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1. 发明公开

EP4400415A1 SYSTEMS AND METHODS FOR CONTROLLING A VARIABLE CAMBER FLIGHT CONTROL SYSTEM OF AN AIRCRAFT IN A CRUISE FLIGHT PHASE 审中-公开
公开(公告)号：EP4400415A1
公开(公告)日：2024-07-17
申请号：EP24151062.7
申请日：2024-01-09
申请人： Bombardier Inc.
发明人： SERMEUS, Kurt
IPC分类号： B64C3/50 , B64C13/02 , B64C9/12 , B64C9/20 , B64C9/00
CPC分类号： B64C3/50 , B64C13/0425 , B64C9/12 , B64C2009/00520130101 , B64C9/20
摘要： The disclosed systems and methods for for controlling a variable camber (VC) flight control system (200) of an aircraft (10) in a cruise flight phase, comprising: i) in response to a first input from a user, operating the VC flight control system (200) in a first mode, the first mode configured to operate the aircraft (10) according to a passenger comfort goal, by maintaining a deck angle of the aircraft (10) at a low and substantially constant value; and ii) in response to a second input from the user, operating the VC flight control system (200) in a second mode, the second mode configured to operate the aircraft (10) according to an efficiency goal.

2. 发明公开

EP4101689A1 AIRCRAFT SEAT 审中-实审
公开(公告)号：EP4101689A1
公开(公告)日：2022-12-14
申请号：EP22188460.4
申请日：2015-09-24
申请人： Bombardier Inc. , Learjet Inc.
发明人： ERHEL, Philippe
IPC分类号： B60N2/14 , B60N2/06 , B60N2/34 , B60N2/22 , B60N2/18 , B60N2/75 , B60N2/838 , B60N2/66 , B60N2/00 , B60N2/02 , B64D11/06
摘要： A vehicle seat (142), comprising:
a seat pan (144), having a seat pan front edge and a seat pan rear edge, wherein the seat pan front edge defines a first pivot point and the seat pan rear edge defines a second pivot point;
a backrest (148), having a backrest top edge and a backrest bottom edge, wherein the backrest bottom edge is articulately disposed adjacent to the seat pan rear edge; and
a headrest (150), having a headrest top edge and a headrest bottom edge, wherein the headrest bottom edge is articulately disposed adjacent to the backrest top edge;
wherein the seat pan (144), the backrest (148), and the headrest (150) are positionable with respect to one another such that the seat is configurable into at least one of a taxi, takeoff and landing position, a napping position, and a sleeping position, and
wherein the first pivot point remains in a substantially fixed position for the taxi, takeoff and landing position and the napping position;
a swivel disposed beneath and supporting the seat, permitting the seat to rotate about a pivotal axis;
first and second armrests (152, 154) disposed on either side of the seat pan;
a first control (156) positioned in the first armrest, the first control being provided to lock and unlock movement of the seat in at least one of lateral and longitudinal directions;
a second control (158) positioned in the second armrest, the second control being provided to lock and unlock at least the swivel; and
a third control (160) positioned beneath the seat pan, the third control being a manual override.

3. 发明公开

EP3816038A1 THERMO-ACOUSTIC INSULATION SYSTEM, MODULE, AND AIRCRAFT INCLUDING THE SAME 审中-实审
公开(公告)号：EP3816038A1
公开(公告)日：2021-05-05
申请号：EP20205082.9
申请日：2020-10-31
申请人： Bombardier Inc.
发明人： VOICU, Carmen , LANGLOIS, Daniel , BLAIS, Jean-Francois
IPC分类号： B64C1/40
摘要： A thermo-acoustic insulation module for an aircraft includes a fiber batt defining an exterior side, an interior side, a thickness between the exterior side and the interior side, and a periphery. The thermo-acoustic insulation module also includes a mass layer disposed at least on the exterior side of the fiber batt, on the interior side of the fiber batt, or between the exterior side and the interior side of the fiber batt. An exterior encapsulating sheet is disposed exteriorly to the exterior side of the fiber batt. Similarly, an interior encapsulating sheet disposed interiorly to the interior side of the fiber batt. A peripheral seam connects the exterior encapsulating sheet to the interior encapsulating sheet adjacent to the periphery of the fiber batt, thereby creating an envelope encapsulating the fiber batt.

4. 发明公开

EP3741675A1 AIRCRAFT WITH CREW QUARTERS 有权
公开(公告)号：EP3741675A1
公开(公告)日：2020-11-25
申请号：EP20175913.1
申请日：2020-05-21
申请人： Bombardier Inc.
发明人： Galin, Alexandre , Ferneley, John , Ahn, Thomas , Banerjee, Siddhartho Konstantin
IPC分类号： B64D11/00
摘要： An aircraft, comprising: a fuselage including a cabin delimited by a cabin floor and having a passenger section and crew quarters separated from the passenger section, the crew quarters including an upper portion above a floor plane (P) defined by the cabin floor and a lower portion beneath the floor plane (P), the crew quarters including a seat being adjustable between a sitting configuration and a berthing configuration, the seat being upright in the sitting configuration such that a crew member in the seat is within both the upper and lower portions of the crew quarters.

