3 WO 2010136572A3 EP 2010057433 W EP2010057433 W EP 2010057433W WO 2010136572 A3 WO2010136572 A3 WO 2010136572A3
- Authority
- WO
- WIPO (PCT)
- Prior art keywords
- arm
- axis
- screen mounting
- display
- head
- Prior art date
Links
Classifications
-
- G—PHYSICS
- G02—OPTICS
- G02B—OPTICAL ELEMENTS, SYSTEMS OR APPARATUS
- G02B27/00—Optical systems or apparatus not provided for by any of the groups G02B1/00 - G02B26/00, G02B30/00
- G02B27/01—Head-up displays
- G02B27/0149—Head-up displays characterised by mechanical features
-
- B—PERFORMING OPERATIONS; TRANSPORTING
- B64—AIRCRAFT; AVIATION; COSMONAUTICS
- B64D—EQUIPMENT FOR FITTING IN OR TO AIRCRAFT; FLIGHT SUITS; PARACHUTES; ARRANGEMENTS OR MOUNTING OF POWER PLANTS OR PROPULSION TRANSMISSIONS IN AIRCRAFT
- B64D43/00—Arrangements or adaptations of instruments
Abstract
The invention relates to a head-up display (1) including: a base (2) attached to the cockpit (C) of an aircraft, an arm (3) connected by one end to the base (2) and by the other end to a screen mounting (4) capable of pivoting relative to the arm (3) about a second axis (X2), characterised in that said display includes: a means (44) for transmitting a rotary movement of the arm (3) relative to the base (2), about a first axis (X1), to a cam (28) that is rotatably mobile about a second axis (X2); a cam follower (27) rigidly connected to the screen mounting (4) rotatable about the second axis (X2), suitable for passing on the rotary movement of the cam (28) to the screen mounting (4) when the screen mounting (4) is not resting against a stop (39, 40) of the arm (3); a means (20) for applying a calibrated force in a direction parallel to the second axis (X2), referred to as the axial direction, capable of eliminating the tangential play between the screen mounting (4) and the arm (3) when the head-up display (1) is in operational position.
Applications Claiming Priority (2)
Application Number | Priority Date | Filing Date | Title |
---|---|---|---|
FR0902614 | 2009-05-29 | ||
FR0902614A FR2946156B1 (en) | 2009-05-29 | 2009-05-29 | HEAD VISUALIZATION DEVICE |
Publications (2)
Publication Number | Publication Date |
---|---|
WO2010136572A2 WO2010136572A2 (en) | 2010-12-02 |
WO2010136572A3 true WO2010136572A3 (en) | 2011-02-24 |
Family
ID=42035988
Family Applications (1)
Application Number | Title | Priority Date | Filing Date |
---|---|---|---|
PCT/EP2010/057433 WO2010136572A2 (en) | 2009-05-29 | 2010-05-28 | Head-up display |
Country Status (2)
Country | Link |
---|---|
FR (1) | FR2946156B1 (en) |
WO (1) | WO2010136572A2 (en) |
Families Citing this family (5)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
JP6435159B2 (en) * | 2014-10-17 | 2018-12-05 | ミネベアミツミ株式会社 | Angle adjustment mechanism and display device |
EP3422078B1 (en) * | 2017-06-30 | 2020-12-23 | Valeo Comfort and Driving Assistance | Combiner positioning unit for a head-up display system, head-up display system and vehicle |
GB2571900B (en) * | 2017-10-25 | 2021-06-09 | Bae Systems Plc | Support for optical combiner of head up display |
WO2019081884A1 (en) * | 2017-10-25 | 2019-05-02 | Bae Systems Plc | Support for optical combiner of head up display |
EP3477358A1 (en) * | 2017-10-25 | 2019-05-01 | BAE SYSTEMS plc | Support for optical combiner of head up display |
Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US851019A (en) * | 1906-07-17 | 1907-04-23 | Johann Michael Model | Cage-ring for ball-bearings. |
US3530355A (en) * | 1968-10-14 | 1970-09-22 | John Alfred Hodgkins | Automatic control systems |
NL6907757A (en) * | 1969-05-21 | 1970-11-24 | ||
US4188090A (en) * | 1977-06-01 | 1980-02-12 | Elliott Brothers (London) Limited | Retractable head-up displays |
US4749256A (en) * | 1987-02-13 | 1988-06-07 | Gec Avionics, Inc. | Mounting apparatus for head-up display |
DE4322540A1 (en) * | 1992-07-10 | 1994-01-13 | Magnetic Elektromotoren Gmbh | Ball lead-screw drive transmission with overload protection - provided by mechanical switch element triggered at set load point to shut down drive |
EP0674203A1 (en) * | 1994-03-25 | 1995-09-27 | Sextant Avionique | Storage device for a holographic mirror, in particular for aircraft |
EP1610009A1 (en) * | 2003-04-03 | 2005-12-28 | Koyo Seiko Co., Ltd. | Offset thrust bearing |
US20070183055A1 (en) * | 2005-11-10 | 2007-08-09 | Eyal Maliah | Head up display mechanism |
-
2009
- 2009-05-29 FR FR0902614A patent/FR2946156B1/en active Active
-
2010
- 2010-05-28 WO PCT/EP2010/057433 patent/WO2010136572A2/en active Application Filing
Patent Citations (9)
Publication number | Priority date | Publication date | Assignee | Title |
---|---|---|---|---|
US851019A (en) * | 1906-07-17 | 1907-04-23 | Johann Michael Model | Cage-ring for ball-bearings. |
US3530355A (en) * | 1968-10-14 | 1970-09-22 | John Alfred Hodgkins | Automatic control systems |
NL6907757A (en) * | 1969-05-21 | 1970-11-24 | ||
US4188090A (en) * | 1977-06-01 | 1980-02-12 | Elliott Brothers (London) Limited | Retractable head-up displays |
US4749256A (en) * | 1987-02-13 | 1988-06-07 | Gec Avionics, Inc. | Mounting apparatus for head-up display |
DE4322540A1 (en) * | 1992-07-10 | 1994-01-13 | Magnetic Elektromotoren Gmbh | Ball lead-screw drive transmission with overload protection - provided by mechanical switch element triggered at set load point to shut down drive |
EP0674203A1 (en) * | 1994-03-25 | 1995-09-27 | Sextant Avionique | Storage device for a holographic mirror, in particular for aircraft |
EP1610009A1 (en) * | 2003-04-03 | 2005-12-28 | Koyo Seiko Co., Ltd. | Offset thrust bearing |
US20070183055A1 (en) * | 2005-11-10 | 2007-08-09 | Eyal Maliah | Head up display mechanism |
Also Published As
Publication number | Publication date |
---|---|
FR2946156B1 (en) | 2011-06-24 |
FR2946156A1 (en) | 2010-12-03 |
WO2010136572A2 (en) | 2010-12-02 |
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