5. 发明授权

EP3478574B1 METHODS AND SYSTEMS FOR DEPLOYING ADJACENT TRAILING EDGE FLAPS 有权
公开(公告)号：EP3478574B1
公开(公告)日：2020-11-18
申请号：EP17737175.4
申请日：2017-06-27
申请人： Bombardier Inc. , Learjet Inc.
发明人： AKEL, Iyad , BUDNITSKY, Dmitry , SMITH, Howard Ian , HANSON, Thomas
IPC分类号： B64C9/16 , B64C13/24

6. 发明公开

EP3730901A2 AIRCRAFT SYSTEM AND METHOD FOR ASSISTING A PILOT DURING FLIGHT 审中-公开
公开(公告)号：EP3730901A2
公开(公告)日：2020-10-28
申请号：EP20166536.1
申请日：2020-03-29
申请人： Bombardier Inc.
发明人： LEBEGUE, Olivier , OUELLETTE, Benoit
IPC分类号： G01C23/00
摘要： Methods and systems for assisting a pilot during flight of an aircraft are disclosed. The method includes receiving data indicative of a current location of the aircraft during flight and data indicative of a flight boundary, and determining that the flight boundary is relevant to the aircraft. The method also includes causing a display device to display a surface representing the flight boundary relative to the current location of the aircraft.

7. 发明公开

EP3712053A1 OPTICALLY ENHANCED AIRCRAFT WINDOW 审中-公开
公开(公告)号：EP3712053A1
公开(公告)日：2020-09-23
申请号：EP20164344.2
申请日：2020-03-19
申请人： Bombardier Inc.
发明人： CHIRIAC, Horatiu Daniel
IPC分类号： B64C1/14 , B64D11/00
摘要： A window includes a first transparent pane having a first surface and a second surface and a second transparent pane having a third surface and a fourth surface. The third surface faces the second surface and is separated from the first transparent pane by a distance. The window also includes an optical enhancer positioned at least one of between the second surface and the third surface, or adjacent to the fourth surface. The first transparent pane transmits light therethrough as a first image with a first image area. The optical enhancer receives the first image, modifies the first image, and produces a second image with a second image area larger than the first image area.

8. 发明公开

EP3701240A1 SYSTEM AND METHOD FOR DETECTING A FUEL LEAK IN AN AIRCRAFT 有权
公开(公告)号：EP3701240A1
公开(公告)日：2020-09-02
申请号：EP18871539.5
申请日：2018-10-19
申请人： Bombardier Inc.
发明人： VISCOTCHI, George , LAPORTE, Alexandre
IPC分类号： G01M3/26 , B64D37/00

9. 发明公开

EP3699081A1 AIRCRAFT WING WITH DISPLACEABLE WINGLET 有权
公开(公告)号：EP3699081A1
公开(公告)日：2020-08-26
申请号：EP20158984.3
申请日：2020-02-24
申请人： Bombardier Inc.
发明人： XI, Fengfeng , MOOSAVIAN, Amin , VIEIRA DE SA, Jose , CAMPOS NARANJO, Gabriel
IPC分类号： B64C3/42
摘要： A wing having a main wing section (11) with a forward spar (14A) and an aft spar (14B) extending through an internal cavity. The forward and aft spars are spaced apart and delimiting a dry segment of the internal cavity (19). A winglet (20) is rotatably coupled to the main wing section (11) by a cant hinge (30) defining a cant axis (32) about which the winglet (20) rotates relative to the main wing section (11) between an extended position in which the winglet (20) is aligned with the main wing section (11), and a folded position in which the winglet (20) is rotated about the cant axis (32). A linkage assembly (40) disposed in the dry segment is pivotably mounted to one of the forward and aft spars (14A, 14B) and is coupled to the cant hinge (30). The linkage assembly (40) is displaceable to apply a force to move the winglet (20) between the extended position and the folded position during flight of the aircraft.

10. 发明公开

EP3697691A1 AIRCRAFT PYLON FAIRING 审中-公开
公开(公告)号：EP3697691A1
公开(公告)日：2020-08-26
申请号：EP18867996.3
申请日：2018-10-15
申请人： Bombardier Inc.
发明人： SADRI, Reza , DUSSAULT, Kathleen , BOILEAU, Edmond
IPC分类号： B64D29/02 , B64C7/00 , B64D27/12

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